diff --git a/ale/drivers/co_drivers.py b/ale/drivers/co_drivers.py
index 25eb2091ac23206b5ee3aed5bc4f5fdda8962179..fb4cf135332a098b07fff40e03745545fef0852c 100644
--- a/ale/drivers/co_drivers.py
+++ b/ale/drivers/co_drivers.py
@@ -11,8 +11,6 @@ from ale.base.label_pds3 import Pds3Label
 from ale.base.type_distortion import RadialDistortion
 from ale.base.type_sensor import Framer
 
-from ale.util import find_latest_metakernel
-
 from ale.rotation import ConstantRotation
 from ale.transformation import FrameChain
 from scipy.spatial.transform import Rotation
diff --git a/tests/pytests/data/N1702360370_1/11344_11349ra_sliced-82000.xc b/tests/pytests/data/N1702360370_1/11344_11349ra_sliced-82000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..a97644c9406c7b19bd0a875c5b6e9f23dd5e75cf
--- /dev/null
+++ b/tests/pytests/data/N1702360370_1/11344_11349ra_sliced-82000.xc
@@ -0,0 +1,19490 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
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+'ckernel.file                                                '
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+'3C170367A^A'
+'3C17036BA^A'
+'3C17036FA^A'
+'3C170373A^A'
+'3C170377A^A'
+'3C17037BA^A'
+'3C17037FA^A'
+'3C170383A^A'
+'3C170387A^A'
+'3C17038BA^A'
+'3C17038FA^A'
+'3C17039207^A'
+'3C16DF336^A'
+'3C16E0C36^A'
+'3C16E2536^A'
+'3C16E3E36^A'
+'3C16E573A^A'
+'3C16E703A^A'
+'3C16E893A^A'
+'3C16EA23A^A'
+'3C16EBB3A^A'
+'3C16ED43A^A'
+'3C16EED3A^A'
+'3C16F063A^A'
+'3C16F1F3A^A'
+'3C16F383A^A'
+'3C16F513A^A'
+'3C16F6A3A^A'
+'3C16F833A^A'
+'3C16F9C3A^A'
+'3C16FB53A^A'
+'3C16FCE3A^A'
+'3C16FE73A^A'
+'3C170003A^A'
+'3C170193A^A'
+'3C170323A^A'
+'3C16DDA84B^A'
+'1^1'
+'97C^3'
+END_ARRAY 1 19451
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /home/kberry/dev/knoten/knoten/examples/data/N1702360370_1.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/N1702360370_1/IssNAAddendum004.ti b/tests/pytests/data/N1702360370_1/IssNAAddendum004.ti
new file mode 100644
index 0000000000000000000000000000000000000000..fee1f26f015610b74ca43b89557bc1aa3adc3b0c
--- /dev/null
+++ b/tests/pytests/data/N1702360370_1/IssNAAddendum004.ti
@@ -0,0 +1,112 @@
+Data was gathered from the Isis2 file: iss_parameters.def.1
+
+The Default focal length is not being used, but was left in
+from isis2.
+
+The boresight of the instrument has been updated to the center
+of the detector.  Previous values were used along with specific
+CK rotation angle frames that were propagated from ISIS2.  These
+values proved to be incorrect and have subsequently been corrected
+so as to use the frames kernel directly as provided by NAIF.  See
+below for additional details pertaining to the SPICE frames
+kernels as there is some special handling of this kernel.
+(KJB, 2009-01-22)
+
+\begindata
+INS-82360_BORESIGHT_LINE=512.5
+INS-82360_BORESIGHT_SAMPLE=512.5
+
+INS-82360_DEFAULT_FOCAL_LENGTH=2003.44
+INS-82360_BL1_CL2_FOCAL_LENGTH=2002.79
+INS-82360_CL1_CL2_FOCAL_LENGTH=2002.88
+INS-82360_CL1_GRN_FOCAL_LENGTH=2002.75
+INS-82360_CL1_IR1_FOCAL_LENGTH=2002.74
+INS-82360_RED_CL2_FOCAL_LENGTH=2002.69
+INS-82360_CL1_IR3_FOCAL_LENGTH=2002.65
+INS-82360_CL1_BL2_FOCAL_LENGTH=2002.37
+INS-82360_CL1_CB1_FOCAL_LENGTH=2002.66
+INS-82360_CL1_CB2_FOCAL_LENGTH=2002.66
+INS-82360_CL1_CB3_FOCAL_LENGTH=2002.68
+INS-82360_CL1_MT1_FOCAL_LENGTH=2002.88
+INS-82360_CL1_MT2_FOCAL_LENGTH=2002.91
+INS-82360_CL1_MT3_FOCAL_LENGTH=2002.87
+INS-82360_CL1_UV3_FOCAL_LENGTH=2003.09
+INS-82360_HAL_CL2_FOCAL_LENGTH=2002.94
+INS-82360_IR2_CL2_FOCAL_LENGTH=2002.71
+INS-82360_IR2_IR1_FOCAL_LENGTH=2002.56
+INS-82360_IR2_IR3_FOCAL_LENGTH=2002.55
+INS-82360_IR4_CL2_FOCAL_LENGTH=2002.89
+INS-82360_IR4_IR3_FOCAL_LENGTH=2002.81
+INS-82360_IRP0_CB2_FOCAL_LENGTH=2002.48
+INS-82360_IRP0_CB3_FOCAL_LENGTH=2002.74
+INS-82360_IRP0_IR1_FOCAL_LENGTH=2002.60
+INS-82360_IRP0_IR3_FOCAL_LENGTH=2002.48
+INS-82360_IRP0_MT2_FOCAL_LENGTH=2002.72
+INS-82360_IRP0_MT3_FOCAL_LENGTH=2002.72
+INS-82360_P0_BL2_FOCAL_LENGTH=2002.19
+INS-82360_P0_CB1_FOCAL_LENGTH=2002.30
+INS-82360_P0_GRN_FOCAL_LENGTH=2002.38
+INS-82360_P0_IR1_FOCAL_LENGTH=2002.35
+INS-82360_P0_MT1_FOCAL_LENGTH=2002.40
+INS-82360_P0_UV3_FOCAL_LENGTH=2002.71
+INS-82360_P120_BL2_FOCAL_LENGTH=2002.11
+INS-82360_P120_CB1_FOCAL_LENGTH=2002.28
+INS-82360_P120_GRN_FOCAL_LENGTH=2002.38
+INS-82360_P120_IR1_FOCAL_LENGTH=2002.39
+INS-82360_P120_MT1_FOCAL_LENGTH=2002.54
+INS-82360_P120_UV3_FOCAL_LENGTH=2002.71
+INS-82360_P60_BL2_FOCAL_LENGTH=2002.13
+INS-82360_P60_CB1_FOCAL_LENGTH=2002.18
+INS-82360_P60_GRN_FOCAL_LENGTH=2002.28
+INS-82360_P60_IR1_FOCAL_LENGTH=2002.36
+INS-82360_P60_MT1_FOCAL_LENGTH=2002.34
+INS-82360_P60_UV3_FOCAL_LENGTH=2002.51
+INS-82360_RED_GRN_FOCAL_LENGTH=2002.61
+INS-82360_RED_IR1_FOCAL_LENGTH=2002.48
+INS-82360_UV1_CL2_FOCAL_LENGTH=2003.03
+INS-82360_UV2_CL2_FOCAL_LENGTH=2002.91
+INS-82360_UV2_UV3_FOCAL_LENGTH=2002.90
+
+INS-82360_PIXEL_PITCH=.012
+
+INS-82360_TRANSX=(0.0 0.012 0.0)
+INS-82360_TRANSY=(0.0 0.0 0.012)
+
+INS-82360_ITRANSS=(0.0 83.333333333333333 0.0)
+INS-82360_ITRANSL=(0.0 0.0 83.333333333333333)
+
+INS-82360_K1=.000008
+\begintext
+
+The Cassini ISS NAC frames kernel is missing one final rotation in its
+CK frames hierarchy.  A 180 degree rotation about the detector center
+(Z-axis) is required to map into the proper detector orientation.  This
+is not included in the NAIF SPICE frames kernel (cas_v??.tf).  The following
+frames definition applies the rotation into camera coordinates and must
+be the frame used in the ISIS camera model converting from the s/c frame to
+the instrument. (KJB, 2009-01-22)
+
+\begindata
+INS_-82360_FRAME_ID           = 14082360
+FRAME_CASSINI_ISS_NAC_USGS    = 14082360
+FRAME_14082360_NAME           = 'CASSINI_ISS_NAC_USGS'
+FRAME_14082360_CLASS          = 4
+FRAME_14082360_CLASS_ID       = 14082360
+FRAME_14082360_CENTER         = -82
+TKFRAME_14082360_SPEC         = 'ANGLES'
+TKFRAME_14082360_RELATIVE     = 'CASSINI_ISS_NAC'
+TKFRAME_14082360_ANGLES       = (0.0,       0.0,    180.0)
+TKFRAME_14082360_AXES         = (  1,         2,        3)
+TKFRAME_14082360_UNITS        = 'DEGREES' 
+
+\begintext
+These are the parameters required for writing c-kernels.  Isis will
+create ck with the same frame endpoints as the mission ck.  For 
+the Cassini spacecraft the ck frame is CASSINI_SC_COORD (-915240), and the
+ck reference frame is J2000 (1).
+
+\begindata
+INS-82360_CK_FRAME_ID=-915240
+INS-82360_CK_REFERENCE_ID=1
+
+\begintext
diff --git a/tests/pytests/data/N1702360370_1/N1702360370_1.xsp b/tests/pytests/data/N1702360370_1/N1702360370_1.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..7e8aaa387bae32ac47b0782293c1d46f0fc4b438
--- /dev/null
+++ b/tests/pytests/data/N1702360370_1/N1702360370_1.xsp
@@ -0,0 +1,3838 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE                                                    '
+BEGIN_ARRAY 1 27
+'MONTE Chebyshev Polynomial Table        '
+'16778BEB67C52B^8'
+'1677B1D5138C06^8'
+'6'
+'0'
+'1'
+'2'
+27
+'1673634^8'
+'1518^6'
+'-501DB261070EEC^8'
+'40D164879F63D4^6'
+'6D711F932804C8^4'
+'-155D24F6AB106C^2'
+'-A0D6AD2C2B2DB^-1'
+'2D8D53CCE8ECDE^-3'
+'-1FEC754F06006E^-5'
+'-1EF46D61F63797^8'
+'-AE37B376BDA788^6'
+'2A4AB5EB14A5C6^4'
+'2517851BDBC436^2'
+'-7FD3D92FF196C4^-1'
+'-136D6136733132^-3'
+'-2F720EAE306416^-7'
+'-9563BB5985F9D8^7'
+'-4AC00FE528AB2^6'
+'CC16A69959BB5^3'
+'103D903DA7712A^2'
+'-2DDBE2283246D4^-1'
+'-A0C7390361E6B8^-4'
+'63340E101EDA68^-7'
+'165E4B4^8'
+'2A3^6'
+'17^2'
+'1^1'
+END_ARRAY 1 27
+BEGIN_ARRAY 2 39
+'MONTE Chebyshev Polynomial Table        '
+'16778BEB67C52B^8'
+'1677B1D5138C06^8'
+'A'
+'0'
+'1'
+'2'
+39
+'167DEF4^8'
+'A8C^5'
+'-78B33D8750302^5'
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+'15A5F67A7013E^2'
+'-15653FF2E1C45E^0'
+'2ACAB3DAAF301A^-1'
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+'-51B097F4C369F4^-3'
+'24BFA44796B2BA^-3'
+'-3E86333515D9B2^-4'
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+'20DC2FC47284A^-5'
+'-2A40556F1D72FA^5'
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+'10F84639827753^2'
+'B83C4B4D3E3C28^-1'
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+'19E42F9309D293^-6'
+'1673634^8'
+'1518^6'
+'23^2'
+'1^1'
+END_ARRAY 2 39
+BEGIN_ARRAY 3 104
+'MONTE Chebyshev Polynomial Table        '
+'16778BEB67C52B^8'
+'1677B1D5138C06^8'
+'25A'
+'6'
+'1'
+'2'
+104
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+'-B2AAFD^-4'
+'5A483D4^-4'
+'1676AF^8'
+'FD2^4'
+'32^2'
+'2^1'
+END_ARRAY 3 104
+BEGIN_ARRAY 4 3601
+'MONTE Difference Line Table             '
+'16778BEB67C52B^8'
+'1677B1D5138C06^8'
+'-52'
+'6'
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+1024
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+'C130C69995E948^-A'
+'-98721074830E7^-C'
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+'0^0'
+'177D96E805185A^-2'
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+'3102B482B5F346^-6'
+'-12C3B90136410B^-8'
+'-85F9211E969CB^-A'
+'2C49DDBFA947BE^-B'
+'-A44F4F5A1CF708^-D'
+'-16C^-D'
+'0^0'
+'0^0'
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+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'6D2A317D600FE4^-4'
+'299DE7659273CE^-5'
+'-65BEC917051384^-7'
+'A1E8929EA3A5F^-9'
+'-7136FB6C97F6B4^-B'
+'-151234994C0DC^-C'
+'950D4^-D'
+'0^0'
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+'6^1'
+'1677B0DC2A9F93^8'
+'3737D2D00D^2'
+'6E6FA5A01A^2'
+'A5A7787027^2'
+'E4C2B2827F^2'
+'123DDEC94D7^3'
+'162F926A72F^3'
+'18286C3B05B^3'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'30A2635E790A86^5'
+'F14D173D12FB7^1'
+'-2DC1159F6FB96C^5'
+'44D10C603BA8A8^1'
+'-F188A9B5452FA8^3'
+'-19641616DDA285^1'
+'-1833579C1BB254^-2'
+'4577B804CDA088^-5'
+'20538199938D0C^-6'
+'-83703BD23583^-8'
+'16FA089AE71B0C^-9'
+'-1D4A048F506258^-B'
+'-BF6^-D'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'16BD918A29A289^-2'
+'-23E9C93C1F23BA^-4'
+'317605DD297154^-6'
+'-1DC4A10199CF98^-8'
+'-E550C298FB3D^-A'
+'69322914A2AFEC^-B'
+'-194EDA38433D54^-C'
+'-75E^-D'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'78C5A1AAE86054^-4'
+'224B811C5DC056^-5'
+'-637A447831C74C^-7'
+'D482F448F7F1C8^-9'
+'-F604F562506E7^-B'
+'-5D0B17DD398EA8^-C'
+'888E4^-D'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'8^1'
+'6^1'
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+'2F8F951433^2'
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+'A40955C30F^2'
+'DB4128931C^2'
+'11278FB6329^3'
+'149B0CE3336^3'
+'180E8A10343^3'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'31A43BA24E4FA2^5'
+'EFAEB565377248^1'
+'-2D767E58784AB8^5'
+'46513D357A0AA^1'
+'-10CBD52888FAEF^4'
+'-195BA51D6AF82^1'
+'-181BF465C142E^-2'
+'4431F04BD7780C^-5'
+'17B13337611488^-6'
+'-620950B47F63C^-8'
+'10DD8B63261D3E^-9'
+'-16E22DB599DA36^-B'
+'-684^-D'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'160DE7B1F1349C^-2'
+'-1E19C57E75BFB4^-4'
+'26CEEFC52DAE6E^-6'
+'-1A9816449975F8^-8'
+'-9645F3464A7928^-A'
+'44B91E73E67254^-B'
+'-12505C5BC786F2^-C'
+'-1CE^-D'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'8312A97C417698^-4'
+'1BE4F2151E2B1D^-5'
+'-4BC68418DC5B54^-7'
+'A3579CC5D9406^-9'
+'-C5D4E09A7E67A^-B'
+'-1E56942FA9A288^-C'
+'-C1C88^-D'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'8^1'
+'6^1'
+'7^1'
+'6^1'
+'16778C04187F3B^8'
+'16778EAB960D4C^8'
+'16778FAD49A1E3^8'
+'16779^8'
+'1677900001^8'
+'167790000406FC^8'
+'16779000219332^8'
+'16779000A4C66D^8'
+'167790043D390C^8'
+'1677901B2B544B^8'
+'16779085CAD2CD^8'
+'167791681887D4^8'
+'1677920BE8EA63^8'
+'167792CD338195^8'
+'167793B4888D0C^8'
+'1677946EEDAFCA^8'
+'1677954B06403E^8'
+'16779636EE4037^8'
+'167796E7DC4031^8'
+'167797B439FD9B^8'
+'167798746D9AC3^8'
+'167798FEDE4241^8'
+'167799C66A6C4D^8'
+'16779A88735D2E^8'
+'16779B23ADB77C^8'
+'16779C1B12B768^8'
+'16779CC4DA8A2D^8'
+'16779D9F18CFEC^8'
+'16779E45AB7467^8'
+'16779F1BD5B597^8'
+'1677A00613ECE4^8'
+'1677A0E0B464C5^8'
+'1677A20435049C^8'
+'1677A2DED57C7E^8'
+'1677A3C71FFBDD^8'
+'1677A4F603A1F3^8'
+'1677A622C944DF^8'
+'1677A77E597A5C^8'
+'1677A87866EACB^8'
+'1677A970C3D548^8'
+'1677AA253757A7^8'
+'1677AAB3D4B24C^8'
+'1677AB70D7D094^8'
+'1677ABEF3B417^8'
+'1677ACBBA61E46^8'
+'1677ADBB3CEB69^8'
+'1677AEDB6D67BE^8'
+'1677AFB84CB2FE^8'
+'1677B0DC2A9F93^8'
+'1677B1EEA39AF6^8'
+'32^2'
+END_ARRAY 4 3601
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /home/kberry/kernel_slice_smaller/N1702360370_1.bsp LOG FILE
+
+; Created 2019-09-05/15:12:52.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL   = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL           = /home/kberry/kernel_slice_smaller/N1702360370_1.bsp
+SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/cassini/kernels/spk/180628RU_SCPSE_11337_11357.bsp
+    INCLUDE_COMMENTS = NO
+    BODIES           = 6, 10, -82, 602
+    BEGIN_TIME       = 2011 DEC 12 03:41:29.222
+    END_TIME         = 2011 DEC 12 06:23:14.893
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/N1702360370_1/N1702360370_1_pds3.lbl b/tests/pytests/data/N1702360370_1/N1702360370_1_pds3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..6269edb68c147d3cd45a4f2ee584c532525b4582
--- /dev/null
+++ b/tests/pytests/data/N1702360370_1/N1702360370_1_pds3.lbl
@@ -0,0 +1,120 @@
+PDS_VERSION_ID = PDS3
+
+/* FILE CHARACTERISTICS */
+
+RECORD_TYPE = FIXED_LENGTH
+RECORD_BYTES = 1048
+FILE_RECORDS = 1028
+
+/* POINTERS TO DATA OBJECTS */
+
+^IMAGE_HEADER = ("N1702360370_1.IMG",1)
+^TELEMETRY_TABLE = ("N1702360370_1.IMG",4)
+^LINE_PREFIX_TABLE = ("N1702360370_1.IMG",5)
+^IMAGE = ("N1702360370_1.IMG",5)
+
+/* IDENTIFICATION DATA ELEMENTS */
+
+ANTIBLOOMING_STATE_FLAG = "OFF"
+BIAS_STRIP_MEAN = 8.850293
+CALIBRATION_LAMP_STATE_FLAG = "N/A"
+COMMAND_FILE_NAME = "trigger_3618_1.ioi"
+COMMAND_SEQUENCE_NUMBER = 3618
+DARK_STRIP_MEAN = 0.269221
+DATA_CONVERSION_TYPE = "TABLE"
+DATA_SET_ID = "CO-S-ISSNA/ISSWA-2-EDR-V1.0"
+DELAYED_READOUT_FLAG = "NO"
+DESCRIPTION = "Incomplete product finalized due to truncated lines."
+DETECTOR_TEMPERATURE = -89.243546 <DEGC>
+EARTH_RECEIVED_START_TIME = 2011-346T22:30:08.981
+EARTH_RECEIVED_STOP_TIME = 2011-346T22:30:49.765
+ELECTRONICS_BIAS = 112
+EXPECTED_MAXIMUM = (62.996498,69.454498)
+EXPECTED_PACKETS = 576
+EXPOSURE_DURATION = 4600.000000
+FILTER_NAME = ("CL1","UV3")
+FILTER_TEMPERATURE = 0.248629
+FLIGHT_SOFTWARE_VERSION_ID = "1.4"
+GAIN_MODE_ID = "29 ELECTRONS PER DN"
+IMAGE_MID_TIME = 2011-346T05:02:22.073
+IMAGE_NUMBER = "1702360370"
+IMAGE_OBSERVATION_TYPE = {"SCIENCE"}
+IMAGE_TIME = 2011-346T05:02:24.373
+INSTRUMENT_DATA_RATE = 182.783997
+INSTRUMENT_HOST_NAME = "CASSINI ORBITER"
+INSTRUMENT_ID = "ISSNA"
+INSTRUMENT_MODE_ID = "FULL"
+INSTRUMENT_NAME = "IMAGING SCIENCE SUBSYSTEM - NARROW ANGLE"
+INST_CMPRS_PARAM = ("N/A","N/A","N/A","N/A")
+INST_CMPRS_RATE = (5.333330,3.631307)
+INST_CMPRS_RATIO = 2.203063
+INST_CMPRS_TYPE = "LOSSLESS"
+LIGHT_FLOOD_STATE_FLAG = "ON"
+METHOD_DESC = "ISSPT2.7;Enceladus;ISS_158EN_ENCEL001_PRIME"
+MISSING_LINES = 31
+MISSING_PACKET_FLAG = "NO"
+MISSION_NAME = "CASSINI-HUYGENS"
+MISSION_PHASE_NAME = "EXTENDED-EXTENDED MISSION"
+OBSERVATION_ID = "ISS_158EN_ENCEL001_PRIME"
+OPTICS_TEMPERATURE = (0.627499,1.905708)
+ORDER_NUMBER = 16
+PARALLEL_CLOCK_VOLTAGE_INDEX = 9
+PREPARE_CYCLE_INDEX = 4
+PRODUCT_CREATION_TIME = 2011-346T15:34:07.000
+PRODUCT_ID = "1_N1702360370.120"
+PRODUCT_VERSION_TYPE = "FINAL"
+READOUT_CYCLE_INDEX = 6
+RECEIVED_PACKETS = 523
+SENSOR_HEAD_ELEC_TEMPERATURE = 1.633024
+SEQUENCE_ID = "S71"
+SEQUENCE_NUMBER = 16
+SEQUENCE_TITLE = "ISS_158EN_ENCEL001_PRIME"
+SHUTTER_MODE_ID = "NACONLY"
+SHUTTER_STATE_ID = "ENABLED"
+SOFTWARE_VERSION_ID = "ISS 11.00 05-24-2006"
+SPACECRAFT_CLOCK_CNT_PARTITION = 1
+SPACECRAFT_CLOCK_START_COUNT = "1702360365.220"
+SPACECRAFT_CLOCK_STOP_COUNT = "1702360370.120"
+START_TIME = 2011-346T05:02:19.773
+STOP_TIME = 2011-346T05:02:24.373
+TARGET_DESC = "Enceladus"
+TARGET_LIST = "N/A"
+TARGET_NAME = "ENCELADUS"
+TELEMETRY_FORMAT_ID = "S&ER3"
+VALID_MAXIMUM = (4095,4095)
+OBJECT = IMAGE_HEADER
+      INTERCHANGE_FORMAT = ASCII
+      HEADER_TYPE = VICAR2
+       BYTES = 3144
+      RECORDS = 1
+      ^DESCRIPTION = "../../label/vicar2.txt"
+END_OBJECT = IMAGE_HEADER
+OBJECT = TELEMETRY_TABLE
+      INTERCHANGE_FORMAT = BINARY
+      ROWS = 1
+      COLUMNS = 2
+      ROW_BYTES = 1048
+      ^STRUCTURE = "../../label/tlmtab.fmt"
+      OBJECT = COLUMN
+            NAME = NULL_PADDING
+            DATA_TYPE = MSB_UNSIGNED_INTEGER
+            START_BYTE = 61
+            BYTES = 987
+      END_OBJECT = COLUMN
+END_OBJECT = TELEMETRY_TABLE
+OBJECT = LINE_PREFIX_TABLE
+      INTERCHANGE_FORMAT = BINARY
+      ROWS = 1024
+      COLUMNS = 7
+      ROW_BYTES = 24
+      ROW_SUFFIX_BYTES = 1024
+      ^LINE_PREFIX_STRUCTURE = "../../label/prefix3.fmt"
+END_OBJECT = LINE_PREFIX_TABLE
+OBJECT = IMAGE
+      LINES = 1024
+      LINE_SAMPLES = 1024
+      SAMPLE_BITS = 8
+      SAMPLE_TYPE = SUN_INTEGER
+      LINE_PREFIX_BYTES = 24
+END_OBJECT = IMAGE
+END
diff --git a/tests/pytests/data/N1702360370_1/cas00172.tsc b/tests/pytests/data/N1702360370_1/cas00172.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..269f1d138cc5510d75f945cc06d8c5c983c7a9e5
--- /dev/null
+++ b/tests/pytests/data/N1702360370_1/cas00172.tsc
@@ -0,0 +1,279 @@
+KPL/SCLK
+
+This file is a SPICE spacecraft clock (SCLK) kernel. This file was generated
+by the NAIF MOSPICE utility program MAKCLK, version 4.0.0, 11-MAR-2009. Please refer to the
+SCLK Required Reading file, NAIF document number 222, and the MAKCLK User's
+Guide, NAIF document number 267, for information regarding this kernel file.
+ 
+\begindata
+
+SCLK_KERNEL_ID           = ( @2018-02-15/13:19:44.80 )
+
+SCLK_DATA_TYPE_82        = ( 1 )
+SCLK01_TIME_SYSTEM_82    = ( 2 )
+SCLK01_N_FIELDS_82       = ( 2 )
+SCLK01_MODULI_82         = ( 4294967296 256 )
+SCLK01_OFFSETS_82        = ( 0 0 )
+SCLK01_OUTPUT_DELIM_82   = ( 1 )
+
+SCLK_PARTITION_START_82  = ( 1.7772134886400E+11 )
+
+SCLK_PARTITION_END_82    = ( 1.0995116277750E+12 )
+
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+    2.6607973963400E+11     4.0817564388800E+08     9.9999362662043E-01
+    2.6619183087000E+11     4.0861349748800E+08     9.9999364921016E-01
+    2.6766740670200E+11     4.1437742897600E+08     9.9999365298777E-01
+    2.6816384185800E+11     4.1631661649600E+08     9.9999364715962E-01
+    2.6967465960600E+11     4.2221821083200E+08     9.9999365001016E-01
+    2.7190971577900E+11     4.3094884356800E+08     9.9999364301114E-01
+    2.7337557583000E+11     4.3667482299200E+08     9.9999363679476E-01
+    2.7356052664400E+11     4.3739728251200E+08     9.9999364094255E-01
+    2.7593428975400E+11     4.4666973569600E+08     9.9999365751542E-01
+    2.7614202664200E+11     4.4748120276800E+08     9.9999364081238E-01
+    2.7847832758000E+11     4.5660732027200E+08     9.9999363703425E-01
+    2.8068082882900E+11     4.6521078603200E+08     9.9999363442010E-01
+    2.8176916455100E+11     4.6946207038400E+08     9.9999362305947E-01
+    2.8194487890800E+11     4.7014845021400E+08     9.9999364138973E-01
+    2.8232227206200E+11     4.7162263284800E+08     9.9999363319436E-01
+    2.8434928415300E+11     4.7954059841600E+08     9.9999363500239E-01
+    2.8649031245200E+11     4.8790393697600E+08     9.9999362794140E-01
+    2.8676600859800E+11     4.8898086818400E+08     9.9999363104202E-01
+    2.8815286654700E+11     4.9439824754400E+08     9.9999362414716E-01
+    2.8961535576000E+11     5.0011105960800E+08     9.9999361964106E-01
+    2.9063779103000E+11     5.0410492189900E+08     9.9999361088895E-01
+    2.9083443810400E+11     5.0487306962400E+08     9.9999359798729E-01
+    2.9398769644800E+11     5.1719040617400E+08     9.9999358846679E-01
+    2.9419847660800E+11     5.1801376089500E+08     9.9999360002793E-01
+    2.9620708537600E+11     5.2585983868000E+08     9.9999359397586E-01
+    2.9763242374400E+11     5.3142753101300E+08     9.9999360297215E-01
+    2.9846853203200E+11     5.3469355812000E+08     9.9999360975676E-01
+    2.9877684204800E+11     5.3589788642400E+08     9.9999359671737E-01
+    2.9893120662300E+11     5.3650086918400E+08     9.9999359770177E-01
+    2.9950603270500E+11     5.3874626919100E+08     9.9999358985534E-01
+    3.0118704188000E+11     5.4531266918900E+08     9.9999358004700E-01
+    3.0167364980400E+11     5.4721346918900E+08     9.9999358479558E-01
+    3.0304499940200E+11     5.5257026919100E+08     9.9999357800000E-01 )
+
+\begintext
+
diff --git a/tests/pytests/data/N1702360370_1/cas_iss_v10.ti b/tests/pytests/data/N1702360370_1/cas_iss_v10.ti
new file mode 100644
index 0000000000000000000000000000000000000000..102325ac12ea627e2e64fa1ac9860c43ac5ae71a
--- /dev/null
+++ b/tests/pytests/data/N1702360370_1/cas_iss_v10.ti
@@ -0,0 +1,790 @@
+KPL/IK
+ 
+ 
+ISS Instrument Kernel
+==============================================================================
+ 
+   This instrument kernel (I-kernel) contains references to the mounting
+   alignment, internal and FOV geometry for the Cassini Imaging Science
+   Subsystem (ISS) instruments.
+ 
+ 
+Version and Date
+----------------------------------------------------------
+ 
+   The TEXT_KERNEL_ID stores version information of loaded project text
+   kernels. Each entry associated with the keyword is a string that consists
+   of four parts: the kernel name, version, entry date, and type. For example,
+   the ISS I-kernel might have an entry as follows:
+ 
+           TEXT_KERNEL_ID += 'CASSINI_ISS V0.0.0 29-SEPTEMBER-1999 IK'
+                                  |          |         |            |
+                                  |          |         |            |
+              KERNEL NAME <-------+          |         |            |
+                                             |         |            V
+                             VERSION <-------+         |       KERNEL TYPE
+                                                       |
+                                                       V
+                                                  ENTRY DATE
+ 
+   ISS I-Kernel Version:
+ 
+           \begindata
+ 
+           TEXT_KERNEL_ID += 'CASSINI_ISS V1.0.0 04-NOVEMBER-2005 IK'
+ 
+           \begintext
+ 
+   Version 0.9.1 -- November 4, 2005 -- Lee Elson
+ 
+            --   Updated description of the INS[#]_FOV_CENTER_PIXEL keyword
+                 and the pixel layouts. No data are changed. See added
+                 reference No. 10.
+ 
+   Version 0.9 -- January 23, 2004 -- Josh Riley and Lee Elson
+ 
+            --   Updated focal lengths using inflight calibration results.
+ 
+   Version 0.8 -- April 23, 2001 -- Scott Turner
+ 
+            --   Updated kernel to utilize new FOV ANGLES specification.
+ 
+   Version 0.7 -- September 27, 2000 -- Scott Turner
+ 
+            --   The value of IFOV for the NAC recorded in previous kernels as
+                 60 should have been 6. The value associated with
+                 INS-82360_IFOV and the table in the documentation have been
+                 updated to reflect this correction.
+ 
+   Version 0.6 -- August 15, 2000 -- Scott Turner
+ 
+            --   Recalculated the FOV definitions to enhance precision.
+ 
+   Version 0.5 -- June 7, 2000 -- Scott Turner
+ 
+            --   Changed the INS[#]_FOV_CENTER_PIXEL keyword to reflect
+                 changes in the I-kernel SIS.
+ 
+   Version 0.4 -- March 27, 2000 -- Scott Turner
+ 
+            --   Included sample code in FORTRAN and C for computing the
+                 angular extents of the ISS fields of view.
+ 
+            --   Added the TEXT_KERNEL_ID keyword.
+ 
+            --   Minor cosmetic alterations to the structure of the kernel to
+                 improve readability.
+ 
+   Version 0.3 -- March 17, 2000 -- Scott Turner
+ 
+            --   This I-kernel reflects changes discussed at the SPICE team
+                 meeting on 3/16/2000.
+ 
+            --   All of the INS[ID]_SEQ_[WORD] keywords were eliminated.
+ 
+            --   INS[ID]_SEQ_FOV_CENTER is now keyed to
+                 INS[ID]_FOV_CENTER_PIXEL.
+ 
+   Version 0.2 -- March 6, 2000 -- Scott Turner
+ 
+            --   Fixed a few errors in the comment text describing the ISS and
+                 this kernel's intended usage.
+ 
+            --   Removed 'NAC' and 'WAC' from keywords. These values were
+                 necessary when both the NAC and WAC shared a single
+                 instrument ID code.
+ 
+            --   Added 'SEQ_' to the FOV keywords that are to be used by PDT
+                 and possibly other sequence tools.
+ 
+            --   Added name to ID code mappings for 'CASSINI_ISS_NAC' and
+                 'CASSINI_ISS_WAC'
+ 
+            --   Added the keywords 'INS-82360_SEQ_PIXEL_SIZE',
+                 'INS-82361_SEQ_PIXEL_SIZE', 'INS-82360_FOV_NAME',
+                 'INS-82361_FOV_NAME', 'INS-82360_BORESIGHT_ID',
+                 'INS-82361_BORESIGHT_ID', 'INS-82360_BORESIGHT_NAME',
+                 'INS-82361_BORESIGHT_NAME'
+ 
+   Version 0.1 -- October 8, 1999 -- Scott Turner
+ 
+            --   Added an additional set of keywords that describe the FOVs of
+                 the instruments to maintain compatibility with previously
+                 discussed standards. These keywords may change or be
+                 eliminated when the kernel evolves. Placeholders for the NAC
+                 and WAC radiators were also placed into keywords conforming
+                 to this standard.
+ 
+            --   Altered the NAC/WAC FOV definition parameters to conform with
+                 GETFOV's expectations. Added documentation describing the
+                 parameters.
+ 
+            --   Changed NAC and WAC ID codes from -82010 and -82020 to -82360
+                 and -82361 respectively.
+ 
+            --   Altered reference No. 4 to include proper document title and
+                 project document number.
+ 
+            --   Added a section for data to store instrument mode timing. The
+                 values present are just place holders until the actual ones
+                 are uncovered.
+ 
+   Version 0.0 -- June 21, 1999 -- Scott Turner
+ 
+            --   Initial Prototype Release for Review.
+ 
+ 
+References
+----------------------------------------------------------
+ 
+            1.   ``Cassini Science Instruments and Investigations'', Revised
+                 Second Printing. Stephen J. Edberg.
+ 
+            2.   Cassini Spacecraft Frames Definition Kernel.
+ 
+            3.   JPL Cassini Project Web Page describing the instruments.
+ 
+            4.   Cassini Document No. 699-416 Imaging Science Subsystem
+                 Calibration Report
+ 
+            5.   Email from Jeff Boyer regarding necessary data for footprint
+                 calculations.
+ 
+            6.   Email discussion with Vance Haemmerle regarding the location
+                 of the (0,0) pixel on the CCD and it's correlation to the NAC
+                 and WAC FOV definition.
+ 
+            7.   Cassini/NAIF SPICE Workshop, November 8-9, 1999.
+ 
+            8.   Email from Vance Haemmerle regarding an incorrect value
+                 recorded for the NAC IFOV parameter.
+ 
+            9.   Memo from P. Thomas "Geometric calibration of the ISS NAC and
+                 WAC", December 18, 2002.
+ 
+           10.   Email from Josh Riley regarding FOV_CENTER_PIXEL keyword.
+ 
+ 
+Contact Information
+----------------------------------------------------------
+ 
+   Direct questions, comments or concerns about the contents of this kernel
+   to:
+ 
+           Lee Elson, NAIF/JPL, (818)-354-4223, Lee.Elson@jpl.nasa.gov
+ 
+ 
+Implementation Notes
+----------------------------------------------------------
+ 
+   This file is used by the SPICE system as follows: programs that make use of
+   this instrument kernel must ``load'' the kernel, normally during program
+   initialization. Loading the kernel associates data items with their names
+   in a data structure called the ``kernel pool''. The SPICELIB routine FURNSH
+   and CSPICE routine furnsh_c load SPICE kernels as shown below:
+ 
+   FORTRAN (SPICELIB)
+ 
+           CALL FURNSH ( 'kernel_name' )
+ 
+   C (CSPICE)
+ 
+           furnsh_c ( "kernel_name" )
+ 
+   In order for a program or subroutine to extract data from the pool, the
+   SPICELIB routines GDPOOL and GIPOOL are used. See [2] for details.
+ 
+   This file was created and may be updated with a text editor or word
+   processor.
+ 
+ 
+Naming Conventions
+----------------------------------------------------------
+ 
+   All names referencing values in this I-kernel start with the characters
+   `INS' followed by the NAIF Cassini spacecraft ID number (-82) followed by a
+   NAIF three digit ID code for the ISS instruments. (NAC = 360, WAC = 361).
+ 
+   The remainder of the name is an underscore character followed by the unique
+   name of the data item. For example, the ISS NAC boresight direction in the
+   ISS NAC optics frame (``CASSINI_ISS_NAC'' -- see [2]) is specified by:
+ 
+           INS-82360_BORESIGHT
+ 
+   The upper bound on the length of the name of any data item is 32
+   characters.
+ 
+   If the same item is included in more than one file, or if the same item
+   appears more than once within a single file, the latest value supersedes
+   any earlier values.
+ 
+ 
+ISS description
+----------------------------------------------------------
+ 
+   From [3]:
+ 
+   ``IMAGING SCIENCE SUBSYSTEM (ISS)
+ 
+   The Cassini orbiter imaging experiments will encompass a wide variety of
+   targets (Saturn, the rings, Titan, the icy satellites, and star fields) and
+   a wide range of observing distances for various scientific purposes. The
+   science objectives include studying the atmospheres of Saturn and Titan,
+   the rings of Saturn and their interactions with the planet's satellites,
+   and the surface characteristics of the satellites, including Titan. Because
+   of these multiple objectives, the Imaging Science Subsystem (ISS) has two
+   separate camera designs. The first is a narrow-angle camera (NAC) design
+   that will obtain high-resolution images of the target of interest. The
+   second is a wide-angle camera (WAC) design that provides a different scale
+   of image resolution and more complete coverage spatially. The spacecraft
+   will carry one NAC and one WAC. The NAC is also used to obtain optical
+   navigation images for the mission with the WAC acting as a functionally
+   redundant backup unit for this purpose.
+ 
+   The cameras are charge-coupled device (CCD) imagers. A CCD is essentially a
+   large-scale integrated circuit (IC) that has a two-dimensional array of
+   hundreds or thousands of charge-isolated wells, each representing a picture
+   element or "pixel." Light falling on a well is absorbed by a
+   photoconductive substrate, such as silicon, which releases a quantity of
+   electrons proportional to the intensity of the light. The CCD detects and
+   stores an accumulated electrical charge representing the light level on
+   each well. These charges are subsequently read out for conversion to
+   digital data. CCDs are much more sensitive to light of a wider spectrum
+   than vidicon tube-type imagers, and they are less massive, require less
+   energy, and interface more easily with digital circuitry.
+ 
+   The Cassini imagers differ primarily in the design of the optics. The NAC
+   has a focal length of 2000 mm, and the WAC , which uses optics inherited
+   from the Voyager mission, has a focal length of 200 mm. The cameras each
+   have a focal plane shutter of the same type as used on both Voyager and
+   Galileo, and they have a two-wheel filter-changing mechanism derived from
+   the Hubble Space Telescope Wide Field/Planetary Camera (WF/PC) design. The
+   CCD detector is cooled to suppress dark current (residual current in the
+   CCD beyond that released by incident light), which is dependent upon
+   temperature. It is also shielded from ionizing radiation.
+ 
+   The CCD detector design is a square array of 1024x1024 pixels, each pixel
+   12 micrometers on a side. The IC chip will use three-phase,
+   front-side-illuminated architecture, with a coating of lumogen phosphor to
+   provide ultraviolet response. The detector is passively cooled by a
+   radiator to approximately 10 degrees C below its nominal operating
+   temperature (approximately minus 90 degrees C), and then it is controlled
+   to the operating temperature by a proportional control heater. To minimize
+   radiator size and heater power, the detector/radiator combination is
+   thermally isolated from the rest of the camera head assembly (CHA).
+ 
+   The entire NAC is thermally isolated from the remote sensing pallet (RSP)
+   on which it is mounted in order to minimize the effects of RSP thermal
+   variations on NAC image quality. The WAC, being an inherited design with
+   less stringent imaging requirements, is not thermally isolated.
+ 
+   The electronics for each camera are identical. All ISS command and
+   telemetry functions will be handled by the electronics, including receipt
+   of commands from the Command and Data Subsystem, expansion of commands, and
+   collection and transmission of imaging data and telemetry to the CDS.
+ 
+   The ISS controls the amount of power it draws from the spacecraft during
+   operations. To accomplish this, the profile of ISS command timing is
+   structured to reduce the power the ISS requires for certain internal
+   functions (e.g., shutter or filter wheel movement). When the filter is
+   moving, the power from the optical heater (if present) in the active camera
+   is turned off. When the movement is complete, the optical heater is turned
+   on (if needed). In addition, simultaneous filter positioning within a
+   single camera, either the WAC or NAC, is not permitted.
+ 
+   During the cruise phase of the mission, the cameras will periodically be
+   turned on for maintenance, calibration, and monitoring of instrument health
+   and performance. Other than these specified times, the ISS will be off and
+   replacement heaters will be on. In addition, decontamination/radiation
+   heater 1 will be on throughout most of the cruise.
+ 
+   Upon arrival at the Saturnian system, the cameras will be on most of the
+   time. Spacecraft power limitations will be the controlling parameter
+   determining whether the ISS will be turned off or put into a low-power
+   state. During the Saturn tour, high-activity periods for Saturn and its
+   rings will be clustered around periapsis (the point in the orbit closest to
+   the planet); for the satellites, the high-activity periods will be when the
+   spacecraft is closest to them. At these times, high-resolution images of
+   all targets will be acquired through various camera filters, and the data
+   will be stored in the spacecraft solid-state recorder (SSR). During lower
+   activity periods (i.e., when the spacecraft is orbiting farther from the
+   targets), long-term atmospheric and ring monitoring will take place, and
+   ISS calibrations will be performed.''
+ 
+ 
+ISS First Order Optical Parameters
+----------------------------------------------------------
+ 
+   The first order optical parameters for the two cameras that constitute the
+   ISS detectors:
+ 
+            --   Narrow Angle Camera
+ 
+            --   Wide Angle Camera
+ 
+   as provided by [4 and 9] for the CL filter combinations compiled into the
+   following table:
+ 
+           ------------------------------  -----------  -----------
+                     parameter                 NAC          WAC
+           ------------------------------  -----------  -----------
+            Effective Focal Length, mm        2003.44      200.77
+               Estimated Uncertainty, mm         0.03        0.01
+            Spectral Band, nm               200-1100     400-1000
+            F/number                          10.5          3.44
+           ------------------------------  -----------  -----------
+ 
+   These values are given in the keywords below in the same units as the table
+   above:
+ 
+   Narrow Angle Camera (NAC):
+ 
+           \begindata
+ 
+           INS-82360_FOCAL_LENGTH     = ( 2003.44   )
+           INS-82360_FL_UNCERTAINTY   = (    0.03   )
+           INS-82360_WAVELENGTH_RANGE = ( 200, 1100 )
+           INS-82360_F/NUMBER         = ( 10.5      )
+ 
+           \begintext
+ 
+   Wide Angle Camera (WAC):
+ 
+           \begindata
+ 
+           INS-82361_FOCAL_LENGTH     = ( 200.77    )
+           INS-82361_FL_UNCERTAINTY   = (   0.01    )
+           INS-82361_WAVELENGTH_RANGE = ( 400, 1000 )
+           INS-82361_F/NUMBER         = ( 3.44      )
+ 
+           \begintext
+ 
+ 
+ISS Field of View Parameters
+----------------------------------------------------------
+ 
+ 
+FOV Sizes (in degrees)
+ 
+                          Spacecraft Frame:
+ 
+                                             Xsc
+                                              ^
+                                              |
+                                              |
+                                              o----->
+                                           Ysc      Zsc
+ 
+ 
+                                              ^
+                        Samples               | Ycm
+              (1,1) + + + >                   |
+                +  \_____________________________________________________  ___
+                +  |                                                     |  |
+                +  |                Samples                              |  |
+                V  |      (1,1) + + + >                                  |  |
+           Lines   |        +  \_____________________________  ___       |  |
+                   |        +  |                             |  |        |  |
+                   |        +  |                             |  |        |  |
+                   |        V  |                             |  |        |  |
+                   |   Lines   |                             |  |        |  |
+                   |           |                             |  |        |  |
+              <--- |           |              x              | 0.35      | 3.4
+            Xcm    |           |                Zcm          |  |        |  |
+                   |           |                             |  |        |  |
+                   |           |                             |  |        |  |
+                   |           |                             |  |        |  |
+                   |           |_____________________________| _|_       |  |
+                   |            NAC                                      |  |
+                   |           |------------0.35-------------|           |  |
+                   |                                                     |  |
+                   |_____________________________________________________| _|_
+                    WAC
+                   |------------------------3.48-------------------------|
+ 
+ 
+   Note that although the above diagram suggests that the NAC and WAC
+   boresights are co-aligned, this is not the case. As [1] and [2] point out,
+   the NAC and WAC are both mounted to the Remote Sensing Palette in different
+   locations. From [6], the CCD samples and lines increase with decreasing X
+   and Y in the NAC and WAC frames. Thus the (1,1) corners of the CCDs are as
+   illustrated on the diagram above.
+ 
+   The FOVs of the ISS detectors have the following angular sizes (from [4]):
+ 
+           ------------  ----------------  ----------------
+             Detector       Horizontal         Vertical
+           ------------  ----------------  ----------------
+               NAC         0.35 degrees      0.35 degrees
+ 
+               WAC         3.48 degrees      3.48 degrees
+           ------------  ----------------  ----------------
+ 
+   The CCD geometry parameters as presented in [1] and [4] are provided below:
+ 
+           ------------------------------  -----------  -----------
+                     parameter                 NAC          WAC
+           ------------------------------  -----------  -----------
+            Detector Array Size             1024x1024    1024x1024
+            Pixel Size, microns               12x12        12x12
+            FOV Angular Size, degrees       0.35x0.35    3.48x3.48
+            IFOV, microradian/pixel            6            60
+           ------------------------------  -----------  -----------
+ 
+   With the keywords and their values:
+ 
+   Narrow Angle Camera (NAC):
+ 
+           \begindata
+ 
+           INS-82360_PIXEL_SAMPLES     =  (  1024  )
+           INS-82360_PIXEL_LINES       =  (  1024  )
+           INS-82360_PIXEL_SIZE        =  (   12   )
+           INS-82360_CCD_CENTER        =  (  512.5, 512.5 )
+           INS-82360_IFOV              =  (   6    )
+ 
+           \begintext
+ 
+   Wide Angle Camera (WAC):
+ 
+           \begindata
+ 
+           INS-82361_PIXEL_SAMPLES     =  (  1024  )
+           INS-82361_PIXEL_LINES       =  (  1024  )
+           INS-82361_PIXEL_SIZE        =  (   12   )
+           INS-82361_CCD_CENTER        =  (  512.5, 512.5 )
+           INS-82361_IFOV              =  (   60   )
+ 
+           \begintext
+ 
+   The keywords INS[ID]_FOV_FRAME, INS[ID]_FOV_SHAPE, INS[ID]_BORESIGHT, and
+   FOV ANGLES specification keywords defined below are used to describe the
+   instrument field of view. Since both the NAC and WAC have square fields of
+   view, the INS[ID]_FOV_SHAPE keyword will always be 'RECTANGLE', and GETFOV
+   will return the four vectors in the instrument frame that describe the
+   edges of the FOV cone. Both the NAC and WAC boresights lie along the
+   Z-axis.
+ 
+ 
+Narrow Angle Camera (NAC) FOV Definition
+ 
+   Since the NAC's angular separation is 0.35 degrees, looking up the Y-axis
+   in the CASSINI_ISS_NAC frame we have: (Note we are arbitrarily choosing
+   vectors that terminate in the Z=1 plane.)
+ 
+ 
+                                  ^ X
+                                  |  ins
+                                  |
+                                  |        /|
+                                  |      /  |
+                                  |    /    |
+                                  |  /    o |
+                                  |/ 0.175  |
+                                  o--------------->
+                                Y  \        |    Z
+                                 ins \      |     ins
+                                       \    |
+                                         \  |
+                                           \|
+ 
+                                  |-- 1.0 --|
+                                                Plane Y = 0
+ 
+ 
+   Now from here we see that the X components of the boundary corners are:
+ 
+           X Component = +/- 1.0 * tan ( 0.175 degrees ) = +/- 0.003054335689
+ 
+   Since the field of view is square this holds for the Y components as well.
+ 
+   These FOV values as well as the values from the preceding table are given
+   in the keywords below in the same units as listed above:
+ 
+   Narrow Angle Camera (NAC):
+ 
+           \begindata
+ 
+           INS-82360_FOV_FRAME                 = 'CASSINI_ISS_NAC'
+           INS-82360_FOV_SHAPE                 = 'RECTANGLE'
+           INS-82360_BORESIGHT                 = (
+ 
+                  0.0000000000000000   0.0000000000000000  +1.0000000000000000
+ 
+                     )
+           INS-82360_FOV_CLASS_SPEC            = 'ANGLES'
+           INS-82360_FOV_REF_VECTOR            = (
+ 
+                 +1.0000000000000000   0.0000000000000000   0.0000000000000000
+ 
+                     )
+           INS-82360_FOV_REF_ANGLE             = ( 0.175 )
+           INS-82360_FOV_CROSS_ANGLE           = ( 0.175 )
+           INS-82360_FOV_ANGLE_UNITS           = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Wide Angle Camera (WAC) FOV Definition
+ 
+   Since the WAC is also a square field of view, similar calculations as to
+   those made for the NAC hold. The half angle of interest is 1.74 degrees as
+   opposed to 0.175. Looking up the Y-axis in the CASSINI_ISS_WAC frame we
+   have: (Note we are arbitrarily choosing vectors that terminate in the Z=1
+   plane.)
+ 
+ 
+                                  ^ X
+                                  |  ins
+                                  |
+                                  |        /|
+                                  |      /  |
+                                  |    /    |
+                                  |  /    o |
+                                  |/ 1.740  |
+                                  o--------------->
+                                Y  \        |    Z
+                                 ins \      |     ins
+                                       \    |
+                                         \  |
+                                           \|
+ 
+                                  |-- 1.0 --|
+                                                Plane Y = 0
+ 
+ 
+   Now from here we see that the X components of the boundary corners are:
+ 
+           X Component = +/- 1.0 * tan ( 1.74 degrees ) = +/- 0.030378068382
+ 
+   Since the field of view is square this holds for the Y components as well.
+ 
+   Again since the field of view is square this computation holds for the Y
+   components as well. All of these values are collected in the FOV keywords
+   defined below. Utilizing the ANGLES FOV specification:
+ 
+   Wide Angle Camera (WAC):
+ 
+           \begindata
+ 
+           INS-82361_FOV_FRAME                 = 'CASSINI_ISS_WAC'
+           INS-82361_FOV_SHAPE                 = 'RECTANGLE'
+           INS-82361_BORESIGHT                 = (
+ 
+                  0.0000000000000000   0.0000000000000000  +1.0000000000000000
+ 
+                     )
+           INS-82361_FOV_CLASS_SPEC            = 'ANGLES'
+           INS-82361_FOV_REF_VECTOR            = (
+ 
+                 +1.0000000000000000   0.0000000000000000   0.0000000000000000
+ 
+                     )
+           INS-82361_FOV_REF_ANGLE             = ( 1.74 )
+           INS-82361_FOV_CROSS_ANGLE           = ( 1.74 )
+           INS-82361_FOV_ANGLE_UNITS           = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+ISS Radiator FOV Definitions
+ 
+   The FOV values for the ISS radiators are place holders until a time when
+   real values are provided.
+ 
+   Narrow Angle Camera Radiator (NAC_RAD):
+ 
+           \begindata
+ 
+           INS-82368_FOV_FRAME                 = 'CASSINI_ISS_NAC_RAD'
+           INS-82368_FOV_SHAPE                 = 'CIRCLE'
+           INS-82368_BORESIGHT                 = (
+ 
+                  0.0000000000000000   0.0000000000000000  +1.0000000000000000
+ 
+                                                 )
+           INS-82368_FOV_CLASS_SPEC            = 'ANGLES'
+           INS-82368_FOV_REF_VECTOR            = (
+ 
+                  0.0000000000000000  +1.0000000000000000  +0.0000000000000001
+ 
+                                                 )
+           INS-82368_FOV_REF_ANGLE             = ( 90.0 )
+           INS-82368_FOV_ANGLE_UNITS           = 'DEGREES'
+ 
+           \begintext
+ 
+   Wide Angle Camera Radiator (WAC_RAD):
+ 
+           \begindata
+ 
+           INS-82369_FOV_FRAME                 = 'CASSINI_ISS_WAC_RAD'
+           INS-82369_FOV_SHAPE                 = 'CIRCLE'
+           INS-82369_BORESIGHT                 = (
+ 
+                  0.0000000000000000   0.0000000000000000  +1.0000000000000000
+ 
+                                                 )
+           INS-82369_FOV_CLASS_SPEC            = 'ANGLES'
+           INS-82369_FOV_REF_VECTOR            = (
+ 
+                  0.0000000000000000  +1.0000000000000000  +0.0000000000000001
+ 
+                                                 )
+           INS-82369_FOV_REF_ANGLE             = ( 90.0 )
+           INS-82369_FOV_ANGLE_UNITS           = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Pixel Parameters
+----------------------------------------------------------
+ 
+   These parameters describe the pixel structure associated with the
+   instruments and their fields of views. In some cases this is a
+   generalization of the notion of pixel, in that instead of representing
+   pixels on a CCD they may represent a collection of individual detectors.
+ 
+   The FOV_CENTER_PIXEL keyword is defined differently from the CCD_CENTER in
+   the CCD geometry keywords above. Unlike the latter, which assumes pixels
+   starting at (1,1), the former assumes that the pixel numbering begins at
+   (0,0). Thus the FOV_CENTER_PIXEL is at (511.5, 511.5) instead of (512.5,
+   512.5).
+ 
+ 
+Narrow Angle Camera (NAC)
+ 
+           \begindata
+ 
+           INS-82360_FOV_CENTER_PIXEL = ( 511.5, 511.5 )
+ 
+           \begintext
+ 
+ 
+Wide Angle Camera (WAC)
+ 
+           \begindata
+ 
+           INS-82361_FOV_CENTER_PIXEL = ( 511.5, 511.5 )
+ 
+           \begintext
+ 
+ 
+Narrow Angle Camera Radiator (NAC_RAD)
+ 
+           \begindata
+ 
+           INS-82368_FOV_CENTER_PIXEL  = ( 0, 0 )
+           INS-82368_PIXEL_SAMPLES     = ( 1 )
+           INS-82368_PIXEL_LINES       = ( 1 )
+ 
+ 
+           \begintext
+ 
+ 
+Wide Angle Camera Radiator (WAC_RAD)
+ 
+           \begindata
+ 
+           INS-82369_FOV_CENTER_PIXEL  = ( 0, 0 )
+           INS-82369_PIXEL_SAMPLES     = ( 1 )
+           INS-82369_PIXEL_LINES       = ( 1 )
+ 
+           \begintext
+ 
+ 
+Instrument Mode Timing
+----------------------------------------------------------
+ 
+   The following values were provided as samples in [5]. The values are
+   defined in [5] as follows:
+ 
+ 
+           ``The initial values for the following keywords are given
+           per instrument number:
+ 
+           INS[instrument number]_[instrument acronym]_MODE_NAME
+           INS[instrument number]_[instrument acronym]_TRIGGER_OFFSET
+           INS[instrument number]_[instrument acronym]_CYCLE_DURATION
+ 
+           INS..._MODE_NAME contains the name of the instrument mode for
+           the INS..._TRIGGER_OFFSET and INS..._CYCLE_DURATION
+           keywords.
+ 
+           INS..._TRIGGER_OFFSET specifies the reference time of the
+           first instrument frame (to be calculated for a footprint)
+           relative to the time of transacting the corresponding TRIGGER
+           command. The units are SFOC duration.
+ 
+           INS..._CYCLE_DURATION specifies the duration between successive
+           instrument frames (from the first one) for the INS..._MODE_NAME.''
+ 
+ 
+ 
+NAC Mode Timing
+ 
+   The following values define the instrument modes and timing for the ISS
+   NAC.
+ 
+           \begindata
+ 
+           INS-82360_MODE_NAME      = 'NOMINAL'
+           INS-82360_TRIGGER_OFFSET = '0:01:00.0'
+           INS-82360_CYCLE_DURATION = '0:01:00.0'
+ 
+           \begintext
+ 
+ 
+WAC Mode Timing
+ 
+   The following values define the instrument modes and timing for the ISS
+   WAC.
+ 
+           \begindata
+ 
+           INS-82361_MODE_NAME      = 'NOMINAL'
+           INS-82361_TRIGGER_OFFSET = '0:01:00.0'
+           INS-82361_CYCLE_DURATION = '0:01:00.0'
+ 
+           \begintext
+ 
+ 
+NAIF ID Code to Name Mapping
+----------------------------------------------------------
+ 
+   The following keywords define names for the corresponding ID Codes. See
+   [10] for details.
+ 
+           \begindata
+ 
+           NAIF_BODY_NAME += ( 'CASSINI_ISS_NAC' )
+           NAIF_BODY_CODE += ( -82360 )
+ 
+           NAIF_BODY_NAME += ( 'CASSINI_ISS_WAC' )
+           NAIF_BODY_CODE += ( -82361 )
+ 
+           NAIF_BODY_NAME += ( 'CASSINI_ISS_NAC_RAD' )
+           NAIF_BODY_CODE += ( -82368 )
+ 
+           NAIF_BODY_NAME += ( 'CASSINI_ISS_WAC_RAD' )
+           NAIF_BODY_CODE += ( -82369 )
+ 
+           \begintext
+ 
+ 
+Platform ID
+----------------------------------------------------------
+ 
+   The ISS instrument is mounted on the Remote Sensing Palette, which is
+   connected to the Cassini Spacecraft body. Therefore the value in the
+   keywords below is -82000.
+ 
+           \begindata
+ 
+           INS-82360_PLATFORM_ID = ( -82000 )
+           INS-82361_PLATFORM_ID = ( -82000 )
+           INS-82368_PLATFORM_ID = ( -82000 )
+           INS-82369_PLATFORM_ID = ( -82000 )
+ 
+           \begintext
+ 
diff --git a/tests/pytests/data/N1702360370_1/cas_v40.tf b/tests/pytests/data/N1702360370_1/cas_v40.tf
new file mode 100644
index 0000000000000000000000000000000000000000..453be6cc351296f3c06478c90cfd3bb1cbd73dfd
--- /dev/null
+++ b/tests/pytests/data/N1702360370_1/cas_v40.tf
@@ -0,0 +1,4513 @@
+KPL/FK
+ 
+ 
+Cassini Spacecraft Frame Definitions Kernel
+==============================================================================
+ 
+   This frame kernel contains the Cassini spacecraft, science instrument, and
+   communication antennae frame definitions.
+ 
+ 
+Version and Date
+----------------------------------------------------------
+ 
+   The TEXT_KERNEL_ID stores version information of loaded project text
+   kernels. Each entry associated with the keyword is a string that consists
+   of four parts: the kernel name, version, entry date, and type. For example,
+   the ISS I-kernel might have an entry as follows:
+ 
+           TEXT_KERNEL_ID += 'CASSINI_ISS V0.0.0 29-SEPTEMBER-1999 IK'
+                                  |          |         |            |
+                                  |          |         |            |
+              KERNEL NAME <-------+          |         |            |
+                                             |         |            V
+                             VERSION <-------+         |       KERNEL TYPE
+                                                       |
+                                                       V
+                                                  ENTRY DATE
+ 
+   Cassini Frame Kernel Version:
+ 
+           \begindata
+ 
+           TEXT_KERNEL_ID += 'CASSINI_FRAMES V4.0.0 05-NOV-2008 FK'
+ 
+           \begintext
+ 
+   Version 4.0 -- November 5, 2008 -- Boris Semenov
+ 
+            --   Added CASSINI_UVIS_SOL_OFF frame, ID -82849. (See [52])
+ 
+            --   Corrected typo in WAC rotation description.
+ 
+            --   Revised the ``Implementation Notes'' section and
+                 spell-checked comments in the whole file.
+ 
+   Version 3.9 -- Oct 14, 2004 -- Lee Elson
+ 
+            --   Updated UVIS_EUV, UVIS_FUV and UVIS_HSP frames per Diane
+                 Conner's request email and SCR 524 ( A. Jouchoux, 6/7/2002:
+                 see [50]) which specifies slightly modified boresight
+                 vectors. The instrument "Y" axis has also been determined
+                 (see [51]) to point along the spacecraft -Z direction instead
+                 of + Z. Change is effective beginning at: TIME:
+                 2002-266T00:00:00.000
+ 
+   Version 3.8 -- May 10, 2004 -- Lee Elson
+ 
+            --   Updated CASSINI_XBAND per Diane Conner's request email. This
+                 was done by modifying the CASSINI_KABAND boresight vector.
+                 See [49] for details.
+ 
+   Version 3.7 -- November 20, 2003 -- Lee Elson
+ 
+            --   Updated CASSINI_XBAND per Diane Conner's request email. This
+                 was done by modifying the CASSINI_KABAND boresight vector.
+                 See [48] for details.
+ 
+   Version 3.6 -- April 18, 2003 -- Lee Elson
+ 
+            --   Modified CASSINI_XBAND frame definition so that its values
+                 are the same as CASSINI_KABAND. Added a new frame called
+                 CASSINI_XBAND_TRUE (NAIF ID -82108) that has the same
+                 definition parameters as the old CASSINI_XBAND. Also modified
+                 text structure so that changes are dated and stand out better
+                 for the human reader. See [46] and [47] for details.
+ 
+            --   Modified descriptive text structure so that changes are dated
+                 and stand out better for the human reader.
+ 
+   Version 3.5 -- September 4, 2002 -- Scott Turner, Richard West, and Rick
+   McCloskey
+ 
+            --   Entries for CASSINI_VIMS_IR_SOL, CASSINI_RADAR_2, and
+                 CASSINI_RADAR_4 were updated to reflect current values. See
+                 [42], [43], and [44] for details.
+ 
+            --   CASSINI_VIMS_IR_SOL is now referenced directly to the
+                 spacecraft frame, CASSINI_SC_COORD, rather than
+                 CASSINI_VIMS_IR.
+ 
+   Version 3.4 -- June 11, 2002 -- Scott Turner and Joshua Colwell
+ 
+            --   Entries for CASSINI_KABAND were updated per Diane Conner's
+                 request email. See [38] for details.
+ 
+            --   Updated entries for CASSINI_CIRS_FPB, CASSINI_CIRS_FP1,
+                 CASSINI_CIRS_FP3, and CASSINI_CIRS_FP4 based on updated
+                 alignment information provided in ECR 100515. See [39] for
+                 details.
+ 
+            --   Modified the entries for CASSINI_UVIS_HSP, CASSINI_UVIS_FUV,
+                 and CASSINI_UVIS_EUV to match the body vector table provided
+                 by Alain Jouchoux in May 3, 2002 e-mail. This same data set
+                 is in the CASPER UVIS definition file. Verified that CASPER
+                 and PDT give consistent results using this frame kernel.
+ 
+            --   Updated the entry for CASSINI_VIMS_IR to match the body
+                 vector table entry provided by Rick McCloskey. See [41] for
+                 details.
+ 
+   Version 3.3 -- February 20, 2002 -- Scott Turner
+ 
+            --   Updated the frame entry and documentation for
+                 CASSINI_VIMS_RAD as a result of ECR 101029 and documentation
+                 submitted with it. See [36] for details.
+ 
+   Version 3.2 -- January 22, 2002 -- Scott Turner
+ 
+            --   Updated frame entries for CASSINI_XBAND and CASSINI_KABAND as
+                 a result of SCR 490. See [35] for details.
+ 
+   Version 3.1 -- August 9, 2001 -- Scott Turner
+ 
+            --   Updated frame entries for CASSINI_XBAND and CASSINI_KABAND as
+                 a result of SCR 468. See [34] for details.
+ 
+   Version 3.0 -- April 23, 2001 -- Scott Turner
+ 
+            --   Restructured the articulating frames: CASSINI_MIMI_LEMMS1,
+                 CASSINI_MIMI_LEMMS2, CASSINI_CDA, CASSINI_CAPS. They now
+                 allow for multiple paths from the instrument frames to the
+                 spacecraft frame depending on what C-kernels are available.
+                 Use caution when loading conflicting C-kernels.
+ 
+            --   Renamed CASSINI_SRU to CASSINI_SRU-A and added CASSINI_SRU-B,
+                 CASSINI_SRU-A_RAD, and CASSINI_SRU-B_RAD.
+ 
+            --   Added the CASSINI_UVIS_SOLAR frame definition to support the
+                 UVIS solar occultation port FOV.
+ 
+            --   Removed CASSINI_UVIS_EUV_OCC and CASSINI_UVIS_FUV_OCC frame
+                 definitions since the FOVs they support are actually tied to
+                 CASSINI_UVIS_EUV and CASSINI_UVIS_FUV frames respectively.
+ 
+            --   Added the CASSINI_VIMS_IR_SOL frame definition to support the
+                 IR channel solar port FOV.
+ 
+   Version 2.9 -- November 16, 2000 -- Scott Turner
+ 
+            --   Corrected the definition of CASSINI_MIMI_INCA to account for
+                 the 9.5 degree offset from the spacecraft -Y axis.
+ 
+            --   Corrected the definition of CASSINI_INMS. The Z-axis of this
+                 frame is now co-aligned with the -X axis of CASSINI_SC_COORD.
+ 
+   Version 2.8 -- October 9, 2000 -- Scott Turner
+ 
+            --   Updated CASSINI_ISS_NAC and CASSINI_ISS_WAC to reflect the
+                 updates associated with the Fomalhaut images taken on
+                 September 18, 2000.
+ 
+            --   Migrated the CASSINI_ISS_NAC_RAD, CASSINI_ISS_WAC_RAD,
+                 CASSINI_VIMS_RAD, CASSINI_CIRS_RAD, CASSINI_CAPS,
+                 CASSINI_CDA, CASSINI_INMS, CASSINI_MAG_PLUS,
+                 CASSINI_MAG_MINUS, CASSINI_MIMI_CHEMS, CASSINI_MIMI_INCA,
+                 CASSINI_MIMI_LEMMS1, CASSINI_MIMI_LEMMS2, CASSINI_RADAR_1,
+                 CASSINI_RADAR_2, CASSINI_RADAR_3, CASSINI_RADAR_4,
+                 CASSINI_RADAR_5, CASSINI_RPWS, CASSINI_RPWS_EXPLUS,
+                 CASSINI_RPWS_EXMINUS, CASSINI_EZPLUS, CASSINI_RPWS_LP,
+                 CASSINI_KUBAND, and CASSINI_SBAND frames from the prototype
+                 section.
+ 
+            --   Updated CASSINI_XBAND and CASSINI_KABAND as the result of SCR
+                 367. These frames were migrated from the prototype section as
+                 well.
+ 
+   Version 2.7 -- July 7, 2000 -- Scott Turner
+ 
+            --   Added the following frame entries RPWS requested:
+                 CASSINI_RPWS_EXPLUS, CASSINI_RPWS_EXMINUS,
+                 CASSINI_RPWS_EZPLUS, CASSINI_RPWS_LP to the prototype frame
+                 section. See [14] for details.
+ 
+            --   Changed the following frame names: CASSINI_HGA_X ->
+                 CASSINI_XBAND, CASSINI_HGA_S -> CASSINI_SBAND, CASSINI_HGA_KA
+                 -> CASSINI_KABAND, CASSINI_HGA_KU -> CASSINI_KUBAND.
+ 
+            --   Halved the Euler angles associated with the CASSINI_CIRS_FP3
+                 and CASSINI_FP4 frames. See [15] for details.
+ 
+   Version 2.6 -- June 26, 2000 -- Scott Turner
+ 
+            --   The RSS frame entries in the prototype section were renamed
+                 to HGA based frames.
+ 
+            --   Removed the CASSINI_MAG frame and replaced it with the
+                 CASSINI_MAG_PLUS and CASSINI_MAG_MINUS frames.
+ 
+   Version 2.5 -- April 2, 2000 -- Scott Turner
+ 
+            --   Added CASSINI_VIMS.
+ 
+            --   Added CASSINI_UVIS_FUV, CASSINI_UVIS_EUV,
+                 CASSINI_UVIS_FUV_OCC, CASSINI_UVIS_EUV_OCC, CASSINI_UVIS_HSP,
+                 and CASSINI_UVIS_HDAC.
+ 
+            --   Fixed the keywords defining the CASSINI_HGA frame to use the
+                 proper ID code, -82101.
+ 
+            --   Updated CASSINI_ISS_NAC and CASSINI_ISS_WAC to reflect the
+                 latest boresight information available in ECR's 100078 and
+                 100079.
+ 
+   Version 2.4 -- March 27, 2000 -- Scott Turner
+ 
+            --   Added the CIRS Focal Plane Boresight frame, CASSINI_CIRS_FPB.
+ 
+            --   CASSINI_CIRS_FP1, CASSINI_CIRS_FP3, CASSINI_CIRS_FP2 are no
+                 longer relative to CASSINI_SC_COORD but to the intermediate
+                 frame CASSINI_CIRS_FPB.
+ 
+            --   Migrated the CASSINI_UVIS frame from the prototype section
+                 and added the CASSINI_UVIS_OCC frame.
+ 
+            --   Added the TEXT_KERNEL_ID keyword to make version information
+                 accessible to programs at runtime.
+ 
+   Version 2.3 -- March 9, 2000 -- Scott Turner
+ 
+            --   Updated the Euler angles for CASSINI_CIRS_FP1,
+                 CASSINI_CIRS_FP3, and CASSINI_CIRS_FP4. Migrated them from
+                 the prototype section into the CIRS Section of the FK.
+ 
+   Version 2.2 -- September 10, 1999 -- Scott Turner
+ 
+            --   Removed TKFRAME_[ID]_BORESIGHT keyword for all but the
+                 antenna frames present. This information can now be found in
+                 the instrument kernel with the keyword: INS[ID]_BORESIGHT.
+ 
+            --   Added a frame for the Stellar Reference Unit (SRU).
+ 
+            --   Added prototype frame entries for several instruments. The
+                 transformations stored here for these frames are NOT for any
+                 real calculations, and in some cases are not connected with
+                 the actual instrument pointing at all. These frames will
+                 migrate from the prototype section as the kernel evolves.
+ 
+            --   Changed CASSINI_SC_BUS to CASSINI_SC_COORD.
+ 
+            --   Changed the LGA frame name definitions to CASSINI_LGA1 and
+                 CASSINI_LGA2 to accommodate simple translation to flight
+                 software frame names.
+ 
+            --   Changed NAC and WAC ID codes from -82010 and -82020 to -82360
+                 and -82361 respectively. This is to conform to the new ID
+                 code scheme proposed by Jeff Boyer.
+ 
+            --   Altered the textual description of the spacecraft coordinate
+                 system to conform with [8].
+ 
+            --   Added some text from [8] to the ISS_NAC frame description.
+ 
+   Version 2.1 -- July 14, 1999 -- Scott Turner
+ 
+            --   Fixed incorrect comments regarding the NAC images.
+ 
+            --   Fixed an improperly specified transformation for LGA2.
+ 
+            --   Added TKFRAME_[ID]_BORESIGHT keyword for the frames present.
+ 
+   Version 2.0 -- May 5, 1999 -- Scott Turner
+ 
+            --   Added ISS NAC and WAC instrument frames.
+ 
+   Version 1.0 -- May 14, 1998 -- Jeff Bytof
+ 
+            --   Initial Release.
+ 
+ 
+References
+----------------------------------------------------------
+ 
+            1.   ``C-kernel Required Reading''
+ 
+            2.   ``Kernel Pool Required Reading''
+ 
+            3.   ``Frames Required Reading''
+ 
+            4.   Cassini spacecraft blueprints. Provided by Kevin Tong, JPL.
+ 
+            5.   ``Cassini Science Instruments and Investigations'', Revised
+                 Second Printing. Stephen J. Edberg.
+ 
+            6.   ``Determination of the ISS Boresights in Cassini Spacecraft
+                 Coordinate System.'' Carolyn Porco and Vance Haemmerle.
+ 
+            7.   Email from Vance Haemmerle regarding WAC alignment.
+ 
+            8.   Cassini Document No. 699-406 ``Project Guidance Analysis
+                 Book''
+ 
+            9.   CASPER CIRS I-kernel Version 3.2
+ 
+           10.   CIRS Fields-of-View PDF attached in an email from Stephen
+                 Edberg to Diane Conner.
+ 
+           11.   Cassini Engineering Change Request #100078
+ 
+           12.   Cassini Engineering Change Request #100079
+ 
+           13.   CASPER VIMS I-kernel Version Version 4.2
+ 
+           14.   Email from Terry Averkamp regarding new RPWS frame entries.
+ 
+           15.   Email from Richard Achterberg regarding the CIRS frame
+                 entries.
+ 
+           16.   Email from Vance Haemmerle regarding the Fomalhaut updates to
+                 the ISS NAC and WAC alignments.
+ 
+           17.   Email from Jeff Boyer regarding radiator boresight
+                 alignments, MIMI_CHEMS orientation, and RPWS orientation.
+ 
+           18.   Email from Sascha Kempf regarding CDA articulation.
+ 
+           19.   CASPER INMS I-kernel Version 5.0
+ 
+           20.   Email from Marcia Burton regarding the MAG field of views and
+                 frame definitions.
+ 
+           21.   CASPER MAG I-kernel Version 6.0
+ 
+           22.   CASPER MIMI I-kernel Version 4.0
+ 
+           23.   CASPER RADAR I-kernel Version 2.2
+ 
+           24.   Email from Terry Averkamp discussing the new RPWS frame
+                 entries.
+ 
+           25.   Email from Thomas Burk regarding the updates to CASSINI_XBAND
+                 and CASSINI_KABAND frames that were the result of SCR 367.
+ 
+           26.   Email from Deborah Bass regarding a correct in the
+                 CASSINI_INMS frame definition.
+ 
+           27.   Email from Donald Mitchell regarding a correction in the
+                 CASSINI_MIMI_INCA frame definition.
+ 
+           28.   Email from Rick McCloskey regarding updates and additions to
+                 the VIMS frame set.
+ 
+           29.   Email from Joshua Colwell regarding the CASSINI_UVIS_SOLAR
+                 frame definition.
+ 
+           30.   Email from Joshua Colwell verifying the CASSINI_UVIS_SOLAR
+                 frame definition.
+ 
+           31.   Email from Rick McCloskey confirming the CASSINI_VIMS_V,
+                 CASSINI_VIMS_IR, CASSINI_VIMS_IR_SOL frame definitions.
+ 
+           32.   Email from Jeff Boyer providing CASSINI_SRU_RAD frame
+                 definition.
+ 
+           33.   Email from Don Mitchell describing the CASSINI_MIMI_LEMMS1
+                 and CASSINI_MIMI_LEMMS2 articulation characteristics.
+ 
+           34.   Email from Trina Ray describing updates for the CASSINI_XBAND
+                 and CASSINI_KABAND frame definitions.
+ 
+           35.   Email from Diane Conner describing updates for the
+                 CASSINI_XBAND and CASSINI_KABAND boresights.
+ 
+           36.   Cassini ECR 101029 - Change CASSINI_VIMS_RAD frame
+                 definition.
+ 
+           37.   Cassini ECR 10325-B -- Change VIMS Sun Viewing Constraints
+                 Flight Rule FF37B2.
+ 
+           38.   Email from Diane Conner regarding CASSINI_KABAND updated
+                 boresight information.
+ 
+           39.   Page 28 from ECR 100515 listing updated alignment information
+                 for CASSINI_CIRS detectors.
+ 
+           40.   Joshua Colwell's updated version 3.3.1 Cassini Spacecraft
+                 Frame Definition kernel.
+ 
+           41.   Email from Rick McCloskey regarding the values in the body
+                 vector table for CASSINI_VIMS_IR.
+ 
+           42.   Email from Rick McCloskey regarding the Euler angles for
+                 CASSINI_VIMS_IR_SOL, the VIMS solar port.
+ 
+           43.   Email correction from Rick McCloskey regarding the Euler
+                 angles for CASSINI_VIMS_IR_SOL.
+ 
+           44.   Email from Richard West regarding the CASSINI_RADAR_2 and
+                 CASSINI_RADAR_4 Euler angles.
+ 
+           45.   Spreadsheet (gnumeric format) from Rick McCloskey regarding
+                 the Euler angles for CASSINI_VIMS_IR_SOL.
+ 
+           46.   Email from Nicole Rappaport outlining needed changes to frame
+                 and radio science instrument kernel due to project use of Ka
+                 band data for X band pointing.
+ 
+           47.   Cassini ECR number 102788 -- Additional Frame and FOV
+                 definitions to SPICE FK & IK Files for RSS
+ 
+           48.   Cassini R/SCR NO: 613 -- Update the Onboard XBAND body vector
+                 table entries for GWE#3
+ 
+           49.   C44 - New CASSINI Rev / Sequence Change Request email
+                 forwarded by Diane Conner
+ 
+           50.   Cassini R/SCR NO: 524 -- Update UVIS_EUV, UVIS_FUV and
+                 UVIS_HSP boresight vectors. ( A. Jouchoux, 6/7/2002).
+ 
+           51.   Email from Josh Colwell indicating that the UVIS instrument Y
+                 axis is co-aligned with the spacecraft -Z axis.
+ 
+           52.   Email from Diane Conner, 11/04/08, providing suggested FK and
+                 IK changes per ECR-108546 ``Add UVIS_SOL_OFF vector to SPICE
+                 Frame, Instrument, and Status Kernels''
+ 
+ 
+Contact Information
+----------------------------------------------------------
+ 
+   Direct questions, comments, or concerns about the contents of this kernel
+   to:
+ 
+           Boris Semenov, NAIF/JPL, (818)-354-8136, Boris.Semenov@jpl.nasa.gov
+ 
+ 
+Implementation Notes
+----------------------------------------------------------
+ 
+   This file is used by the SPICE system as follows: programs that make use of
+   this frame kernel must `load' the kernel, normally during program
+   initialization. The SPICELIB routine FURNSH loads a kernel file as shown
+   below:
+ 
+           FORTRAN: (SPICELIB)
+ 
+              CALL FURNSH ( frame_kernel_name )
+ 
+           C: (CSPICE)
+ 
+              furnsh_c ( frame_kernel_name );
+ 
+           IDL: (Icy)
+ 
+              cspice_furnsh, frame_kernel_name
+ 
+           MATLAB: (Mice)
+ 
+              cspice_furnsh( frame_kernel_name )
+ 
+   This file was created and may be updated with a text editor or word
+   processor.
+ 
+   Note: the keyword TKFRAME_[ID]_BORESIGHT defines the instrument or antenna
+   boresight axis in the instrument or antenna frame. In order for a program
+   or subroutine to extract data for this keyword, the SPICELIB routine GDPOOL
+   is used. See [2] for more details.
+ 
+ 
+Cassini Frames
+----------------------------------------------------------
+ 
+   The following Cassini frames are defined in this kernel file:
+ 
+           Frame Name                Relative To              Type     NAIF ID
+           =======================   ===================      =======  =======
+ 
+           AACS Body Frame:
+           ----------------
+            CASSINI_SC_COORD         J2000                    CK       -82000
+            CASSINI_SRU-A            CASSINI_SC_COORD         FIXED    -82001
+            CASSINI_SRU-B            CASSINI_SC_COORD         FIXED    -82002
+            CASSINI_SRU-A_RAD        CASSINI_SC_COORD         FIXED    -82008
+            CASSINI_SRU-B_RAD        CASSINI_SC_COORD         FIXED    -82009
+ 
+           Antenna Frames (-821xx):
+           ------------------------
+            CASSINI_HGA              CASSINI_SC_COORD         FIXED    -82101
+            CASSINI_LGA1             CASSINI_SC_COORD         FIXED    -82102
+            CASSINI_LGA2             CASSINI_SC_COORD         FIXED    -82103
+            CASSINI_XBAND            CASSINI_SC_COORD         FIXED    -82104
+            CASSINI_KABAND           CASSINI_SC_COORD         FIXED    -82105
+            CASSINI_KUBAND           CASSINI_SC_COORD         FIXED    -82106
+            CASSINI_SBAND            CASSINI_SC_COORD         FIXED    -82107
+            CASSINI_XBAND_TRUE       CASSINI_SC_COORD         FIXED    -82108
+ 
+ 
+           ISS Frames (-8236x):
+           ------------------------
+            CASSINI_ISS_NAC          CASSINI_SC_COORD         FIXED    -82360
+            CASSINI_ISS_WAC          CASSINI_SC_COORD         FIXED    -82361
+            CASSINI_ISS_NAC_RAD      CASSINI_SC_COORD         FIXED    -82368
+            CASSINI_ISS_WAC_RAD      CASSINI_SC_COORD         FIXED    -82369
+ 
+           CIRS Frames (-8289x):
+           ------------------------
+            CASSINI_CIRS_FP1         CASSINI_CIRS_FPB         FIXED    -82890
+            CASSINI_CIRS_FP3         CASSINI_CIRS_FPB         FIXED    -82891
+            CASSINI_CIRS_FP4         CASSINI_CIRS_FPB         FIXED    -82892
+            CASSINI_CIRS_FPB         CASSINI_SC_COORD         FIXED    -82893
+            CASSINI_CIRS_RAD         CASSINI_SC_COORD         FIXED    -82898
+ 
+           UVIS Frames (-8284x):
+           ------------------------
+            CASSINI_UVIS_FUV         CASSINI_SC_COORD         FIXED    -82840
+            CASSINI_UVIS_EUV         CASSINI_SC_COORD         FIXED    -82842
+            CASSINI_UVIS_SOLAR       CASSINI_SC_COORD         FIXED    -82843
+            CASSINI_UVIS_SOL_OFF     CASSINI_SC_COORD         FIXED    -82849
+            CASSINI_UVIS_HSP         CASSINI_SC_COORD         FIXED    -82844
+            CASSINI_UVIS_HDAC        CASSINI_SC_COORD         FIXED    -82845
+ 
+           VIMS Frames (-8283x):
+           ------------------------
+            CASSINI_VIMS_V           CASSINI_SC_COORD         FIXED    -82370
+            CASSINI_VIMS_IR          CASSINI_SC_COORD         FIXED    -82371
+            CASSINI_VIMS_IR_SOL      CASSINI_SC_COORD         FIXED    -82372
+            CASSINI_VIMS_RAD         CASSINI_SC_COORD         FIXED    -82378
+ 
+           CAPS Frames (-8282x):
+           ------------------------
+            CASSINI_CAPS_BASE        CASSINI_SC_COORD         FIXED    -82822
+            CASSINI_CAPS_ART         CASSINI_CAPS_BASE        CK       -82821
+            CASSINI_CAPS             CASSINI_CAPS_ART         CK       -82820
+                                     CASSINI_SC_COORD         CK       -82820
+ 
+           CDA Frames (-8279x):
+           ------------------------
+            CASSINI_CDA_BASE         CASSINI_SC_COORD         FIXED    -82792
+            CASSINI_CDA_ART          CASSINI_CDA_BASE         CK       -82971
+            CASSINI_CDA              CASSINI_CDA_ART          CK       -82790
+                                     CASSINI_SC_COORD         CK       -82790
+ 
+           INMS Frames (-8274x):
+           ------------------------
+            CASSINI_INMS             CASSINI_SC_COORD         FIXED    -82740
+ 
+           MAG Frames (-8235x):
+           ------------------------
+            CASSINI_MAG_PLUS         CASSINI_SC_COORD         FIXED    -82350
+            CASSINI_MAG_MINUS        CASSINI_SC_COORD         FIXED    -82351
+ 
+           MIMI Frames (-8276x):
+           ------------------------
+            CASSINI_MIMI_CHEMS       CASSINI_SC_COORD         FIXED    -82760
+            CASSINI_MIMI_INCA        CASSINI_SC_COORD         FIXED    -82761
+            CASSINI_MIMI_LEMMS_BASE  CASSINI_SC_COORD         FIXED    -82765
+            CASSINI_MIMI_LEMMS_ART   CASSINI_MIMI_LEMMS_BASE  CK       -82764
+            CASSINI_MIMI_LEMMS1      CASSINI_MIMI_LEMMS_ART   CK       -82762
+                                     CASSINI_SC_COORD         CK       -82762
+            CASSINI_MIMI_LEMMS2      CASSINI_MIMI_LEMMS_ART   CK       -82763
+                                     CASSINI_SC_COORD         CK       -82763
+ 
+           RADAR Frames (-8281x):
+           ------------------------
+            CASSINI_RADAR_1          CASSINI_SC_COORD         FIXED    -82810
+            CASSINI_RADAR_2          CASSINI_SC_COORD         FIXED    -82811
+            CASSINI_RADAR_3          CASSINI_SC_COORD         FIXED    -82812
+            CASSINI_RADAR_4          CASSINI_SC_COORD         FIXED    -82813
+            CASSINI_RADAR_5          CASSINI_SC_COORD         FIXED    -82814
+ 
+           RPWS Frames (-8273x):
+           ------------------------
+            CASSINI_RPWS             CASSINI_SC_COORD         FIXED    -82730
+            CASSINI_RPWS_EXPLUS      CASSINI_SC_COORD         FIXED    -82731
+            CASSINI_RPWS_EXMINUS     CASSINI_SC_COORD         FIXED    -82732
+            CASSINI_RPWS_EZPLUS      CASSINI_SC_COORD         FIXED    -82733
+            CASSINI_RPWS_LP          CASSINI_SC_COORD         FIXED    -82734
+ 
+ 
+   where: the frame ID codes are built from the spacecraft ID code, the
+   instrument subsystem number, and the instrument number in a multiple
+   instrument subsystem. The numbers 8 and 9 are reserved for the radiators.
+   For example the ISS frame IDs are constructed as follows:
+ 
+              CASSINI_ISS_WAC ID = -82 36  1
+                                    |   |  |
+                                    |   |  |
+           SPACECRAFT ID CODE <-----+   |  +----> INSTRUMENT NUMBER
+                                        |
+                                        V
+                          INSTRUMENT SUBSYSTEM NUMBER
+ 
+ 
+Cassini Frames Hierarchy
+----------------------------------------------------------
+ 
+   Notes:
+ 
+   This diagram is subject to major revisions as this kernel evolves to suit
+   the needs of each instrument.
+ 
+   The articulating instrument frames have two paths back to the spacecraft
+   frame. The first is a direct path via a single C-kernel connecting the
+   instrument frame to the spacecraft frame. The second is one that utilizes a
+   fixed offset C-kernel to rotate the instrument frame into the articulation
+   frame, and then an articulation C-kernel and a base frame. For details see
+   the sections for CASSINI_CDA, CASSINI_CAPS, and CASSINI_MIMI_LEMMS.
+ 
+   The diagram below shows the Cassini frames hierarchy:
+ 
+ 
+             'IAU_EARTH' (EARTH BODY FIXED)
+              |
+              |<--- pck
+              |
+           'J2000' INERTIAL
+              |
+              |<--- ck
+              |
+             'CASSINI_SC_COORD'
+                  |
+                 'CASSINI_SRU-A'
+                  |
+                 'CASSINI_SRU-B'
+                  |
+                 'CASSINI_SRU-A_RAD'
+                  |
+                 'CASSINI_SRU-B_RAD'
+                  |
+                 'CASSINI_HGA'
+                  |
+                 'CASSINI_XBAND'
+                  |
+                 'CASSINI_KABAND'
+                  |   |
+                  |  'CASSINI_XBAND_TRUE'
+                  |
+                 'CASSINI_KUBAND'
+                  |
+                 'CASSINI_SBAND'
+                  |
+                 'CASSINI_LGA1'
+                  |
+                 'CASSINI_LGA2'
+                  |
+                 'CASSINI_ISS_NAC'
+                  |
+                 'CASSINI_ISS_WAC'
+                  |
+                 'CASSINI_ISS_NAC_RAD'
+                  |
+                 'CASSINI_ISS_WAC_RAD'
+                  |
+                 'CASSINI_CIRS_FPB'
+                  |   |
+                  |  'CASSINI_CIRS_FP1'
+                  |   |
+                  |  'CASSINI_CIRS_FP3'
+                  |   |
+                  |  'CASSINI_CIRS_FP4'
+                  |
+                 'CASSINI_CIRS_RAD'
+                  |
+                 'CASSINI_UVIS_FUV'
+                  |
+                 'CASSINI_UVIS_EUV'
+                  |
+                 'CASSINI_UVIS_SOLAR'
+                  |
+                 'CASSINI_UVIS_SOL_OFF'
+                  |
+                 'CASSINI_UVIS_HSP'
+                  |
+                 'CASSINI_UVIS_HDAC'
+                  |
+                 'CASSINI_VIMS_V'
+                  |
+                 'CASSINI_VIMS_IR'
+                  |
+                 'CASSINI_VIMS_IR_SOL'
+                  |
+                 'CASSINI_VIMS_RAD'
+                  |
+                 'CASSINI_CAPS_BASE'
+                  |   |
+                  |   |<--- ck
+                  |   |
+                  |  'CASSINI_CAPS_ART'
+                  |       |
+                  |       |<--- ck
+                  |       |
+                  o------'CASSINI_CAPS'
+                  |  ^
+                  |  |
+                  |  + ck
+                  |
+                 'CASSINI_CDA_BASE'
+                  |   |
+                  |   |<--- ck
+                  |   |
+                  |  'CASSINI_CDA_ART'
+                  |       |
+                  |       |<--- ck
+                  |       |
+                  o------'CASSINI_CDA'
+                  |  ^
+                  |  |
+                  |  + ck
+                  |
+                 'CASSINI_INMS'
+                  |
+                 'CASSINI_MAG_PLUS'
+                  |
+                 'CASSINI_MAG_MINUS'
+                  |
+                 'CASSINI_MIMI_CHEMS'
+                  |
+                 'CASSINI_MIMI_INCA'
+                  |
+                 'CASSINI_MIMI_LEMMS_BASE'
+                  |   |
+                  |   |<--- ck
+                  |   |
+                  |  'CASSINI_MIMI_LEMMS_ART'
+                  |       |
+                  |       |<--- ck
+                  |       |
+                  o------'CASSINI_MIMI_LEMMS1'
+                  |  ^    |
+                  |  |    |
+                  |  + ck |
+                  |       |
+                  o------'CASSINI_MIMI_LEMMS2'
+                  |  ^
+                  |  |
+                  |  + ck
+                  |
+                 'CASSINI_RADAR_1'
+                  |
+                 'CASSINI_RADAR_2'
+                  |
+                 'CASSINI_RADAR_3'
+                  |
+                 'CASSINI_RADAR_4'
+                  |
+                 'CASSINI_RADAR_5'
+                  |
+                 'CASSINI_RPWS'
+                  |
+                 'CASSINI_RPWS_EXPLUS'
+                  |
+                 'CASSINI_RPWS_EXMINUS'
+                  |
+                 'CASSINI_RPWS_EZPLUS'
+                  |
+                 'CASSINI_RPWS_LP'
+ 
+ 
+ 
+ 
+Spacecraft Frame
+----------------------------------------------------------
+ 
+   From [8]: (Note: The figures referenced below can not be reproduced here.
+   There is a diagram below that basically illustrates what is contained
+   there.)
+ 
+   ``The Stellar reference Unit (SRU) detector is a CCD. Its coordinate system
+   is defined according to the geometry of the detector. Figure 2.1.2a depicts
+   the SRU orientation and coordinates relative to the S/C coordinates. From
+   the ACS point of view, the S/C coordinate system is defined with respect to
+   the SRU coordinate frame, such that :
+ 
+   +X = +b (SRU boresight)
+ 
+   +Y = +v
+ 
+   +Z = -h
+ 
+   Therefore, by definition, there are no misalignments between the SRU and
+   the S/C coordinate frames.
+ 
+   The SRU coordinate system is defined by the pixel and line shift directions
+   defined in Figure 2.1.2b. These directions are represented by unit vectors
+   h and v respectively. Both h and v pass through the origin which is located
+   at the exact center of the 1024 x 1024 array. As indicated in Figure
+   2.1.2b, the SRU boresight b passes through this point, is normal to both h
+   and v, and points outward through the optics towards the scene being
+   viewed.''
+ 
+   Stellar Reference Unit Frame:
+ 
+ 
+                                     Cassini Spacecraft
+ 
+                                            /\
+                             ----------------------------------
+                             \                                /
+                              \                              /    HGA
+                               \                            /
+               MAG Boom          --------------------------
+            ... =================|                        |
+                                 |           h            |
+                                  \          ^           /
+                                   |         |          |
+                                   |         |          |
+                       Y   <-------|   v <---o          |
+                        sc         |           b, X     |
+                                   |               sc   |
+                                   |                    |
+                                   |                    |
+                                   |                    |
+                                   |                    |
+                                   ----------------------
+                                          /      \
+                                         /        \  Main Rocket Engine
+                                         ----------
+                                             |
+                                             |
+                                             |
+                                             V
+ 
+                                             Z
+                                              sc
+ 
+           where b and X   point out of the screen or page.
+                        sc
+ 
+ 
+   From [8]:
+ 
+   ``The spacecraft basebody coordinate system is a body fixed coordinate
+   system. It is a structural coordinate system defined when the spacecraft is
+   assembled. The primary geometrical and mass properties are fixed to this
+   system. The (X,Y,Z) coordinate system is not observable in space.
+ 
+   Referring to Figure 2.1.1, the origin of the spacecraft coordinate system
+   lies at the center of the field joint between the bus and the upper
+   equipment module (UEM) upper shell structure assembly [7]. This location is
+   defined by bolt holes A, D, and H (as shown on the Configuration lay out
+   10129891, Figure 3). The Z-axis emanates from the origin and is
+   perpendicular to a plane generated by the mating surfaces of the bus at
+   bolt holes A, D, and H. The +Z-axis is on the propulsion module side of the
+   interface. The X-axis emanates from the origin and is parallel to the line
+   through the true centers of bolt holes A and H at the bus and the UEM upper
+   shell structure assembly interface. The -X-axis points towards the Huygens
+   probe. The Y-axis is mutually perpendicular to the X and Z axes, with the
+   +Y axis oriented along the magnetometer boom.''
+ 
+   Spacecraft bus attitude with respect to an inertial frame is provided by a
+   C kernel (see [1] for more information).
+ 
+           \begindata
+ 
+           FRAME_CASSINI_SC_COORD   = -82000
+           FRAME_-82000_NAME        = 'CASSINI_SC_COORD'
+           FRAME_-82000_CLASS       = 3
+           FRAME_-82000_CLASS_ID    = -82000
+           FRAME_-82000_CENTER      = -82
+           CK_-82000_SCLK           = -82
+           CK_-82000_SPK            = -82
+ 
+           \begintext
+ 
+   The nominal definition of the Stellar Reference Unit-A frame is displayed
+   below. As described above and in [8], the boresight axis lies along the
+   spacecraft +X axis. The rotation matrix that takes vectors from the SRU-A
+   frame into the spacecraft frame is computed:
+ 
+ 
+           [     ]    [     ]  [       ]  [     ]
+           [ ROT ]  = [ 0.0 ]  [ -90.0 ]  [ 0.0 ]
+           [     ]    [     ]  [       ]  [     ]
+                             Z          Y        X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_SRU-A      = -82001
+           FRAME_-82001_NAME        = 'CASSINI_SRU-A'
+           FRAME_-82001_CLASS       = 4
+           FRAME_-82001_CLASS_ID    = -82001
+           FRAME_-82001_CENTER      = -82
+           TKFRAME_-82001_SPEC      = 'ANGLES'
+           TKFRAME_-82001_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82001_ANGLES    = ( 0.0,  -90.0,  0.0 )
+           TKFRAME_-82001_AXES      = (  3,       2,    1 )
+           TKFRAME_-82001_UNITS     = 'DEGREES'
+ 
+           \begintext
+ 
+   The nominal definition of the Stellar Reference Unit-B frame is displayed
+   below. Nominally SRU-A and SRU-B are aligned, so the boresight axis lies
+   along the spacecraft +X axis. The rotation matrix that takes vectors from
+   the SRU-B frame into the spacecraft frame is computed:
+ 
+           [     ]    [     ]  [       ]  [     ]
+           [ ROT ]  = [ 0.0 ]  [ -90.0 ]  [ 0.0 ]
+           [     ]    [     ]  [       ]  [     ]
+                             Z          Y        X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+ 
+           \begindata
+ 
+           FRAME_CASSINI_SRU-B      = -82002
+           FRAME_-82002_NAME        = 'CASSINI_SRU-B'
+           FRAME_-82002_CLASS       = 4
+           FRAME_-82002_CLASS_ID    = -82002
+           FRAME_-82002_CENTER      = -82
+           TKFRAME_-82002_SPEC      = 'ANGLES'
+           TKFRAME_-82002_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82002_ANGLES    = ( 0.0,  -90.0,  0.0 )
+           TKFRAME_-82002_AXES      = (  3,       2,    1 )
+           TKFRAME_-82002_UNITS     = 'DEGREES'
+ 
+           \begintext
+ 
+   The nominal definition of the Stellar Reference Unit-A Radiator frame is
+   displayed below. As described in [32], the rotation matrix that takes
+   vectors from the SRU-A_RAD frame into the spacecraft frame is computed:
+ 
+           [     ]    [       ]  [       ]  [     ]
+           [ ROT ]  = [ 180.0 ]  [ -90.0 ]  [ 0.0 ]
+           [     ]    [       ]  [       ]  [     ]
+                               X          Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+ 
+           \begindata
+           FRAME_CASSINI_SRU-A_RAD  = -82008
+           FRAME_-82008_NAME        = 'CASSINI_SRU-A_RAD'
+           FRAME_-82008_CLASS       = 4
+           FRAME_-82008_CLASS_ID    = -82008
+           FRAME_-82008_CENTER      = -82
+           TKFRAME_-82008_SPEC      = 'ANGLES'
+           TKFRAME_-82008_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82008_ANGLES    = ( 180.0, -90.0, 0.0 )
+           TKFRAME_-82008_AXES      = (     3,     1,   3 )
+           TKFRAME_-82008_UNITS     = 'DEGREES'
+           \begintext
+ 
+   The nominal definition of the Stellar Reference Unit-B Radiator frame is
+   displayed below. As with the SRU-B frame, this is nominally the same frame
+   as SRU-A_RAD. The rotation matrix that takes vectors from the SRU-B_RAD
+   frame into the spacecraft frame is computed:
+ 
+           [     ]    [       ]  [       ]  [     ]
+           [ ROT ]  = [ 180.0 ]  [ -90.0 ]  [ 0.0 ]
+           [     ]    [       ]  [       ]  [     ]
+                               X          Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+           FRAME_CASSINI_SRU-B_RAD  = -82009
+           FRAME_-82009_NAME        = 'CASSINI_SRU-B_RAD'
+           FRAME_-82009_CLASS       = 4
+           FRAME_-82009_CLASS_ID    = -82009
+           FRAME_-82009_CENTER      = -82
+           TKFRAME_-82009_SPEC      = 'ANGLES'
+           TKFRAME_-82009_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82009_ANGLES    = ( 180.0, -90.0, 0.0 )
+           TKFRAME_-82009_AXES      = (     3,     1,   3 )
+           TKFRAME_-82009_UNITS     = 'DEGREES'
+           \begintext
+ 
+ 
+Antenna Frame Definitions
+----------------------------------------------------------
+ 
+   This section of the frames kernel defines the Cassini spacecraft antenna
+   frames. The ID codes associated with each of the frames are determined by
+   subtracting the three digit antenna code (101-103) from the DSN Cassini
+   spacecraft bus ID code (-82000).
+ 
+   Note the angles in the frame definitions are specified for the "from
+   antenna to (relative to) base frame" transformation.
+ 
+ 
+High Gain Antenna (HGA)
+ 
+   The high gain antenna points nominally along the spacecraft -Z axis. As
+   such the rotation matrix required that takes vectors represented in the
+   high gain antenna frame into the spacecraft frame is constructed as
+   follows:
+ 
+           [     ]    [     ]  [        ]  [     ]
+           [ ROT ]  = [ 0.0 ]  [ +180.0 ]  [ 0.0 ]
+           [     ]    [     ]  [        ]  [     ]
+                             Z           Y        X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_HGA        = -82101
+           FRAME_-82101_NAME        = 'CASSINI_HGA'
+           FRAME_-82101_CLASS       = 4
+           FRAME_-82101_CLASS_ID    = -82101
+           FRAME_-82101_CENTER      = -82
+           TKFRAME_-82101_SPEC      = 'ANGLES'
+           TKFRAME_-82101_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82101_ANGLES    = ( 0.0,  180.0,  0.0 )
+           TKFRAME_-82101_AXES      = (  3,      2,    1  )
+           TKFRAME_-82101_UNITS     = 'DEGREES'
+           TKFRAME_-82101_BORESIGHT = ( 0.0, 0.0, 1.0 )
+ 
+           \begintext
+ 
+   The XBAND, XBAND_TRUE, KABAND, KUBAND, and SBAND frames are all frames
+   associated with the orbiter's High Gain Antenna. These names were chosen
+   for reasons of consistency with AACS, PDT, and sequencing software.
+ 
+ 
+High Gain Antenna X Band (XBAND)
+ 
+   The high gain antenna is capable of operating in several bands, each of
+   which may be calibrated and adjusted independently. The nominal frame
+   definition for the XBAND is displayed below:
+ 
+           [     ]    [     ]  [     ]  [       ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ 180.0 ]
+           [     ]    [     ]  [     ]  [       ]
+                             Z        Y          X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           FRAME_CASSINI_XBAND       = -82104
+           FRAME_-82104_NAME         = 'CASSINI_XBAND'
+           FRAME_-82104_CLASS        = 4
+           FRAME_-82104_CLASS_ID     = -82104
+           FRAME_-82104_CENTER       = -82
+           TKFRAME_-82104_SPEC       = 'ANGLES'
+           TKFRAME_-82104_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82104_ANGLES     = (   0.0,  0.0,  180.0 )
+           TKFRAME_-82104_AXES       = (     3,    2,      1 )
+           TKFRAME_-82104_UNITS      = 'DEGREES'
+ 
+ 
+   From [25], the XBAND boresight has been adjusted to the following vector in
+   spacecraft coordinates:
+ 
+                                    [  0.0005000  ]
+           XBAND Boresight Vector = [  0.0004000  ]
+                                    [ -0.9999998  ]
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   By the methodology outlined above, this produces the following frame
+   definition:
+ 
+           [     ]    [             ]  [             ]  [     ]
+           [ ROT ]  = [ -128.659808 ]  [ -179.963313 ]  [ 0.0 ]
+           [     ]    [             ]  [             ]  [     ]
+                                     Z                X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           First Updated Frame Definition:
+ 
+           FRAME_CASSINI_XBAND       = -82104
+           FRAME_-82104_NAME         = 'CASSINI_XBAND'
+           FRAME_-82104_CLASS        = 4
+           FRAME_-82104_CLASS_ID     = -82104
+           FRAME_-82104_CENTER       = -82
+           TKFRAME_-82104_SPEC       = 'ANGLES'
+           TKFRAME_-82104_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82104_ANGLES     = (   -128.659808,  -179.963313,   0.0 )
+           TKFRAME_-82104_AXES       = (      3,            1,          3   )
+           TKFRAME_-82104_UNITS      = 'DEGREES'
+ 
+ 
+   From [34], the XBAND boresight has been adjusted again to the following
+   vector in spacecraft coordinates:
+ 
+                                    [  0.0005200  ]
+           XBAND Boresight Vector = [  0.0005800  ]
+                                    [ -0.9999997  ]
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   By the methodology outlined above, this produces the following frame
+   definition:
+ 
+           [     ]    [                  ]  [                  ]  [     ]
+           [ ROT ]  = [ -138.12213046232 ]  [ -179.95536809121 ]  [ 0.0 ]
+           [     ]    [                  ]  [                  ]  [     ]
+                                          Z                     X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+ 
+           Second Updated Frame Definition:
+ 
+           FRAME_CASSINI_XBAND       = -82104
+           FRAME_-82104_NAME         = 'CASSINI_XBAND'
+           FRAME_-82104_CLASS        = 4
+           FRAME_-82104_CLASS_ID     = -82104
+           FRAME_-82104_CENTER       = -82
+           TKFRAME_-82104_SPEC       = 'ANGLES'
+           TKFRAME_-82104_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82104_ANGLES     = ( -138.12213046232,
+                                         -179.95536809121,
+                                            0.0            )
+           TKFRAME_-82104_AXES       = (    3,
+                                            1,
+                                            3              )
+           TKFRAME_-82104_UNITS      = 'DEGREES'
+ 
+ 
+   From [35], the XBAND boresight has been adjusted to the following vector in
+   spacecraft coordinates:
+ 
+                                    [  0.0004839  ]
+           XBAND Boresight Vector = [  0.0001745  ]
+                                    [ -0.9999999  ]
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   By the methodology outlined above, this produces the following frame
+   definition:
+ 
+           [     ]    [                  ]  [                  ]  [     ]
+           [ ROT ]  = [ -109.82989689352 ]  [ -179.97052693372 ]  [ 0.0 ]
+           [     ]    [                  ]  [                  ]  [     ]
+                                          Z                     X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Third Updated Frame Definition:
+ 
+ 
+           FRAME_CASSINI_XBAND       = -82104
+           FRAME_-82104_NAME         = 'CASSINI_XBAND'
+           FRAME_-82104_CLASS        = 4
+           FRAME_-82104_CLASS_ID     = -82104
+           FRAME_-82104_CENTER       = -82
+           TKFRAME_-82104_SPEC       = 'ANGLES'
+           TKFRAME_-82104_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82104_ANGLES     = ( -109.82989689352,
+                                         -179.97052693372,
+                                            0.0            )
+           TKFRAME_-82104_AXES       = (    3,
+                                            1,
+                                            3              )
+           TKFRAME_-82104_UNITS      = 'DEGREES'
+ 
+ 
+ 
+   ______________________________________________________________
+   ++++++++++++++++++++March 18, 2003++++++++++++++++++++++++++++
+ 
+   From [46], the XBAND boresight has been adjusted so that it is co-aligned
+   with the KABAND boresight. By defining the frame relative to
+   'CASSINI_KABAND', the following frame definition is valid:
+ 
+           [     ]    [                  ]  [                  ]  [     ]
+           [ ROT ]  = [     0.0          ]  [         0.0      ]  [ 0.0 ]
+           [     ]    [                  ]  [                  ]  [     ]
+                                          Z                     X        Y
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+ 
+           \begindata
+ 
+           FRAME_CASSINI_XBAND       = -82104
+           FRAME_-82104_NAME         = 'CASSINI_XBAND'
+           FRAME_-82104_CLASS        = 4
+           FRAME_-82104_CLASS_ID     = -82104
+           FRAME_-82104_CENTER       = -82
+           TKFRAME_-82104_SPEC       = 'ANGLES'
+           TKFRAME_-82104_RELATIVE   = 'CASSINI_KABAND'
+           TKFRAME_-82104_ANGLES     = (    0.0,
+                                            0.0,
+                                            0.0            )
+           TKFRAME_-82104_AXES       = (    3,
+                                            1,
+                                            2              )
+           TKFRAME_-82104_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+High Gain Antenna X Band True (XBAND_TRUE)
+______________________________________________________________
+++++++++++++++++++++March 18, 2003++++++++++++++++++++++++++++
+ 
+   In order to preserve the original boresight information for the XBAND
+   antenna, a new frame is defined containing that information. The change
+   history is documented above under the XBAND frame.
+ 
+   From [35], the XBAND boresight has been adjusted to the following vector in
+   spacecraft coordinates:
+ 
+                                    [  0.0004839  ]
+           XBAND Boresight Vector = [  0.0001745  ]
+                                    [ -0.9999999  ]
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   By the methodology outlined above, this produces the following frame
+   definition:
+ 
+           [     ]    [                  ]  [                  ]  [     ]
+           [ ROT ]  = [ -109.82989689352 ]  [ -179.97052693372 ]  [ 0.0 ]
+           [     ]    [                  ]  [                  ]  [     ]
+                                          Z                     X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_XBAND_TRUE  = -82108
+           FRAME_-82108_NAME         = 'CASSINI_XBAND_TRUE'
+           FRAME_-82108_CLASS        = 4
+           FRAME_-82108_CLASS_ID     = -82108
+           FRAME_-82108_CENTER       = -82
+           TKFRAME_-82108_SPEC       = 'ANGLES'
+           TKFRAME_-82108_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82108_ANGLES     = ( -109.82989689352,
+                                         -179.97052693372,
+                                            0.0            )
+           TKFRAME_-82108_AXES       = (    3,
+                                            1,
+                                            3              )
+           TKFRAME_-82108_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+High Gain Antenna KA Band (KABAND)
+ 
+   The high gain antenna is capable of operating in several bands, each of
+   which may be calibrated and adjusted independently. The nominal frame
+   definition for the KABAND is displayed below:
+ 
+           [     ]    [     ]  [     ]  [       ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ 180.0 ]
+           [     ]    [     ]  [     ]  [       ]
+                             Z        Y          X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           FRAME_CASSINI_KABAND      = -82105
+           FRAME_-82105_NAME         = 'CASSINI_KABAND'
+           FRAME_-82105_CLASS        = 4
+           FRAME_-82105_CLASS_ID     = -82105
+           FRAME_-82105_CENTER       = -82
+           TKFRAME_-82105_SPEC       = 'ANGLES'
+           TKFRAME_-82105_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82105_ANGLES     = (   0.0,  0.0, 180.0 )
+           TKFRAME_-82105_AXES       = (     3,    2,     1 )
+           TKFRAME_-82105_UNITS      = 'DEGREES'
+ 
+ 
+   From [25], the KABAND boresight has been adjusted to the following vector
+   in spacecraft coordinates:
+ 
+                                     [  0.0005000  ]
+           KABAND Boresight Vector = [  0.0004000  ]
+                                     [ -0.9999998  ]
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   By the methodology outlined above, this produces the following frame
+   definition:
+ 
+           [     ]    [             ]  [             ]  [     ]
+           [ ROT ]  = [ -128.659808 ]  [ -179.963313 ]  [ 0.0 ]
+           [     ]    [             ]  [             ]  [     ]
+                                     Z                X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           First Updated Frame Definition:
+ 
+           FRAME_CASSINI_KABAND      = -82105
+           FRAME_-82105_NAME         = 'CASSINI_KABAND'
+           FRAME_-82105_CLASS        = 4
+           FRAME_-82105_CLASS_ID     = -82105
+           FRAME_-82105_CENTER       = -82
+           TKFRAME_-82105_SPEC       = 'ANGLES'
+           TKFRAME_-82105_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82105_ANGLES     = (   -128.659808,  -179.963313,   0.0 )
+           TKFRAME_-82105_AXES       = (      3,            1,          3   )
+           TKFRAME_-82105_UNITS      = 'DEGREES'
+ 
+ 
+   From [34], the KABAND boresight has been adjusted again to the following
+   vector in spacecraft coordinates:
+ 
+                                     [  0.0005300  ]
+           KABAND Boresight Vector = [  0.0006600  ]
+                                     [ -0.9999996  ]
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   By the methodology outlined above, this produces the following frame
+   definition:
+ 
+           [     ]    [                  ]  [                  ]  [     ]
+           [ ROT ]  = [ -141.23448009520 ]  [ -179.95150122158 ]  [ 0.0 ]
+           [     ]    [                  ]  [                  ]  [     ]
+                                          Z                     X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Second Updated Frame Definition:
+ 
+           FRAME_CASSINI_KABAND      = -82105
+           FRAME_-82105_NAME         = 'CASSINI_KABAND'
+           FRAME_-82105_CLASS        = 4
+           FRAME_-82105_CLASS_ID     = -82105
+           FRAME_-82105_CENTER       = -82
+           TKFRAME_-82105_SPEC       = 'ANGLES'
+           TKFRAME_-82105_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82105_ANGLES     = ( -141.23448009520,
+                                         -179.95150122158,
+                                            0.0            )
+           TKFRAME_-82105_AXES       = (    3,
+                                            1,
+                                            3              )
+           TKFRAME_-82105_UNITS      = 'DEGREES'
+ 
+ 
+   From [35], the KABAND boresight has been adjusted to the following vector
+   in spacecraft coordinates:
+ 
+                                     [  0.0004839  ]
+           KABAND Boresight Vector = [  0.0001745  ]
+                                     [ -0.9999999  ]
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   By the methodology outlined above, this produces the following frame
+   definition:
+ 
+           [     ]    [                  ]  [                  ]  [     ]
+           [ ROT ]  = [ -109.82989689352 ]  [ -179.97052693372 ]  [ 0.0 ]
+           [     ]    [                  ]  [                  ]  [     ]
+                                          Z                     X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+ 
+           FRAME_CASSINI_KABAND      = -82105
+           FRAME_-82105_NAME         = 'CASSINI_KABAND'
+           FRAME_-82105_CLASS        = 4
+           FRAME_-82105_CLASS_ID     = -82105
+           FRAME_-82105_CENTER       = -82
+           TKFRAME_-82105_SPEC       = 'ANGLES'
+           TKFRAME_-82105_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82105_ANGLES     = ( -109.82989689352,
+                                         -179.97052693372,
+                                            0.0            )
+           TKFRAME_-82105_AXES       = (    3,
+                                            1,
+                                            3              )
+           TKFRAME_-82105_UNITS      = 'DEGREES'
+ 
+ 
+   From [38], the KABAND boresight has been adjusted to the following vector
+   in spacecraft coordinates:
+ 
+                                     [  0.0005280  ]
+           KABAND Boresight Vector = [  0.0003500  ]
+                                     [ -0.9999998  ]
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   By the methodology outlined above, this produces the following frame
+   definition:
+ 
+           [     ]    [                  ]  [                  ]  [     ]
+           [ ROT ]  = [ -123.53955356526 ]  [ -179.96370485104 ]  [ 0.0 ]
+           [     ]    [                  ]  [                  ]  [     ]
+                                          Z                     X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+ 
+ 
+           FRAME_CASSINI_KABAND      = -82105
+           FRAME_-82105_NAME         = 'CASSINI_KABAND'
+           FRAME_-82105_CLASS        = 4
+           FRAME_-82105_CLASS_ID     = -82105
+           FRAME_-82105_CENTER       = -82
+           TKFRAME_-82105_SPEC       = 'ANGLES'
+           TKFRAME_-82105_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82105_ANGLES     = ( -123.53955356526,
+                                         -179.96370485104,
+                                            0.0            )
+           TKFRAME_-82105_AXES       = (    3,
+                                            1,
+                                            3              )
+           TKFRAME_-82105_UNITS      = 'DEGREES'
+ 
+ 
+   ______________________________________________________________
+   ++++++++++++++++++++November 20, 2003++++++++++++++++++++++++++++
+ 
+   From [48], the KABAND boresight has been adjusted to the following vector
+   in spacecraft coordinates:
+ 
+                                     [  0.0004273  ]
+           KABAND Boresight Vector = [  0.0008606 ]
+                                     [ -0.9999995 ]
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   By the methodology outlined above, this produces the following frame
+   definition:
+ 
+           [     ]    [                  ]  [                  ]  [     ]
+           [ ROT ]  = [ -153.59495523828 ]  [ -179.94494778906 ]  [ 0.0 ]
+           [     ]    [                  ]  [                  ]  [     ]
+                                          Z                     X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+ 
+ 
+           FRAME_CASSINI_KABAND      = -82105
+           FRAME_-82105_NAME         = 'CASSINI_KABAND'
+           FRAME_-82105_CLASS        = 4
+           FRAME_-82105_CLASS_ID     = -82105
+           FRAME_-82105_CENTER       = -82
+           TKFRAME_-82105_SPEC       = 'ANGLES'
+           TKFRAME_-82105_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82105_ANGLES     = ( -153.59495523828,
+                                         -179.94494778906,
+                                            0.0            )
+           TKFRAME_-82105_AXES       = (    3,
+                                            1,
+                                            3              )
+           TKFRAME_-82105_UNITS      = 'DEGREES'
+ 
+ 
+ 
+   ______________________________________________________________
+   ++++++++++++++++++++May 10, 2004++++++++++++++++++++++++++++
+ 
+   From [49], the KABAND boresight has been adjusted to the following vector
+   in spacecraft coordinates:
+ 
+                                     [  0.0004900 ]
+           KABAND Boresight Vector = [  0.0004500 ]
+                                     [ -0.9999998 ]
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   By the methodology outlined above, this produces the following frame
+   definition:
+ 
+           [     ]    [                  ]  [                  ]  [     ]
+           [ ROT ]  = [ -132.56335175319 ]  [ -179.96188215322 ]  [ 0.0 ]
+           [     ]    [                  ]  [                  ]  [     ]
+                                          Z                     X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_KABAND      = -82105
+           FRAME_-82105_NAME         = 'CASSINI_KABAND'
+           FRAME_-82105_CLASS        = 4
+           FRAME_-82105_CLASS_ID     = -82105
+           FRAME_-82105_CENTER       = -82
+           TKFRAME_-82105_SPEC       = 'ANGLES'
+           TKFRAME_-82105_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82105_ANGLES     = ( -132.56335175319,
+                                         -179.96188215322,
+                                            0.0            )
+           TKFRAME_-82105_AXES       = (    3,
+                                            1,
+                                            3              )
+           TKFRAME_-82105_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+High Gain Antenna KU Band (KUBAND)
+ 
+   The high gain antenna is capable of operating in several bands, each of
+   which may be calibrated and adjusted independently. The nominal frame
+   definition for the KUBAND is displayed below:
+ 
+           [     ]    [     ]  [     ]  [       ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ 180.0 ]
+           [     ]    [     ]  [     ]  [       ]
+                             Z        Y          X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_KUBAND      = -82106
+           FRAME_-82106_NAME         = 'CASSINI_KUBAND'
+           FRAME_-82106_CLASS        = 4
+           FRAME_-82106_CLASS_ID     = -82106
+           FRAME_-82106_CENTER       = -82
+           TKFRAME_-82106_SPEC       = 'ANGLES'
+           TKFRAME_-82106_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82106_ANGLES     = (   0.0,  0.0,  180.0 )
+           TKFRAME_-82106_AXES       = (     3,    2,      1 )
+           TKFRAME_-82106_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+High Gain Antenna S Band (SBAND)
+ 
+   The high gain antenna is capable of operating in several bands, each of
+   which may be calibrated and adjusted independently. The nominal frame
+   definition for the SBAND is displayed below:
+ 
+           [     ]    [     ]  [     ]  [       ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ 180.0 ]
+           [     ]    [     ]  [     ]  [       ]
+                             Z        Y          X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_SBAND       = -82107
+           FRAME_-82107_NAME         = 'CASSINI_SBAND'
+           FRAME_-82107_CLASS        = 4
+           FRAME_-82107_CLASS_ID     = -82107
+           FRAME_-82107_CENTER       = -82
+           TKFRAME_-82107_SPEC       = 'ANGLES'
+           TKFRAME_-82107_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82107_ANGLES     = (   0.0, 0.0, 180.0 )
+           TKFRAME_-82107_AXES       = (     3,   2,     1 )
+           TKFRAME_-82107_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Low Gain Antenna One (LGA1)
+ 
+   The first low gain antenna points nominally along the spacecraft -Z axis.
+   As such the rotation matrix required that takes vectors represented in the
+   first low gain antenna frame into the spacecraft frame is constructed as
+   follows:
+ 
+           [     ]    [     ]  [        ]  [     ]
+           [ ROT ]  = [ 0.0 ]  [ +180.0 ]  [ 0.0 ]
+           [     ]    [     ]  [        ]  [     ]
+                             Z           Y        X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_LGA1       = -82102
+           FRAME_-82102_NAME        = 'CASSINI_LGA1'
+           FRAME_-82102_CLASS       = 4
+           FRAME_-82102_CLASS_ID    = -82102
+           FRAME_-82102_CENTER      = -82
+           TKFRAME_-82102_SPEC      = 'ANGLES'
+           TKFRAME_-82102_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82102_ANGLES    = ( 0.0,   180.0,  0.0 )
+           TKFRAME_-82102_AXES      = (  3,      2,     1  )
+           TKFRAME_-82102_UNITS     = 'DEGREES'
+           TKFRAME_-82102_BORESIGHT = ( 0.0, 0.0, 1.0 )
+ 
+           \begintext
+ 
+ 
+Low Gain Antenna Two (LGA2)
+ 
+   The second low gain antenna points nominally along the spacecraft -X axis.
+   As such the rotation matrix required that takes vectors represented in the
+   second low gain antenna frame into the spacecraft frame is constructed as
+   follows:
+ 
+           [     ]    [     ]  [      ]  [     ]
+           [ ROT ]  = [ 0.0 ]  [ 90.0 ]  [ 0.0 ]
+           [     ]    [     ]  [      ]  [     ]
+                             Z         Y        X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_LGA2       = -82103
+           FRAME_-82103_NAME        = 'CASSINI_LGA2'
+           FRAME_-82103_CLASS       = 4
+           FRAME_-82103_CLASS_ID    = -82103
+           FRAME_-82103_CENTER      = -82
+           TKFRAME_-82103_SPEC      = 'ANGLES'
+           TKFRAME_-82103_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82103_ANGLES    = ( 0.0,     90.0,     0.0 )
+           TKFRAME_-82103_AXES      = (   3,       2,       1  )
+           TKFRAME_-82103_UNITS     = 'DEGREES'
+           TKFRAME_-82103_BORESIGHT = ( 0.0, 0.0, 1.0 )
+ 
+           \begintext
+ 
+ 
+ISS Frames
+----------------------------------------------------------
+ 
+   The Narrow Angle Camera (NAC) and Wide Angle Camera (WAC) are mounted on
+   the remote sensing pallet on the +X side of the Cassini spacecraft, and
+   nominally directed along the -Y axis of the AACS body frame.
+ 
+   Note the angles in the frame definitions are specified for the "from
+   instrument to (relative to) base frame" transformation.
+ 
+ 
+Imaging Science Subsystem Narrow Angle Camera (ISS_NAC)
+ 
+   The ISS NAC points nominally along the spacecraft -Y axis. The following
+   frame definition encapsulates this nominal frame.
+ 
+   From [8]:
+ 
+   ``The Narrow Angle Camera (NAC) detector is a CCD. Its coordinate system is
+   defined according to the geometry of the detector. The narrow angle
+   coordinate system is defined in the same manner as the SRU coordinate
+   systems defined above and the four central pixels of center of the full CCD
+   are selected for the definition of the origin of the coordinate system.
+ 
+   The Narrow Angle Camera is the primary instrument on the Remote Sensing
+   Pallet (RSP). AACS is responsible for providing pointing knowledge of the
+   boresight vector of this instrument. All other RSP instruments use the
+   pointing provided to the NAC as their reference for determining their
+   pointing.''
+ 
+           Nominal Frame Definition:
+ 
+           FRAME_CASSINI_ISS_NAC    = -82360
+           FRAME_-82360_NAME        = 'CASSINI_ISS_NAC'
+           FRAME_-82360_CLASS       = 4
+           FRAME_-82360_CLASS_ID    = -82360
+           FRAME_-82360_CENTER      = -82
+           TKFRAME_-82360_SPEC      = 'ANGLES'
+           TKFRAME_-82360_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82360_ANGLES    = (   -90.0,     0.0,     90.0 )
+           TKFRAME_-82360_AXES      = (     1,       2,        3   )
+           TKFRAME_-82360_UNITS     = 'DEGREES'
+ 
+ 
+   [6] describes the inflight calibration of the ISS that was the result of
+   the CICLOPS (Cassini Imaging Central Laboratory for Operations) analysis of
+   8 NAC images that were taken during ICO (Instrument Checkout). The rotation
+   matrix that takes vectors represented in the ISS_NAC frame into the
+   spacecraft frame follows:
+ 
+           [     ]    [            ]  [              ]  [           ]
+           [ ROT ]  = [ -90.024236 ]  [ -0.047029483 ]  [ 89.892082 ]
+           [     ]    [            ]  [              ]  [           ]
+                                    X                 Y              Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   The angles were taken directly from [6].
+ 
+ 
+           FRAME_CASSINI_ISS_NAC    = -82360
+           FRAME_-82360_NAME        = 'CASSINI_ISS_NAC'
+           FRAME_-82360_CLASS       = 4
+           FRAME_-82360_CLASS_ID    = -82360
+           FRAME_-82360_CENTER      = -82
+           TKFRAME_-82360_SPEC      = 'ANGLES'
+           TKFRAME_-82360_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82360_ANGLES    = ( -90.024236, -0.047029483,  89.892082 )
+           TKFRAME_-82360_AXES      = (   1,         2,             3        )
+           TKFRAME_-82360_UNITS     = 'DEGREES'
+ 
+ 
+   From [10]:
+ 
+   ``The NAC boresight is not precisely aligned with the S/C -Y body vector.
+   Its alignment was determined during ICO-1 ISS observations of Spica, when
+   the spacecraft was using SRU-B for orientation determination. The alignment
+   parameters cited under Change Requested take into account the offset, as
+   determined by AACS, between SRU-A and SRU-B.''
+ 
+   [10] also describes a series of frame transformations that convert the
+   CASSINI_ISS_NAC frame into the CASSINI_SC_COORD frame, accounting for the
+   offset between SRU-A and SRU-B. This results in following frame definition:
+ 
+   The rotation matrix that takes vectors represented in the ISS_NAC frame
+   into the spacecraft frame follows:
+ 
+           [     ]    [              ]  [             ]  [             ]
+           [ ROT ]  = [ -89.99231636 ]  [ -0.03586589 ]  [ 89.93339682 ]
+           [     ]    [              ]  [             ]  [             ]
+                                      X                Y                Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+ 
+           FRAME_CASSINI_ISS_NAC    = -82360
+           FRAME_-82360_NAME        = 'CASSINI_ISS_NAC'
+           FRAME_-82360_CLASS       = 4
+           FRAME_-82360_CLASS_ID    = -82360
+           FRAME_-82360_CENTER      = -82
+           TKFRAME_-82360_SPEC      = 'ANGLES'
+           TKFRAME_-82360_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82360_ANGLES    = (-89.99231636, -0.03586589, 89.93339682)
+           TKFRAME_-82360_AXES      = (  1,           2,           3         )
+           TKFRAME_-82360_UNITS     = 'DEGREES'
+ 
+ 
+   From [16]:
+ 
+   ``The following results were obtained by using 3 long exposure Fomalhaut
+   NAC frames, each with 6 stars and using a 3 parameter fit (shift in line,
+   shift in sample and rotation about optic axis).''
+ 
+              AACS       NAC boresight
+ 
+               X         0.0005760  +/- 0.0000018
+               Y        -0.99999982 +/- 0.00000001
+               Z        -0.0001710  +/- 0.0000016
+ 
+   The results of the Fomalhaut image calibrations produced the following
+   update to the ISS_NAC frame definition:
+ 
+   The rotation matrix that takes vectors represented in the ISS_NAC frame
+   into the spacecraft frame follows:
+ 
+           [     ]    [            ]  [          ]  [         ]
+           [ ROT ]  = [ -90.009796 ]  [ -0.03300 ]  [ 89.9148 ]
+           [     ]    [            ]  [          ]  [         ]
+                                    X             Y            Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_ISS_NAC    = -82360
+           FRAME_-82360_NAME        = 'CASSINI_ISS_NAC'
+           FRAME_-82360_CLASS       = 4
+           FRAME_-82360_CLASS_ID    = -82360
+           FRAME_-82360_CENTER      = -82
+           TKFRAME_-82360_SPEC      = 'ANGLES'
+           TKFRAME_-82360_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82360_ANGLES    = (-90.009796, -0.03300, 89.9148 )
+           TKFRAME_-82360_AXES      = (  1,         2,        3      )
+           TKFRAME_-82360_UNITS     = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Imaging Science Subsystem Wide Angle Camera (ISS_WAC)
+ 
+   The ISS WAC points nominally along the spacecraft -Y axis. The following
+   frame definition encapsulates this nominal frame.
+ 
+           Nominal Frame Definition:
+ 
+           FRAME_CASSINI_ISS_WAC    = -82361
+           FRAME_-82361_NAME        = 'CASSINI_ISS_WAC'
+           FRAME_-82361_CLASS       = 4
+           FRAME_-82361_CLASS_ID    = -82361
+           FRAME_-82361_CENTER      = -82
+           TKFRAME_-82361_SPEC      = 'ANGLES'
+           TKFRAME_-82361_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82361_ANGLES    = (   -90.0,     0.0,     90.0 )
+           TKFRAME_-82361_AXES      = (     1,       2,        3   )
+           TKFRAME_-82361_UNITS     = 'DEGREES'
+ 
+ 
+   [6] describes the inflight calibration of ISS that was the result of the
+   CICLOPS (Cassini Imaging Central Laboratory for Operations) analysis of 36
+   WAC images taken during ICO (Instrument Checkout). At this time the images
+   taken were only sufficient to develop the location of the WAC's optical
+   axis. There are three determinations of this axes location in the
+   spacecraft frame. In [7] V.Haemmerle suggests that the 2-parameter fit
+   average coupled with nominal twist would be the safest assumption to
+   determine the frame transformation from ISS_WAC to the AACS body frame. The
+   rotation matrix that takes ISS_WAC vectors into the spacecraft frame would
+   be constructed as follows:
+ 
+           [     ]    [             ]  [              ]  [     ]
+           [ ROT ]  = [ +89.9116120 ]  [ -90.00059931 ]  [ 0.0 ]
+           [     ]    [             ]  [              ]  [     ]
+                                     Z                 Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   These angles were computed using the assumption that the WAC optical axis
+   lies along the vector:
+ 
+                                     [  0.00154266 ]
+           WAC Optical Axis Vector = [ -0.99999881 ]
+                                     [ -0.00001046 ]
+ 
+   in AACS body coordinates. Further we assume nominal twist, hence the first
+   rotation about Z is 0.0 degrees.
+ 
+ 
+           FRAME_CASSINI_ISS_WAC    = -82361
+           FRAME_-82361_NAME        = 'CASSINI_ISS_WAC'
+           FRAME_-82361_CLASS       = 4
+           FRAME_-82361_CLASS_ID    = -82361
+           FRAME_-82361_CENTER      = -82
+           TKFRAME_-82361_SPEC      = 'ANGLES'
+           TKFRAME_-82361_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82361_ANGLES    = (   89.9116120,  -90.00059931,  0.0 )
+           TKFRAME_-82361_AXES      = (            3,             2,    3 )
+           TKFRAME_-82361_UNITS     = 'DEGREES'
+ 
+ 
+   From [11]:
+ 
+   ``The WAC boresight is not precisely aligned with the S/C -Y body vector.
+   Its alignment was determined during ICO-1 ISS observations of Spica, when
+   the spacecraft was using SRU-B for orientation determination. The alignment
+   parameters cited under Change Request take into account the offset, as
+   determined by AACS, between SRU-A and SRU-B.''
+ 
+   Taking the boresight from the ECR ([11]):
+ 
+                                     [  0.0013481161  ]
+           WAC Optical Axis Vector = [ -0.99999894    ]
+                                     [  0.00054612156 ]
+ 
+   and assuming no twist, we derive the following angles:
+ 
+           [     ]    [             ]  [              ]  [     ]
+           [ ROT ]  = [ +89.9227586 ]  [ -89.96870954 ]  [ 0.0 ]
+           [     ]    [             ]  [              ]  [     ]
+                                     Z                 Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   These angles were computed using the assumption that the WAC optical axis
+   lies along the vector listed above. Further we assume nominal twist, hence
+   the first rotation about Z is 0.0 degrees.
+ 
+ 
+           FRAME_CASSINI_ISS_WAC    = -82361
+           FRAME_-82361_NAME        = 'CASSINI_ISS_WAC'
+           FRAME_-82361_CLASS       = 4
+           FRAME_-82361_CLASS_ID    = -82361
+           FRAME_-82361_CENTER      = -82
+           TKFRAME_-82361_SPEC      = 'ANGLES'
+           TKFRAME_-82361_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82361_ANGLES    = (   89.9227586,  -89.96870954,  0.0 )
+           TKFRAME_-82361_AXES      = (            3,             2,    3 )
+           TKFRAME_-82361_UNITS     = 'DEGREES'
+ 
+ 
+   From [16]:
+ 
+   ``The following results were obtained by using 3 long exposure Fomalhaut
+   WAC frames, each using 12 stars near the center of frame and using a 3
+   parameter fit (shift in line, shift in sample and rotation about optic
+   axis).''
+ 
+              AACS       WAC boresight
+ 
+               X         0.00121834 +/- 0.00000078
+               Y        -0.99999923 +/- 0.00000001
+               Z         0.00025445 +/- 0.00000094
+ 
+   The results of the Fomalhaut image calibrations produced the following
+   update to the ISS_WAC frame definition:
+ 
+   The rotation matrix that takes vectors represented in the ISS_WAC frame
+   into the spacecraft frame follows:
+ 
+           [     ]    [            ]  [           ]  [         ]
+           [ ROT ]  = [ -89.985421 ]  [ -0.069806 ]  [ 89.9736 ]
+           [     ]    [            ]  [           ]  [         ]
+                                    X              Y            Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_ISS_WAC    = -82361
+           FRAME_-82361_NAME        = 'CASSINI_ISS_WAC'
+           FRAME_-82361_CLASS       = 4
+           FRAME_-82361_CLASS_ID    = -82361
+           FRAME_-82361_CENTER      = -82
+           TKFRAME_-82361_SPEC      = 'ANGLES'
+           TKFRAME_-82361_RELATIVE  = 'CASSINI_SC_COORD'
+           TKFRAME_-82361_ANGLES    = ( -89.985421,  -0.069806,  89.9736 )
+           TKFRAME_-82361_AXES      = (   1,          2,          3      )
+           TKFRAME_-82361_UNITS     = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+ISS Radiators (ISS_NAC_RAD and ISS_WAC_RAD)
+ 
+   The ISS radiators are nominally oriented with their +Z axes directed down
+   the spacecraft +X axis.
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   As [17] indicates, both the ISS_NAC_RAD and ISS_WAC_RAD boresights are
+   nominally aligned with the +X axis in the spacecraft frame. By the
+   methodology outlined above, this produces the following frame definitions:
+ 
+           [     ]    [       ]  [       ]  [     ]
+           [ ROT ]  = [ -90.0 ]  [ -90.0 ]  [ 0.0 ]
+           [     ]    [       ]  [       ]  [     ]
+                               Z          X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_ISS_NAC_RAD = -82368
+           FRAME_-82368_NAME         = 'CASSINI_ISS_NAC_RAD'
+           FRAME_-82368_CLASS        = 4
+           FRAME_-82368_CLASS_ID     = -82368
+           FRAME_-82368_CENTER       = -82
+           TKFRAME_-82368_SPEC       = 'ANGLES'
+           TKFRAME_-82368_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82368_ANGLES     = ( -90.0,   -90.0,     0.0 )
+           TKFRAME_-82368_AXES       = (     3,       1,       3 )
+           TKFRAME_-82368_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+   Since the boresights are the same, both frame definitions are also the
+   same, thus we have:
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_ISS_WAC_RAD = -82369
+           FRAME_-82369_NAME         = 'CASSINI_ISS_WAC_RAD'
+           FRAME_-82369_CLASS        = 4
+           FRAME_-82369_CLASS_ID     = -82369
+           FRAME_-82369_CENTER       = -82
+           TKFRAME_-82369_SPEC       = 'ANGLES'
+           TKFRAME_-82369_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82369_ANGLES     = ( -90.0,   -90.0,     0.0 )
+           TKFRAME_-82369_AXES       = (     3,       1,       3 )
+           TKFRAME_-82369_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+CIRS Frames
+----------------------------------------------------------
+ 
+   The Composite Infrared Spectrometer (CIRS) is mounted on the remote sensing
+   pallet on the +X side of the Cassini spacecraft, and nominally directed
+   along the -Y axis of the AACS body frame.
+ 
+   Note the angles in the frame definitions are specified for the "from
+   instrument to (relative to) base frame" transformation.
+ 
+ 
+Composite Infrared Spectrometer Focal Plane Boresight (CIRS_FPB)
+ 
+   The CIRS FPB points nominally along the spacecraft -Y axis. The rotation
+   matrix that takes vectors represented in the CIRS_FPB frame into the
+   spacecraft frame follows:
+ 
+           [     ]    [     ]  [      ]  [     ]
+           [ ROT ]  = [ 0.0 ]  [-90.0 ]  [ 0.0 ]
+           [     ]    [     ]  [      ]  [     ]
+                             Z         X        Y
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   The following frame definition encapsulates this nominal frame:
+ 
+           Nominal Frame Definition
+ 
+           FRAME_CASSINI_CIRS_FPB    = -82893
+           FRAME_-82893_NAME         = 'CASSINI_CIRS_FPB'
+           FRAME_-82893_CLASS        = 4
+           FRAME_-82893_CLASS_ID     = -82893
+           FRAME_-82893_CENTER       = -82
+           TKFRAME_-82893_SPEC       = 'ANGLES'
+           TKFRAME_-82893_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82893_ANGLES     = (  0.0,    -90.0,    0.0 )
+           TKFRAME_-82893_AXES       = (    3,        1,      2 )
+           TKFRAME_-82893_UNITS      = 'DEGREES'
+ 
+ 
+   ECR 100515 [39] included mounting alignment updates for all CIRS focal
+   planes. The optical boresight has moved from it's nominal configuration of
+   the -Y axis in the spacecraft frame 1.7 milliradians towards +X and -0.04
+   milliradians towards -Z. The rotation matrix that takes vectors represented
+   in the CIRS_FPB frame into the spacecraft frame follows:
+ 
+           [     ]    [     ]  [                  ]  [                ]
+           [ ROT ]  = [ 0.0 ]  [ -90.002291831180 ]  [ -0.09740282517 ]
+           [     ]    [     ]  [                  ]  [                ]
+                             Z                     X                   Y
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_CIRS_FPB    = -82893
+           FRAME_-82893_NAME         = 'CASSINI_CIRS_FPB'
+           FRAME_-82893_CLASS        = 4
+           FRAME_-82893_CLASS_ID     = -82893
+           FRAME_-82893_CENTER       = -82
+           TKFRAME_-82893_SPEC       = 'ANGLES'
+           TKFRAME_-82893_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82893_ANGLES     = (
+                                          0.0
+                                        -90.0022918311805233
+                                         -0.097402825172240,
+                                       )
+           TKFRAME_-82893_AXES       = (  3,  1,  2 )
+ 
+           TKFRAME_-82893_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Composite Infrared Spectrometer Focal Plane #1 (CIRS_FP1)
+ 
+   The CIRS FP1 points nominally along the spacecraft -Y axis. The following
+   frame definition encapsulates this nominal frame.
+ 
+           Nominal Frame Definition:
+ 
+           FRAME_CASSINI_CIRS_FP1    = -82890
+           FRAME_-82890_NAME         = 'CASSINI_CIRS_FP1'
+           FRAME_-82890_CLASS        = 4
+           FRAME_-82890_CLASS_ID     = -82890
+           FRAME_-82890_CENTER       = -82
+           TKFRAME_-82890_SPEC       = 'ANGLES'
+           TKFRAME_-82890_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82890_ANGLES     = (  -90.0,     0.0,    90.0 )
+           TKFRAME_-82890_AXES       = (      1,       2,       3 )
+           TKFRAME_-82890_UNITS      = 'DEGREES'
+ 
+ 
+   [9] and [10] describe the most up to date values the orientation of the
+   CIRS focal planes. The rotation matrix that takes vectors represented in
+   the CIRS_FP1 frame into the CIRS_FPB frame follows:
+ 
+           [     ]    [     ]  [     ]  [            ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ 0.23319382 ]
+           [     ]    [     ]  [     ]  [            ]
+                             Z        X               Y
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   The angles were computed from [10].
+ 
+ 
+           FRAME_CASSINI_CIRS_FP1    = -82890
+           FRAME_-82890_NAME         = 'CASSINI_CIRS_FP1'
+           FRAME_-82890_CLASS        = 4
+           FRAME_-82890_CLASS_ID     = -82890
+           FRAME_-82890_CENTER       = -82
+           TKFRAME_-82890_SPEC       = 'ANGLES'
+           TKFRAME_-82890_RELATIVE   = 'CASSINI_CIRS_FPB'
+           TKFRAME_-82890_ANGLES     = (  0.0,     0.0,   -0.23319382 )
+           TKFRAME_-82890_AXES       = (    3,       1,             2 )
+           TKFRAME_-82890_UNITS      = 'DEGREES'
+ 
+ 
+   [39] introduces new offsets for the FP1 from the optical boresight (FPB).
+   They are: 3.98 milliradians towards +X in the spacecraft frame and 0.07
+   milliradians towards +Z in the spacecraft frame. These offsets result in
+   the following rotation matrix:
+ 
+           [     ]    [     ]  [                 ]  [                ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0040107045659 ]  [ -0.22803720246 ]
+           [     ]    [     ]  [                 ]  [                ]
+                             Z                    X                   Y
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_CIRS_FP1    = -82890
+           FRAME_-82890_NAME         = 'CASSINI_CIRS_FP1'
+           FRAME_-82890_CLASS        = 4
+           FRAME_-82890_CLASS_ID     = -82890
+           FRAME_-82890_CENTER       = -82
+           TKFRAME_-82890_SPEC       = 'ANGLES'
+           TKFRAME_-82890_RELATIVE   = 'CASSINI_CIRS_FPB'
+           TKFRAME_-82890_ANGLES     = (
+                                          0.0,
+                                          4.0107045659158E-03,
+                                         -2.2803720246207E-01
+                                       )
+           TKFRAME_-82890_AXES       = (  3,  1,  2 )
+           TKFRAME_-82890_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Composite Infrared Spectrometer Focal Plane #3 (CIRS_FP3)
+ 
+   The CIRS FP3 points nominally along the spacecraft -Y axis. The following
+   frame definition encapsulates this nominal frame.
+ 
+           Nominal Frame Definition:
+ 
+           FRAME_CASSINI_CIRS_FP3    = -82891
+           FRAME_-82891_NAME         = 'CASSINI_CIRS_FP3'
+           FRAME_-82891_CLASS        = 4
+           FRAME_-82891_CLASS_ID     = -82891
+           FRAME_-82891_CENTER       = -82
+           TKFRAME_-82891_SPEC       = 'ANGLES'
+           TKFRAME_-82891_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82891_ANGLES     = (  -90.0,     0.0,    90.0 )
+           TKFRAME_-82891_AXES       = (      1,       2,       3 )
+           TKFRAME_-82891_UNITS      = 'DEGREES'
+ 
+ 
+   [9] and [10] describe the most up to date values the orientation of the
+   CIRS focal planes. The rotation matrix that takes vectors represented in
+   the CIRS_FP3 frame into the CIRS_FPB frame follows:
+ 
+           [     ]    [     ]  [     ]  [             ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ 0.002549662 ]
+           [     ]    [     ]  [     ]  [             ]
+                             Z        X                Y
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   The angles were computed from [10] with updates from [15].
+ 
+ 
+           FRAME_CASSINI_CIRS_FP3    = -82891
+           FRAME_-82891_NAME         = 'CASSINI_CIRS_FP3'
+           FRAME_-82891_CLASS        = 4
+           FRAME_-82891_CLASS_ID     = -82891
+           FRAME_-82891_CENTER       = -82
+           TKFRAME_-82891_SPEC       = 'ANGLES'
+           TKFRAME_-82891_RELATIVE   = 'CASSINI_CIRS_FPB'
+           TKFRAME_-82891_ANGLES     = ( 0.0,     0.0,   0.02549662 )
+           TKFRAME_-82891_AXES       = (   3,       1,            2 )
+           TKFRAME_-82891_UNITS      = 'DEGREES'
+ 
+ 
+   [39] includes an update to the offset of CASSINI_CIRS_FP3 from
+   CASSINI_CIRS_FPB. Instead of 0.445 milliradians, the new value is 0.47
+   milliradians of separation between the optical boresight and focal plane
+   3's boresight. The rotation matrix that takes vectors represented in the
+   CIRS_FP3 frame into the CIRS_FPB frame follows:
+ 
+           [     ]    [     ]  [     ]  [             ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ 0.002692902 ]
+           [     ]    [     ]  [     ]  [             ]
+                             Z        X                Y
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_CIRS_FP3    = -82891
+           FRAME_-82891_NAME         = 'CASSINI_CIRS_FP3'
+           FRAME_-82891_CLASS        = 4
+           FRAME_-82891_CLASS_ID     = -82891
+           FRAME_-82891_CENTER       = -82
+           TKFRAME_-82891_SPEC       = 'ANGLES'
+           TKFRAME_-82891_RELATIVE   = 'CASSINI_CIRS_FPB'
+           TKFRAME_-82891_ANGLES     = ( 0.0,  0.0,  2.6929016371149E-02 )
+           TKFRAME_-82891_AXES       = (   3,    1,                    2 )
+           TKFRAME_-82891_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Composite Infrared Spectrometer Focal Plane #4 (CIRS_FP4)
+ 
+   The CIRS FP4 points nominally along the spacecraft -Y axis. The following
+   frame definition encapsulates this nominal frame.
+ 
+           Nominal Frame Definition:
+ 
+           FRAME_CASSINI_CIRS_FP4    = -82892
+           FRAME_-82892_NAME         = 'CASSINI_CIRS_FP4'
+           FRAME_-82892_CLASS        = 4
+           FRAME_-82892_CLASS_ID     = -82892
+           FRAME_-82892_CENTER       = -82
+           TKFRAME_-82892_SPEC       = 'ANGLES'
+           TKFRAME_-82892_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82892_ANGLES     = (  -90.0,     0.0,    90.0 )
+           TKFRAME_-82892_AXES       = (      1,       2,       3 )
+           TKFRAME_-82892_UNITS      = 'DEGREES'
+ 
+ 
+   [9] and [10] describe the most up to date values the orientation of the
+   CIRS focal planes. The rotation matrix that takes vectors represented in
+   the CIRS_FP4 frame into the CIRS_FPB frame follows:
+ 
+           [     ]    [     ]  [     ]  [             ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ -0.02549662 ]
+           [     ]    [     ]  [     ]  [             ]
+                             Z        X                Y
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   The angles were taken directly from [10] with updates from [15].
+ 
+ 
+           FRAME_CASSINI_CIRS_FP4    = -82892
+           FRAME_-82892_NAME         = 'CASSINI_CIRS_FP4'
+           FRAME_-82892_CLASS        = 4
+           FRAME_-82892_CLASS_ID     = -82892
+           FRAME_-82892_CENTER       = -82
+           TKFRAME_-82892_SPEC       = 'ANGLES'
+           TKFRAME_-82892_RELATIVE   = 'CASSINI_CIRS_FPB'
+           TKFRAME_-82892_ANGLES     = ( 0.0,     0.0,   -0.02549662 )
+           TKFRAME_-82892_AXES       = (   3,       1,             2 )
+           TKFRAME_-82892_UNITS      = 'DEGREES'
+ 
+ 
+   [39] includes an update to the offset of CASSINI_CIRS_FP4 from
+   CASSINI_CIRS_FPB. Instead of 0.445 milliradians, the new value is 0.47
+   milliradians of separation between the optical boresight and focal plane
+   4's boresight. The rotation matrix that takes vectors represented in the
+   CIRS_FP4 frame into the CIRS_FPB frame follows:
+ 
+           [     ]    [     ]  [     ]  [              ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ -0.002692902 ]
+           [     ]    [     ]  [     ]  [              ]
+                             Z        X                 Y
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_CIRS_FP4    = -82892
+           FRAME_-82892_NAME         = 'CASSINI_CIRS_FP4'
+           FRAME_-82892_CLASS        = 4
+           FRAME_-82892_CLASS_ID     = -82892
+           FRAME_-82892_CENTER       = -82
+           TKFRAME_-82892_SPEC       = 'ANGLES'
+           TKFRAME_-82892_RELATIVE   = 'CASSINI_CIRS_FPB'
+           TKFRAME_-82892_ANGLES     = ( 0.0,  0.0,  -2.6929016371149E-02 )
+           TKFRAME_-82892_AXES       = (   3,    1,                     2 )
+           TKFRAME_-82892_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+CIRS Radiator (CIRS_RAD)
+ 
+   The CIRS radiator is nominally oriented with its +Z axis directed down the
+   spacecraft +X axis.
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   As [17] indicates, the CIRS_RAD boresight is nominally aligned with the +X
+   axis in the spacecraft frame. By the methodology outlined above, this
+   produces the following frame definition:
+ 
+           [     ]    [       ]  [       ]  [     ]
+           [ ROT ]  = [ -90.0 ]  [ -90.0 ]  [ 0.0 ]
+           [     ]    [       ]  [       ]  [     ]
+                               Z          X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_CIRS_RAD    = -82898
+           FRAME_-82898_NAME         = 'CASSINI_CIRS_RAD'
+           FRAME_-82898_CLASS        = 4
+           FRAME_-82898_CLASS_ID     = -82898
+           FRAME_-82898_CENTER       = -82
+           TKFRAME_-82898_SPEC       = 'ANGLES'
+           TKFRAME_-82898_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82898_ANGLES     = ( -90.0,   -90.0,     0.0 )
+           TKFRAME_-82898_AXES       = (     3,       1,       3 )
+           TKFRAME_-82898_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+UVIS Frames
+----------------------------------------------------------
+ 
+   The Ultraviolet Imaging Spectrograph (UVIS) is mounted on the remote
+   sensing pallet on the +X side of the Cassini spacecraft, and nominally
+   directed along the -Y axis of the AACS body frame.
+ 
+   Note the angles in the frame definitions are specified for the "from
+   instrument to (relative to) base frame" transformation.
+ 
+ 
+Ultraviolet Imaging Spectrograph Far Ultraviolet Spectrograph (UVIS_FUV)
+ 
+   An examination of [5] reveals that UVIS_FUV points nominally along the
+   spacecraft -Y axis. The rotation matrix that takes vectors represented in
+   the UVIS_FUV frame into the spacecraft frame follows:
+ 
+           [     ]    [     ]  [     ]  [       ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ -90.0 ]
+           [     ]    [     ]  [     ]  [       ]
+                             Z        Y          X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   The following frame definition describes this nominal frame:
+ 
+           Nominal Frame Definition:
+ 
+           FRAME_CASSINI_UVIS_FUV    = -82840
+           FRAME_-82840_NAME         = 'CASSINI_UVIS_FUV'
+           FRAME_-82840_CLASS        = 4
+           FRAME_-82840_CLASS_ID     = -82840
+           FRAME_-82840_CENTER       = -82
+           TKFRAME_-82840_SPEC       = 'ANGLES'
+           TKFRAME_-82840_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82840_ANGLES     = ( 0.0,     0.0,   -90.0 )
+           TKFRAME_-82840_AXES       = (   3,       2,       1 )
+           TKFRAME_-82840_UNITS      = 'DEGREES'
+ 
+ 
+   From [40], the UVIS_FUV boresight has been adjusted to the following vector
+   in spacecraft coordinates:
+ 
+                                       [  0.0002     ]
+           UVIS_FUV Boresight Vector = [ -0.99999998 ]
+                                       [  0.0001     ]
+ 
+   This leads to the following rotation matrix that takes vectors represented
+   in the UVIS_FUV frame into the spacecraft frame:
+ 
+           [     ]    [          ]  [           ]  [          ]
+           [ ROT ]  = [ -89.9999 ]  [ -0.011459 ]  [ 0.005729 ]
+           [     ]    [          ]  [           ]  [          ]
+                                  X              Y             X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+ 
+           FRAME_CASSINI_UVIS_FUV    = -82840
+           FRAME_-82840_NAME         = 'CASSINI_UVIS_FUV'
+           FRAME_-82840_CLASS        = 4
+           FRAME_-82840_CLASS_ID     = -82840
+           FRAME_-82840_CENTER       = -82
+           TKFRAME_-82840_SPEC       = 'ANGLES'
+           TKFRAME_-82840_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82840_ANGLES     = (
+                                         -89.999999,
+                                          -0.01145916,
+                                           0.005729578
+                                       )
+           TKFRAME_-82840_AXES       = ( 1, 2, 1 )
+           TKFRAME_-82840_UNITS      = 'DEGREES'
+ 
+ 
+   ______________________________________________________________
+   ++++++++++++++++++++October 14, 2004++++++++++++++++++++++++++++
+ 
+   From [50], the UVIS_FUV boresight has been adjusted to the following vector
+   in spacecraft coordinates:
+ 
+                                       [  0.0002000  ]
+           UVIS_FUV Boresight Vector = [ -0.9999999  ]
+                                       [  0.0001000  ]
+ 
+   In addition, from [51] the instrument Y axis is specified to be parallel to
+   the spacecraft -Z axis. This leads to the following rotation matrix that
+   takes vectors represented in the UVIS_FUV frame into the spacecraft frame:
+ 
+           [   ]   [                ] [                ] [                ]
+           [ROT] = [ -90.00000000000] [+179.98854084310] [+179.99427042161]
+           [   ]   [                ] [                ] [                ]
+                                     X                  Y                  X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_UVIS_FUV    = -82840
+           FRAME_-82840_NAME         = 'CASSINI_UVIS_FUV'
+           FRAME_-82840_CLASS        = 4
+           FRAME_-82840_CLASS_ID     = -82840
+           FRAME_-82840_CENTER       = -82
+           TKFRAME_-82840_SPEC       = 'ANGLES'
+           TKFRAME_-82840_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82840_ANGLES     = (
+                                          -90.00000000000,
+                                         +179.98854084310 ,
+                                         +179.99427042161
+                                       )
+           TKFRAME_-82840_AXES       = ( 1, 2, 1 )
+           TKFRAME_-82840_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Ultraviolet Imaging Spectrograph Extreme Ultraviolet Spectrograph (UVIS_EUV)
+ 
+   An examination of [5] reveals that the UVIS_EUV points nominally along the
+   spacecraft -Y axis. The rotation matrix that takes vectors represented in
+   the UVIS_EUV frame into the spacecraft frame follows:
+ 
+           [     ]    [     ]  [     ]  [       ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ -90.0 ]
+           [     ]    [     ]  [     ]  [       ]
+                             Z        Y          X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   The following frame definition describes this nominal frame:
+ 
+           Nominal Frame Definition:
+ 
+           FRAME_CASSINI_UVIS_EUV    = -82842
+           FRAME_-82842_NAME         = 'CASSINI_UVIS_EUV'
+           FRAME_-82842_CLASS        = 4
+           FRAME_-82842_CLASS_ID     = -82842
+           FRAME_-82842_CENTER       = -82
+           TKFRAME_-82842_SPEC       = 'ANGLES'
+           TKFRAME_-82842_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82842_ANGLES     = ( 0.0,     0.0,   -90.0 )
+           TKFRAME_-82842_AXES       = (   3,       2,       1 )
+           TKFRAME_-82842_UNITS      = 'DEGREES'
+ 
+ 
+   From [40], the UVIS_EUV boresight has been adjusted to the following vector
+   in spacecraft coordinates:
+ 
+                                       [  0.0012     ]
+           UVIS_EUV Boresight Vector = [ -0.99999843 ]
+                                       [  0.0013     ]
+ 
+   This leads to the following rotation matrix that takes vectors represented
+   in the UVIS_EUV frame into the spacecraft frame:
+ 
+           [     ]    [          ]  [           ]  [          ]
+           [ ROT ]  = [ -89.8984 ]  [ -0.068755 ]  [ -0.02704 ]
+           [     ]    [          ]  [           ]  [          ]
+                                  X              Y             X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+ 
+           FRAME_CASSINI_UVIS_EUV    = -82842
+           FRAME_-82842_NAME         = 'CASSINI_UVIS_EUV'
+           FRAME_-82842_CLASS        = 4
+           FRAME_-82842_CLASS_ID     = -82842
+           FRAME_-82842_CENTER       = -82
+           TKFRAME_-82842_SPEC       = 'ANGLES'
+           TKFRAME_-82842_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82842_ANGLES     = (
+                                         -89.8984716,
+                                          -0.068755,
+                                          -0.027044457
+                                       )
+           TKFRAME_-82842_AXES       = ( 1, 2, 1 )
+           TKFRAME_-82842_UNITS      = 'DEGREES'
+ 
+ 
+   ______________________________________________________________
+   ++++++++++++++++++++October 14, 2004++++++++++++++++++++++++++++
+ 
+   From [50], the UVIS_EUV boresight has been adjusted to the following vector
+   in spacecraft coordinates:
+ 
+                                       [  0.0011999   ]
+           UVIS_EUV Boresight Vector = [ -0.9999984   ]
+                                       [  0.0012999   ]
+ 
+   In addition, from [51] the instrument Y axis is specified to be parallel to
+   the spacecraft -Z axis. This leads to the following rotation matrix that
+   takes vectors represented in the UVIS_EUV frame into the spacecraft frame:
+ 
+           [   ]   [               ] [                ] [                ]
+           [ROT] = [-90.00000000000] [+179.93125071716] [+179.92552119261]
+           [   ]   [               ] [                ] [                ]
+                                    X                  Y                  X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_UVIS_EUV    = -82842
+           FRAME_-82842_NAME         = 'CASSINI_UVIS_EUV'
+           FRAME_-82842_CLASS        = 4
+           FRAME_-82842_CLASS_ID     = -82842
+           FRAME_-82842_CENTER       = -82
+           TKFRAME_-82842_SPEC       = 'ANGLES'
+           TKFRAME_-82842_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82842_ANGLES     = (
+                                         -90.00000000000,
+                                         +179.93125071716 ,
+                                         +179.92552119261
+                                       )
+           TKFRAME_-82842_AXES       = ( 1, 2, 1 )
+           TKFRAME_-82842_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Ultraviolet Imaging Spectrograph Solar Occultation Port (UVIS_SOLAR)
+ 
+   [29] and [30] indicate that the UVIS solar occultation port points
+   nominally 20 degrees offset from the nominal UVIS boresights in the -Y
+   direction of the nominal instrument frames. The rotation matrix that takes
+   vectors represented in the CASSINI_UVIS_SOLAR frame into the
+   CASSINI_SC_COORD frame follows:
+ 
+           [     ]    [     ]  [     ]  [        ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ -110.0 ]
+           [     ]    [     ]  [     ]  [        ]
+                             Z        Y           X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_UVIS_SOLAR    = -82843
+           FRAME_-82843_NAME           = 'CASSINI_UVIS_SOLAR'
+           FRAME_-82843_CLASS          = 4
+           FRAME_-82843_CLASS_ID       = -82843
+           FRAME_-82843_CENTER         = -82
+           TKFRAME_-82843_SPEC         = 'ANGLES'
+           TKFRAME_-82843_RELATIVE     = 'CASSINI_SC_COORD'
+           TKFRAME_-82843_ANGLES       = ( 0.0,     0.0,   -110.0 )
+           TKFRAME_-82843_AXES         = (   3,       2,      1   )
+           TKFRAME_-82843_UNITS        = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Ultraviolet Imaging Spectrograph Solar Occultation Port with Offset
+(UVIS_SOL_OFF)
+ 
+   In reality the UVIS solar occultation port boresight has an offset from its
+   nominal viewing direction. For convenience of the ground system tools,
+   instead of incorporating this offset into the definition of the
+   CASSINI_UVIS_SOLAR frame, this FK defines a separate frame,
+   CASSINI_UVIS_SOL_OFF (ID -82849), aligned with the actual view direction.
+   The rotation matrix that takes vectors represented in the
+   CASSINI_UVIS_SOL_OFF frame into the CASSINI_SC_COORD frame is (from [52]):
+ 
+           [     ]    [        ]  [     ]  [          ]
+           [ ROT ]  = [ -110.0 ]  [ 0.0 ]  [ -0.11459 ]
+           [     ]    [        ]  [     ]  [          ]
+                                X        Z             Y
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+             i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_UVIS_SOL_OFF  = -82849
+           FRAME_-82849_NAME           = 'CASSINI_UVIS_SOL_OFF'
+           FRAME_-82849_CLASS          = 4
+           FRAME_-82849_CLASS_ID       = -82849
+           FRAME_-82849_CENTER         = -82
+           TKFRAME_-82849_SPEC         = 'ANGLES'
+           TKFRAME_-82849_RELATIVE     = 'CASSINI_SC_COORD'
+           TKFRAME_-82849_ANGLES       = ( -110.0,    0.0,  -0.11459 )
+           TKFRAME_-82849_AXES         = (    1,      3,     2       )
+           TKFRAME_-82849_UNITS        = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Ultraviolet Imaging Spectrograph High Speed Photometer (UVIS_HSP)
+ 
+   An examination of [5] reveals that the UVIS_HSP points nominally along the
+   spacecraft -Y axis. The rotation matrix that takes vectors represented in
+   the UVIS_HSP frame into the spacecraft frame follows:
+ 
+           [     ]    [     ]  [     ]  [       ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ -90.0 ]
+           [     ]    [     ]  [     ]  [       ]
+                             Z        Y          X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   The following frame definition describes this nominal frame:
+ 
+           Nominal Frame Definition:
+ 
+           FRAME_CASSINI_UVIS_HSP    = -82844
+           FRAME_-82844_NAME         = 'CASSINI_UVIS_HSP'
+           FRAME_-82844_CLASS        = 4
+           FRAME_-82844_CLASS_ID     = -82844
+           FRAME_-82844_CENTER       = -82
+           TKFRAME_-82844_SPEC       = 'ANGLES'
+           TKFRAME_-82844_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82844_ANGLES     = ( 0.0,     0.0,   -90.0 )
+           TKFRAME_-82844_AXES       = (   3,       2,       1 )
+           TKFRAME_-82844_UNITS      = 'DEGREES'
+ 
+ 
+   From [40], the UVIS_HSP boresight has been adjusted to the following vector
+   in spacecraft coordinates:
+ 
+                                       [  0.0012     ]
+           UVIS_HSP Boresight Vector = [ -0.99999856 ]
+                                       [ -0.0012     ]
+ 
+   This leads to the following rotation matrix that takes vectors represented
+   in the UVIS_HSP frame into the spacecraft frame:
+ 
+           [     ]    [          ]  [           ]  [          ]
+           [ ROT ]  = [ -89.9028 ]  [ -0.068755 ]  [ -0.16599 ]
+           [     ]    [          ]  [           ]  [          ]
+                                  X              Y             X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+ 
+           FRAME_CASSINI_UVIS_HSP    = -82844
+           FRAME_-82844_NAME         = 'CASSINI_UVIS_HSP'
+           FRAME_-82844_CLASS        = 4
+           FRAME_-82844_CLASS_ID     = -82844
+           FRAME_-82844_CENTER       = -82
+           TKFRAME_-82844_SPEC       = 'ANGLES'
+           TKFRAME_-82844_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82844_ANGLES     = (
+                                         -89.9027658,
+                                          -0.068755,
+                                          -0.1659861
+                                       )
+           TKFRAME_-82844_AXES       = ( 1, 2, 1 )
+           TKFRAME_-82844_UNITS      = 'DEGREES'
+ 
+ 
+   ______________________________________________________________
+   ++++++++++++++++++++October 14, 2004++++++++++++++++++++++++++++
+ 
+   From [50], the UVIS_HSP boresight has been adjusted to the following vector
+   in spacecraft coordinates:
+ 
+                                       [  0.0011999   ]
+           UVIS_HSP Boresight Vector = [ -0.9999985   ]
+                                       [ -0.0011999   ]
+ 
+   In addition, from [51] the instrument Y axis is specified to be parallel to
+   the spacecraft -Z axis. This leads to the following rotation matrix that
+   takes vectors represented in the UVIS_HSP frame into the spacecraft frame:
+ 
+           [   ]   [                ] [                ] [                ]
+           [ROT] = [- 90.00000000000] [+179.93125072403] [-179.93125077352]
+           [   ]   [                ] [                ] [                ]
+                                     X                  Y                  X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_UVIS_HSP    = -82844
+           FRAME_-82844_NAME         = 'CASSINI_UVIS_HSP'
+           FRAME_-82844_CLASS        = 4
+           FRAME_-82844_CLASS_ID     = -82844
+           FRAME_-82844_CENTER       = -82
+           TKFRAME_-82844_SPEC       = 'ANGLES'
+           TKFRAME_-82844_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82844_ANGLES     = (
+                                         -90.00000000000,
+                                        +179.93125072403,
+                                        -179.93125077352
+                                       )
+           TKFRAME_-82844_AXES       = ( 1, 2, 1 )
+           TKFRAME_-82844_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Ultraviolet Imaging Spectrograph Hydrogen - Deuterium Absorption Cell
+(UVIS_HDAC)
+ 
+   An examination of [5] reveals that the UVIS_HDAC points nominally along the
+   spacecraft -Y axis. The rotation matrix that takes vectors represented in
+   the UVIS_HSP frame into the spacecraft frame follows:
+ 
+           [     ]    [     ]  [     ]  [       ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ -90.0 ]
+           [     ]    [     ]  [     ]  [       ]
+                             Z        Y          X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   The following frame definition describes this nominal frame:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_UVIS_HDAC   = -82845
+           FRAME_-82845_NAME         = 'CASSINI_UVIS_HDAC'
+           FRAME_-82845_CLASS        = 4
+           FRAME_-82845_CLASS_ID     = -82845
+           FRAME_-82845_CENTER       = -82
+           TKFRAME_-82845_SPEC       = 'ANGLES'
+           TKFRAME_-82845_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82845_ANGLES     = ( 0.0,     0.0,   -90.0 )
+           TKFRAME_-82845_AXES       = (   3,       2,       1 )
+           TKFRAME_-82845_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+VIMS Frames
+----------------------------------------------------------
+ 
+   The Visible and Infrared Mapping Spectrometer is mounted on the remote
+   sensing pallet on the +X side of the Cassini spacecraft, and nominally
+   directed along the -Y axis of the AACS body frame.
+ 
+   Note the angles in the frame definitions are specified for the ``from
+   instrument to (relative to) base frame'' transformation.
+ 
+ 
+Visible and Infrared Mapping Spectrometer Visible (VIMS_V)
+ 
+   The VIMS_V detector points nominally along the spacecraft -Y axis. The
+   following frame definition encapsulates this nominal frame.
+ 
+   From [13]:
+ 
+           [     ]    [     ]  [     ]  [       ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ -90.0 ]
+           [     ]    [     ]  [     ]  [       ]
+                             Z        Y          X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_VIMS_V      = -82370
+           FRAME_-82370_NAME         = 'CASSINI_VIMS_V'
+           FRAME_-82370_CLASS        = 4
+           FRAME_-82370_CLASS_ID     = -82370
+           FRAME_-82370_CENTER       = -82
+           TKFRAME_-82370_SPEC       = 'ANGLES'
+           TKFRAME_-82370_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82370_ANGLES     = (  0.0,     0.0,    -90.0 )
+           TKFRAME_-82370_AXES       = (    3,       2,        1 )
+           TKFRAME_-82370_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Visible and Infrared Mapping Spectrometer Infrared (VIMS_IR)
+ 
+   The VIMS_IR detector points nominally along the spacecraft -Y axis. The
+   following frame definition encapsulates this nominal frame.
+ 
+   From [13]:
+ 
+           [     ]    [     ]  [     ]  [       ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ -90.0 ]
+           [     ]    [     ]  [     ]  [       ]
+                             Z        Y          X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           FRAME_CASSINI_VIMS_IR     = -82371
+           FRAME_-82371_NAME         = 'CASSINI_VIMS_IR'
+           FRAME_-82371_CLASS        = 4
+           FRAME_-82371_CLASS_ID     = -82371
+           FRAME_-82371_CENTER       = -82
+           TKFRAME_-82371_SPEC       = 'ANGLES'
+           TKFRAME_-82371_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82371_ANGLES     = (  0.0,     0.0,    -90.0 )
+           TKFRAME_-82371_AXES       = (    3,       2,        1 )
+           TKFRAME_-82371_UNITS      = 'DEGREES'
+ 
+ 
+   From [41], the VIMS_IR boresight has been adjusted to the following vector
+   in spacecraft coordinates:
+ 
+                                      [  0.0021251 ]
+           VIMS_IR Boresight Vector = [ -0.9999974 ]
+                                      [ -0.0008495 ]
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   By the methodology outlined above, this produces the following frame
+   definition:
+ 
+           [     ]    [             ]  [             ]  [     ]
+           [ ROT ]  = [ -360.121759 ]  [ -90.0486727 ]  [ 0.0 ]
+           [     ]    [             ]  [             ]  [     ]
+                                     Z                X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_VIMS_IR     = -82371
+           FRAME_-82371_NAME         = 'CASSINI_VIMS_IR'
+           FRAME_-82371_CLASS        = 4
+           FRAME_-82371_CLASS_ID     = -82371
+           FRAME_-82371_CENTER       = -82
+           TKFRAME_-82371_SPEC       = 'ANGLES'
+           TKFRAME_-82371_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82371_ANGLES     = (
+                                         -360.12175939433,
+                                          -90.048672769633,
+                                            0.0
+                                       )
+           TKFRAME_-82371_AXES       = ( 3, 1, 3 )
+           TKFRAME_-82371_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Visible and Infrared Mapping Spectrometer Infrared Solar Port (VIMS_IR_SOL)
+ 
+   [28] indicates that the VIMS IR channel solar port points nominally 20
+   degrees offset from the VIMS IR boresight in the -Y direction of the
+   VIMS_IR frame. The rotation matrix that takes vectors represented in the
+   VIMS_IR_SOL frame into the VIMS_IR frame follows:
+ 
+           [     ]    [     ]  [     ]  [       ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ -20.0 ]
+           [     ]    [     ]  [     ]  [       ]
+                             Z        Y          X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+ 
+           FRAME_CASSINI_VIMS_IR_SOL   = -82372
+           FRAME_-82372_NAME           = 'CASSINI_VIMS_IR_SOL'
+           FRAME_-82372_CLASS          = 4
+           FRAME_-82372_CLASS_ID       = -82372
+           FRAME_-82372_CENTER         = -82
+           TKFRAME_-82372_SPEC         = 'ANGLES'
+           TKFRAME_-82372_RELATIVE     = 'CASSINI_VIMS_IR'
+           TKFRAME_-82372_ANGLES       = ( 0.0,     0.0,   -20.0 )
+           TKFRAME_-82372_AXES         = (   3,       2,       1 )
+           TKFRAME_-82372_UNITS        = 'DEGREES'
+ 
+ 
+   [42] requested that CASSINI_VIMS_IR_SOL be referenced directly to
+   CASSINI_SC_COORD. In addition, [42], [43], and [45] also carry updates to
+   the alignment of the solar port. The rotation matrix that takes vectors
+   represented in the VIMS_IR_SOL frame into the CASSINI_SC_COORD frame
+   follows:
+ 
+           [     ]    [                 ]  [     ]  [                ]
+           [ ROT ]  = [ 0.0859436686699 ]  [ 0.0 ]  [ -110.630253571 ]
+           [     ]    [                 ]  [     ]  [                ]
+                                         Z        Y                   X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_VIMS_IR_SOL   = -82372
+           FRAME_-82372_NAME           = 'CASSINI_VIMS_IR_SOL'
+           FRAME_-82372_CLASS          = 4
+           FRAME_-82372_CLASS_ID       = -82372
+           FRAME_-82372_CENTER         = -82
+           TKFRAME_-82372_SPEC         = 'ANGLES'
+           TKFRAME_-82372_RELATIVE     = 'CASSINI_SC_COORD'
+           TKFRAME_-82372_ANGLES       = (    0.085943668669984,
+                                              0.0,
+                                           -110.63025357166      )
+           TKFRAME_-82372_AXES         = (    3,    2,    1      )
+           TKFRAME_-82372_UNITS        = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Visible and Infrared Mapping Spectrometer Radiator (VIMS_RAD)
+ 
+   The VIMS radiator is nominally oriented with its +Z axis directed down the
+   spacecraft +X axis. This is not the case for the radiator plate itself,
+   which is mounted in the housing such that it is canted by 28.05 degrees. In
+   the spacecraft coordinate frame, the cant is towards the spacecraft -Y
+   axis.
+ 
+   This, however, is not the end of the story. Thermally, the radiator housing
+   and the radiator plate have interaction with respect to solar heating so
+   that the effective boresight for symmetric solar heating, regardless of
+   direction, is not offset by 28.05 degrees from the spacecraft +X axis.
+   Initially the +Z axis of the radiator frame was determined to be the +X
+   axis of the spacecraft frame. This results in the following:
+ 
+   Since only boresight information has been provided, the frame
+   transformation outlined below was constructed by computing the RA and DEC
+   of the boresight vector relative to the CASSINI_SC_COORD frame. These
+   angles are then utilized in the following fashion to construct the frame
+   definition:
+ 
+           [     ]    [          ]  [           ]  [     ]
+           [ ROT ]  = [ -(RA+90) ]  [ -(90-DEC) ]  [ 0.0 ]
+           [     ]    [          ]  [           ]  [     ]
+                                  Z              X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+   This produces a frame whose Z-axis agrees with the specified boresight.
+ 
+   As [17] indicates, the VIMS_RAD boresight is nominally aligned with the +X
+   axis in the spacecraft frame. By the methodology outlined above, this
+   produces the following frame definition:
+ 
+           [     ]    [       ]  [       ]  [     ]
+           [ ROT ]  = [ -90.0 ]  [ -90.0 ]  [ 0.0 ]
+           [     ]    [       ]  [       ]  [     ]
+                               Z          X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           FRAME_CASSINI_VIMS_RAD    = -82378
+           FRAME_-82378_NAME         = 'CASSINI_VIMS_RAD'
+           FRAME_-82378_CLASS        = 4
+           FRAME_-82378_CLASS_ID     = -82378
+           FRAME_-82378_CENTER       = -82
+           TKFRAME_-82378_SPEC       = 'ANGLES'
+           TKFRAME_-82378_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82378_ANGLES     = ( -90.0,   -90.0,     0.0 )
+           TKFRAME_-82378_AXES       = (     3,       1,       3 )
+           TKFRAME_-82378_UNITS      = 'DEGREES'
+ 
+ 
+   From [36]:
+ 
+   A solar heating analysis and identification of a solar heating
+   ``effective'' radiator boresight was performed for ECR 100325-B covering
+   Flight Rule FF37B2 [37]. The solar heating analysis identified that a VIMS
+   radiator boresight offset from the spacecraft +X axis in the direction of
+   the spacecraft -Y axis by 4.5 degrees would define a thermally
+   ``effective'' boresight.
+ 
+   To implement this change, the rotation about the Z-axis needs to be
+   increased by 4.5 degrees as follows:
+ 
+           [     ]    [       ]  [       ]  [     ]
+           [ ROT ]  = [ -85.5 ]  [ -90.0 ]  [ 0.0 ]
+           [     ]    [       ]  [       ]  [     ]
+                               Z          X        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_VIMS_RAD    = -82378
+           FRAME_-82378_NAME         = 'CASSINI_VIMS_RAD'
+           FRAME_-82378_CLASS        = 4
+           FRAME_-82378_CLASS_ID     = -82378
+           FRAME_-82378_CENTER       = -82
+           TKFRAME_-82378_SPEC       = 'ANGLES'
+           TKFRAME_-82378_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82378_ANGLES     = ( -85.5,   -90.0,     0.0 )
+           TKFRAME_-82378_AXES       = (     3,       1,       3 )
+           TKFRAME_-82378_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+CAPS Frames
+----------------------------------------------------------
+ 
+   The Cassini Plasma Spectrometer is mounted on an actuator which is in turn
+   attached to the fields and particles pallet which is roughly located on the
+   -X side of the Cassini spacecraft.
+ 
+   The actuator allows the instrument to articulate, so to make proper use of
+   this frame requires a C-kernel (or set of C-kernels) with appropriate
+   coverage for the epochs of interest.
+ 
+   To connect the CASSINI_CAPS frame with the spacecraft coordinate frame
+   (CASSINI_SC_COORD) two possible branches exist depending on the set of
+   C-kernels loaded:
+ 
+ 
+               CASSINI_SC_COORD           CASSINI_SC_COORD
+               ----------------           ----------------
+                      |                          |
+                      |<--- fixed offset         |
+                      |                          |
+                      V                          |
+               CASSINI_CAPS_BASE                 |
+               -----------------                 |
+                      |                          |
+                      |<--- c-kernel             |<--- c-kernel
+                      |                          |
+                      V                          |
+               CASSINI_CAPS_ART                  |
+               ----------------                  |
+                      |                          |
+                      |<--- c-kernel             |
+                      |                          |
+                      V                          V
+                 CASSINI_CAPS               CASSINI_CAPS
+                 ------------               ------------
+ 
+ 
+   The branch illustrated on the left of the figure above utilizes a series of
+   transformations to connect the spacecraft frame with the instrument frame.
+   The general strategy in this branch is the following:
+ 
+            --   Define a fixed offset frame that connects the spacecraft
+                 frame to the base or 'zero-point' of the articulation of the
+                 instrument.
+ 
+            --   Define a C-kernel based frame to perform the rotation about
+                 the articulation axis.
+ 
+            --   Define a C-kernel based frame that performs the final
+                 rotation necessary to produce the instrument frame.
+ 
+   This last frame in the absence of the right branch could be another fixed
+   offset frame. However, making it a C-kernel allows the branch on the right
+   to exist. This alternate route up the frame tree allows the construction
+   and use of C-kernels that tie the instrument frame directly back to the
+   spacecraft frame. This is often convenient for science data analysis.
+ 
+   Without further ado, the frame definitions:
+ 
+ 
+Cassini Plasma Spectrometer Zero-Articulation Base Frame (CAPS_BASE)
+ 
+   The Z-axis of this frame is the articulation axis of CAPS. The X-axis is
+   constructed by taking the vector product of the CAPS articulation axis with
+   the boresight in the 'zero-angle' or base position. The Y-axis completes
+   the right handed frame. The articulation axis of CAPS is the Z-axis of
+   CASSINI_SC_COORD, and the boresight in its 'zero-angle' configuration is
+   the negative Y-axis of this spacecraft frame, so we end up with the
+   following:
+ 
+   The rotation matrix that takes vectors represented in the CAPS_BASE frame
+   into the spacecraft coordinate frame follows:
+ 
+           [     ]    [     ]  [     ]  [     ]
+           [ ROT ]  = [ 0.0 ]  [ 0.0 ]  [ 0.0 ]
+           [     ]    [     ]  [     ]  [     ]
+                             Z        Y        X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_CAPS_BASE    = -82822
+           FRAME_-82822_NAME         = 'CASSINI_CAPS_BASE'
+           FRAME_-82822_CLASS        = 4
+           FRAME_-82822_CLASS_ID     = -82822
+           FRAME_-82822_CENTER       = -82
+           TKFRAME_-82822_SPEC       = 'ANGLES'
+           TKFRAME_-82822_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82822_ANGLES     = (   0.0,     0.0,     0.0 )
+           TKFRAME_-82822_AXES       = (     3,       2,       1 )
+           TKFRAME_-82822_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Cassini Plasma Spectrometer Articulation Frame (CAPS_ART)
+ 
+   The Z-axis of this frame is the articulation axis of CAPS. The X-axis is
+   constructed by taking the vector product of the CAPS articulation axis with
+   the boresight at some articulated position. The Y-axis completes the right
+   handed frame.
+ 
+   This frame encapsulates the articulation characteristics of the CAPS
+   instrument. To make use of it requires a C-kernel with coverage at the
+   epochs of interest be loaded.
+ 
+   The rotation matrix that takes vectors from the CAPS_ART frame to the
+   CAPS_BASE frame follows:
+ 
+           [     ]    [       ]
+           [ ROT ]  = [ ANGLE ]
+           [     ]    [       ]
+                               Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i, and ANGLE is the articulation angle.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_CAPS_ART   = -82821
+           FRAME_-82821_NAME        = 'CASSINI_CAPS_ART'
+           FRAME_-82821_CLASS       = 3
+           FRAME_-82821_CLASS_ID    = -82821
+           FRAME_-82821_CENTER      = -82
+           CK_-82821_SCLK           = -82
+           CK_-82821_SPK            = -82
+ 
+           \begintext
+ 
+ 
+Cassini Plasma Spectrometer Frame (CAPS)
+ 
+   The negative Y-axis of this frame is the instrument boresight. The Z-axis
+   is defined as the articulation axis of the detectors, and the X-axis
+   completes the right handed frame.
+ 
+   This frame requires one of two possible C-kernels:
+ 
+            --   One kernel connects this instrument frame (-82820) directly
+                 to the spacecraft frame (-82000).
+ 
+            --   The other possible kernel connects this instrument frame
+                 (-82820) to the articulation frame (-82821) defined above.
+                 The kernel that makes this connection for all epochs after
+                 launch is delivered with the kernel set. See the kernel
+                 comments for details of frame construction.
+ 
+   One should take care in the simultaneous loading of C-kernels that utilize
+   different paths of the frame tree to connect CASSINI_CAPS to
+   CASSINI_SC_COORD. See [1] for details regarding C-kernel precedence.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_CAPS       = -82820
+           FRAME_-82820_NAME        = 'CASSINI_CAPS'
+           FRAME_-82820_CLASS       = 3
+           FRAME_-82820_CLASS_ID    = -82820
+           FRAME_-82820_CENTER      = -82
+           CK_-82820_SCLK           = -82
+           CK_-82820_SPK            = -82
+ 
+           \begintext
+ 
+ 
+CDA Frames
+----------------------------------------------------------
+ 
+   The Cosmic Dust Analyzer is mounted on the -X side of the Cassini
+   spacecraft. The entire assembly is capable of articulating from it's zero
+   angle position. The following describes the boresight in the spacecraft
+   frame as a function of the articulation angle a:
+ 
+           From [18]:
+ 
+           x = 1/8 ( -1 - SQRT(3) + (-1 + SQRT(3)) COS(a) - 2 SQRT(6) SIN(a) )
+           y = 1/8 (  3 + SQRT(3) + (-3 + SQRT(3)) COS(a) - 2 SQRT(2) SIN(a) )
+           z = 1/4 ( -1 + SQRT(3) + ( 1 + SQRT(3)) COS(a) )
+ 
+ 
+   The actuator allows the instrument to articulate, so to make proper use of
+   this frame requires a C-kernel (or set of C-kernels) with appropriate
+   coverage for the epochs of interest.
+ 
+   To connect the CASSINI_CDA frame with the spacecraft coordinate frame
+   (CASSINI_SC_COORD) two possible branches exist depending on the set of
+   C-kernels loaded:
+ 
+ 
+               CASSINI_SC_COORD           CASSINI_SC_COORD
+               ----------------           ----------------
+                      |                          |
+                      |<--- fixed offset         |
+                      |                          |
+                      V                          |
+               CASSINI_CDA_BASE                  |
+               ----------------                  |
+                      |                          |
+                      |<--- c-kernel             |<--- c-kernel
+                      |                          |
+                      V                          |
+               CASSINI_CDA_ART                   |
+               ---------------                   |
+                      |                          |
+                      |<--- c-kernel             |
+                      |                          |
+                      V                          V
+                 CASSINI_CDA                CASSINI_CDA
+                 -----------                -----------
+ 
+ 
+   The branch illustrated on the left of the figure above utilizes a series of
+   transformations to connect the spacecraft frame with the instrument frame.
+   The general strategy in this branch is the following:
+ 
+            --   Define a fixed offset frame that connects the spacecraft
+                 frame to the base or 'zero-point' of the articulation of the
+                 instrument.
+ 
+            --   Define a C-kernel based frame to perform the rotation about
+                 the articulation axis.
+ 
+            --   Define a C-kernel based frame that performs the final
+                 rotation necessary to produce the instrument frame.
+ 
+   This last frame in the absence of the right branch could be another fixed
+   offset frame. However, making it a C-kernel allows the branch on the right
+   to exist. This alternate route up the frame tree allows the construction
+   and use of C-kernels that tie the instrument frame directly back to the
+   spacecraft frame. This is often convenient for science data analysis.
+ 
+   Without further ado, the frame definitions:
+ 
+ 
+Cosmic Dust Analyzer Zero-Articulation Base Frame (CDA_BASE)
+ 
+   The Z-axis of this frame is the articulation axis of CDA. The X-axis is
+   constructed by taking the vector product of the CDA articulation axis with
+   the boresight in the 'zero-angle' or base position. The Y-axis completes
+   the right handed frame.
+ 
+   An examination of the relationship connecting the boresight position in the
+   spacecraft frame with the articulation angle, yields the following:
+ 
+           The articulation axis of CDA in CASSINI_SC_COORD is:
+ 
+           (+4.8296291314453E-01, -8.3651630373781E-01, -2.5881904510252E-01)
+ 
+           The 'zero-angle' boresight in CASSINI_SC_COORD is:
+ 
+           (-2.5000000000000E-01, 4.3301270189222E-01, 8.6602540378444E-01)
+ 
+ 
+   The articulation axis points in the opposite direction of the cone swept
+   out by the boresight vectors. This was done to preserve the sense of the
+   positive angle in the definition provided in [18].
+ 
+   Computing the frame described above we end up with:
+ 
+   The rotation matrix that takes vectors represented in the CDA_BASE frame
+   into the spacecraft coordinate frame follows:
+ 
+           [     ]    [       ]  [     ]  [       ]
+           [ ROT ]  = [ 150.0 ]  [ 0.0 ]  [ 105.0 ]
+           [     ]    [       ]  [     ]  [       ]
+                               Z        Y          X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_CDA_BASE    = -82792
+           FRAME_-82792_NAME         = 'CASSINI_CDA_BASE'
+           FRAME_-82792_CLASS        = 4
+           FRAME_-82792_CLASS_ID     = -82792
+           FRAME_-82792_CENTER       = -82
+           TKFRAME_-82792_SPEC       = 'ANGLES'
+           TKFRAME_-82792_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82792_ANGLES     = ( 150.0,     0.0,   105.0 )
+           TKFRAME_-82792_AXES       = (     3,       2,       1 )
+           TKFRAME_-82792_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Cosmic Dust Analyzer Articulation Frame (CDA_ART)
+ 
+   The Z-axis of this frame is the articulation axis of CDA. The X-axis is
+   constructed by taking the vector product of the CDA articulation axis with
+   the boresight at some articulated position. The Y-axis completes the right
+   handed frame.
+ 
+   This frame encapsulates the articulation characteristics of the CDA
+   instrument. To make use of it requires a C-kernel with coverage at the
+   epochs of interest be loaded.
+ 
+   The rotation matrix that takes vectors from the CDA_ART frame to the
+   CDA_BASE frame follows:
+ 
+           [     ]    [       ]
+           [ ROT ]  = [ ANGLE ]
+           [     ]    [       ]
+                               Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i, and ANGLE is the articulation angle.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_CDA_ART    = -82791
+           FRAME_-82791_NAME        = 'CASSINI_CDA_ART'
+           FRAME_-82791_CLASS       = 3
+           FRAME_-82791_CLASS_ID    = -82791
+           FRAME_-82791_CENTER      = -82
+           CK_-82791_SCLK           = -82
+           CK_-82791_SPK            = -82
+ 
+           \begintext
+ 
+ 
+Cosmic Dust Analyzer Frame (CDA)
+ 
+   The Z-axis of this frame is the instrument boresight. The X-axis of is the
+   same as the X-axis of CASSINI_CDA_ART, and the Y-axis completes the right
+   handed frame.
+ 
+   This frame requires one of two possible C-kernels:
+ 
+            --   One kernel connects this instrument frame (-82790) directly
+                 to the spacecraft frame (-82000).
+ 
+            --   The other possible kernel connects this instrument frame
+                 (-82790) to the articulation frame (-82791) defined above.
+                 The kernel that makes this connection for all epochs after
+                 launch is delivered with the kernel set. See the kernel
+                 comments for details of frame construction.
+ 
+   One should take care in the simultaneous loading of C-kernels that utilize
+   different paths of the frame tree to connect CASSINI_CDA to
+   CASSINI_SC_COORD. See [1] for details regarding C-kernel precedence.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_CDA        = -82790
+           FRAME_-82790_NAME        = 'CASSINI_CDA'
+           FRAME_-82790_CLASS       = 3
+           FRAME_-82790_CLASS_ID    = -82790
+           FRAME_-82790_CENTER      = -82
+           CK_-82790_SCLK           = -82
+           CK_-82790_SPK            = -82
+ 
+           \begintext
+ 
+ 
+INMS Frames
+----------------------------------------------------------
+ 
+   The Ion and Neutral Mass Spectrometer is mounted on the fields and
+   particles pallet roughly located on the -X side of the Cassini spacecraft.
+   The instrument boresight is nominally directed along the -X axis of the
+   AACS body frame.
+ 
+   Note the angles in the frame definitions are specified for the ``from
+   instrument to (relative to) base frame'' transformation.
+ 
+   From [19], we have the following nominal frame definition:
+ 
+           [     ]    [     ]  [       ]  [     ]
+           [ ROT ]  = [ 0.0 ]  [ +90.0 ]  [ 0.0 ]
+           [     ]    [     ]  [       ]  [     ]
+                             X          Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_INMS        = -82740
+           FRAME_-82740_NAME         = 'CASSINI_INMS'
+           FRAME_-82740_CLASS        = 4
+           FRAME_-82740_CLASS_ID     = -82740
+           FRAME_-82740_CENTER       = -82
+           TKFRAME_-82740_SPEC       = 'ANGLES'
+           TKFRAME_-82740_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82740_ANGLES     = (   0.0,   +90.0,     0.0 )
+           TKFRAME_-82740_AXES       = (     1,       2,       3 )
+           TKFRAME_-82740_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+MAG Frames
+----------------------------------------------------------
+ 
+   The Magnetometer is mounted on the magnetometer boom which protrudes from
+   the spacecraft body in the direction of the +Y axis of the AACS body frame.
+   [20] establishes the need for two separate frame definitions, one for the
+   Plus-X directed frame, the other for the Minux-X one.
+ 
+   Note the angles in the frame definitions are specified for the ``from
+   instrument to (relative to) base frame'' transformation.
+ 
+ 
+Magnetometer Plus-X (MAG_PLUS)
+ 
+   The MAG_PLUS detector is pointed nominally in the direction of the
+   spacecraft +X axis. The following definition encapsulates this frame:
+ 
+           From [21]:
+ 
+           [     ]    [     ]  [       ]  [     ]
+           [ ROT ]  = [ 0.0 ]  [ -90.0 ]  [ 0.0 ]
+           [     ]    [     ]  [       ]  [     ]
+                             X          Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_MAG_PLUS    = -82350
+           FRAME_-82350_NAME         = 'CASSINI_MAG_PLUS'
+           FRAME_-82350_CLASS        = 4
+           FRAME_-82350_CLASS_ID     = -82350
+           FRAME_-82350_CENTER       = -82
+           TKFRAME_-82350_SPEC       = 'ANGLES'
+           TKFRAME_-82350_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82350_ANGLES     = (   0.0,   -90.0,     0.0 )
+           TKFRAME_-82350_AXES       = (     1,       2,       3 )
+           TKFRAME_-82350_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Magnetometer Minus-X (MAG_MINUS)
+ 
+   The MAG_MINUS detector is pointed nominally in the direction of the
+   spacecraft -X axis. The following definition encapsulates this frame:
+ 
+           From [21]:
+ 
+           [     ]    [     ]  [      ]  [     ]
+           [ ROT ]  = [ 0.0 ]  [ 90.0 ]  [ 0.0 ]
+           [     ]    [     ]  [      ]  [     ]
+                             X         Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_MAG_MINUS   = -82351
+           FRAME_-82351_NAME         = 'CASSINI_MAG_MINUS'
+           FRAME_-82351_CLASS        = 4
+           FRAME_-82351_CLASS_ID     = -82351
+           FRAME_-82351_CENTER       = -82
+           TKFRAME_-82351_SPEC       = 'ANGLES'
+           TKFRAME_-82351_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82351_ANGLES     = (   0.0,    90.0,     0.0 )
+           TKFRAME_-82351_AXES       = (     1,       2,       3 )
+           TKFRAME_-82351_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+MIMI Frames
+----------------------------------------------------------
+ 
+   Most of the components of the Magnetospheric Imaging Instrument are mounted
+   on the fields and particles pallet roughly located on the -X side of the
+   Cassini spacecraft. The one exception is the Ion and Neutral Camera which
+   is mounted on the -Y side of the orbiter.
+ 
+   Note the angles in the frame definitions are specified for the ``from
+   instrument to (relative to) base frame'' transformation.
+ 
+ 
+Magnetospheric Imaging Instrument Charge Energy Mass Spectrometer (MIMI_CHEMS)
+ 
+   The MIMI_CHEMS detector is nominally pointed along the -X axis of the
+   spacecraft frame. The following definition encapsulates this frame:
+ 
+           From [17]:
+ 
+           [     ]    [     ]  [      ]  [      ]
+           [ ROT ]  = [ 0.0 ]  [ 90.0 ]  [ 90.0 ]
+           [     ]    [     ]  [      ]  [      ]
+                             X         Y         Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_MIMI_CHEMS  = -82760
+           FRAME_-82760_NAME         = 'CASSINI_MIMI_CHEMS'
+           FRAME_-82760_CLASS        = 4
+           FRAME_-82760_CLASS_ID     = -82760
+           FRAME_-82760_CENTER       = -82
+           TKFRAME_-82760_SPEC       = 'ANGLES'
+           TKFRAME_-82760_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82760_ANGLES     = (   0.0,   90.0,    90.0 )
+           TKFRAME_-82760_AXES       = (     1,      2,       3 )
+           TKFRAME_-82760_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Magnetospheric Imaging Instrument Ion and Neutral Camera (MIMI_INCA)
+ 
+   The MIMI_INCA detector is nominally pointed along the -Y axis of the
+   spacecraft frame with a 9.5 degree offset in the direction of the +X axis
+   of the spacecraft. The following definition encapsulates this frame:
+ 
+           From [22]:
+ 
+           [     ]    [       ]  [      ]  [     ]
+           [ ROT ]  = [ -90.0 ]  [ -9.5 ]  [ 0.0 ]
+           [     ]    [       ]  [      ]  [     ]
+                               X         Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_MIMI_INCA   = -82761
+           FRAME_-82761_NAME         = 'CASSINI_MIMI_INCA'
+           FRAME_-82761_CLASS        = 4
+           FRAME_-82761_CLASS_ID     = -82761
+           FRAME_-82761_CENTER       = -82
+           TKFRAME_-82761_SPEC       = 'ANGLES'
+           TKFRAME_-82761_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82761_ANGLES     = ( -90.0,  -9.5,     0.0 )
+           TKFRAME_-82761_AXES       = (     1,     2,       3 )
+           TKFRAME_-82761_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Magnetospheric Imaging Instrument Low Energy Magnetospheric Measurements
+(MIMI_LEMMS)
+ 
+   The actuator allows the detectors to articulate, so to make proper use of
+   this frame requires a C-kernel (or set of C-kernels) with appropriate
+   coverage for the epochs of interest.
+ 
+   To connect the CASSINI_MIMI_LEMMS1 and CASSINI_MIMI_LEMMS2 frames with the
+   spacecraft coordinate frame (CASSINI_SC_COORD) two possible branches exist
+   depending on the set of C-kernels loaded:
+ 
+ 
+               CASSINI_SC_COORD              CASSINI_SC_COORD
+               ----------------              ----------------
+                      |                      |              |
+                      |<--- fixed offset     |              |
+                      |                      |              |
+                      V                      |              |
+            CASSINI_MIMI_LEMMS_BASE          |              |
+            -----------------------          |              |
+                      |                      |              |
+                      |<--- c-kernel         |<--- c-kernel |
+                      |                      |              |
+                      V                      |              |
+             CASSINI_MIMI_LEMMS_ART          |              |
+             ----------------------          |              |
+                |                |           |              |
+                |<--- c-kernel   |           | c-kernel --->|
+                |                |           |              |
+                V                |           V              |
+            CASSINI_MIMI_LEMMS1  |     CASSINI_MIMI_LEMMS1  |
+            -------------------  |     -------------------  |
+                                 |                          |
+                    c-kernel --->|                          |
+                                 |                          |
+                                 V                          V
+                       CASSINI_MIMI_LEMMS2          CASSINI_MIMI_LEMMS2
+                       -------------------          -------------------
+ 
+ 
+   The branches illustrated on the left of the figure above utilize a series
+   of transformations to connect the spacecraft frame with the detector
+   frames. The general strategy in these branches is the following:
+ 
+            --   Define a fixed offset frame that connects the spacecraft
+                 frame to the base or 'zero-point' of the articulation of the
+                 detectors.
+ 
+            --   Define a C-kernel based frame to perform the rotation about
+                 the articulation axis.
+ 
+            --   Define a C-kernel based frame that performs the final
+                 rotation necessary to produce either of the instrument frame.
+ 
+   These last frames (MIMI_LEMMS1 and MIMI_LEMMS2) in the absence of the right
+   branch could be another fixed offset frame. However, making them C-kernels
+   allows the branches on the right to exist. This alternate route up the
+   frame tree allows the construction and use of C-kernels that tie the
+   individual detector frames directly back to the spacecraft frame. This is
+   often convenient for science data analysis.
+ 
+   Without further ado, the frame definitions:
+ 
+ 
+Magnetospheric Imaging Instrument Low Energy Magnetospheric Measurements
+Zero-Articulation Base Frame (MIMI_LEMMS_BASE)
+ 
+   The Z-axis of this frame is the articulation axis of MIMI_LEMMS. The X-axis
+   is constructed by taking the vector product of the MIMI_LEMMS articulation
+   axis with the MIMI_LEMMS1 boresight in the 'zero-angle' or base position.
+   The Y-axis completes the right handed frame.
+ 
+   As [33] indicates, the articulation axis is the Y-axis in CASSINI_SC_COORD
+   and the 'zero-angle' boresight of MIMI_LEMMS1 is the -Z-axis in
+   CASSINI_SC_COORD. Combining this information with the frame definition laid
+   out above, we have:
+ 
+   The rotation matrix that takes vectors represented in the MIMI_LEMMS_BASE
+   frame into the spacecraft coordinate frame follows:
+ 
+           [     ]    [       ]  [     ]  [       ]
+           [ ROT ]  = [ 180.0 ]  [ 0.0 ]  [ -90.0 ]
+           [     ]    [       ]  [     ]  [       ]
+                               Z        Y          X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_MIMI_LEMMS_BASE = -82765
+           FRAME_-82765_NAME             = 'CASSINI_MIMI_LEMMS_BASE'
+           FRAME_-82765_CLASS            = 4
+           FRAME_-82765_CLASS_ID         = -82765
+           FRAME_-82765_CENTER           = -82
+           TKFRAME_-82765_SPEC           = 'ANGLES'
+           TKFRAME_-82765_RELATIVE       = 'CASSINI_SC_COORD'
+           TKFRAME_-82765_ANGLES         = ( 180.0,     0.0,   -90.0 )
+           TKFRAME_-82765_AXES           = (     3,       2,       1 )
+           TKFRAME_-82765_UNITS          = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Magnetospheric Imaging Instrument Low Energy Magnetospheric Measurements
+Articulation Frame (MIMI_LEMMS_ART)
+ 
+   The Z-axis of this frame is the articulation axis of MIMI_LEMMS. The X-axis
+   is constructed by taking the vector product of the MIMI_LEMMS articulation
+   axis with the MIMI_LEMMS1 boresight at some articulated position. The
+   Y-axis completes the right handed frame.
+ 
+   This frame encapsulates the articulation characteristics of the MIMI_LEMMS
+   instrument. To make use of it requires a C-kernel with coverage at the
+   epochs of interest be loaded.
+ 
+   The rotation matrix that takes vectors from the MIMI_LEMMS_ART frame to the
+   MIMI_LEMMS_BASE frame follows:
+ 
+           [     ]    [       ]
+           [ ROT ]  = [ ANGLE ]
+           [     ]    [       ]
+                               Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i, and ANGLE is the articulation angle.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_MIMI_LEMMS_ART  = -82764
+           FRAME_-82764_NAME             = 'CASSINI_MIMI_LEMMS_ART'
+           FRAME_-82764_CLASS            = 3
+           FRAME_-82764_CLASS_ID         = -82764
+           FRAME_-82764_CENTER           = -82
+           CK_-82764_SCLK                = -82
+           CK_-82764_SPK                 = -82
+ 
+           \begintext
+ 
+ 
+Magnetospheric Imaging Instrument Low Energy Magnetospheric Measurements 1
+(MIMI_LEMMS1)
+ 
+   The Z-axis of this frame is the instrument boresight.
+ 
+   This frame requires one of two possible C-kernels:
+ 
+            --   One kernel connects this instrument frame (-82762) directly
+                 to the spacecraft frame (-82000).
+ 
+            --   The other possible kernel connects this instrument frame
+                 (-82762) to the articulation frame (-82764) defined above.
+                 The kernel that makes this connection for all epochs after
+                 launch is delivered with the kernel set. See the kernel
+                 comments for details of the frame construction.
+ 
+   One should take care in the simultaneous loading of C-kernels that utilize
+   different paths of the frame tree to connect CASSINI_MIMI_LEMMS1 to
+   CASSINI_SC_COORD. See [1] for details regarding C-kernel precedence.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_MIMI_LEMMS1 = -82762
+           FRAME_-82762_NAME         = 'CASSINI_MIMI_LEMMS1'
+           FRAME_-82762_CLASS        = 3
+           FRAME_-82762_CLASS_ID     = -82762
+           FRAME_-82762_CENTER       = -82
+           CK_-82762_SCLK            = -82
+           CK_-82762_SPK             = -82
+ 
+           \begintext
+ 
+ 
+Magnetospheric Imaging Instrument Low Energy Magnetospheric Measurements 2
+(MIMI_LEMMS2)
+ 
+   The Z-axis of this frame is the instrument boresight.
+ 
+   This frame requires one of two possible C-kernels:
+ 
+            --   One kernel connects this instrument frame (-82763) directly
+                 to the spacecraft frame (-82000).
+ 
+            --   The other possible kernel connects this instrument frame
+                 (-82763) to the articulation frame (-82764) defined above.
+                 The kernel that makes this connection for all epochs after
+                 launch is delivered with the kernel set. See the kernel
+                 comments for details of the frame construction.
+ 
+   One should take care in the simultaneous loading of C-kernels that utilize
+   different paths of the frame tree to connect CASSINI_MIMI_LEMMS2 to
+   CASSINI_SC_COORD. See [1] for details regarding C-kernel precedence.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_MIMI_LEMMS2 = -82763
+           FRAME_-82763_NAME         = 'CASSINI_MIMI_LEMMS2'
+           FRAME_-82763_CLASS        = 3
+           FRAME_-82763_CLASS_ID     = -82763
+           FRAME_-82763_CENTER       = -82
+           CK_-82763_SCLK            = -82
+           CK_-82763_SPK             = -82
+ 
+           \begintext
+ 
+ 
+RADAR Frames
+----------------------------------------------------------
+ 
+   Compiled from [23] and [5]:
+ 
+   The RADAR instrument consists of 5 beams in the following configuration:
+ 
+ 
+                                          ^ Xsc
+                                          |
+                                          |
+                                Ysc       |
+                                   <------o
+                                          |  Zsc
+                                          |
+ 
+                                          .
+                                          .
+                                          .
+ 
+              Beam 1      Beam 2      Beam 3    Beam 4      Beam 5
+                                          |
+             |-----x-----|-----x-----|----x----|-----x-----|-----x-----|
+                                          |
+                   |-- 1.35 ---|-- 0.85 --|-- 0.85 --|-- 1.35 ---|
+                                          |
+                                          |
+                                          V
+ 
+                                   Beam 3 Direction
+ 
+ 
+   The above figure illustrates the separation in degrees between the beam
+   centers and their relation to the spacecraft frame.
+ 
+   Note the angles in the frame definitions are specified fro the ``from
+   instrument to (relative to) base frame'' transformation.
+ 
+ 
+RADAR Beam 1 (RADAR_1)
+ 
+   RADAR Beam 1 is directed nominally 2.2 degrees off of the -Z axis of the
+   spacecraft in the direction of the +Y axis of the spacecraft frame. The
+   following definition encapsulates this frame:
+ 
+           From [23]:
+ 
+           [     ]    [       ]  [     ]  [     ]
+           [ ROT ]  = [ 177.8 ]  [ 0.0 ]  [ 0.0 ]
+           [     ]    [       ]  [     ]  [     ]
+                               X        Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_RADAR_1     = -82810
+           FRAME_-82810_NAME         = 'CASSINI_RADAR_1'
+           FRAME_-82810_CLASS        = 4
+           FRAME_-82810_CLASS_ID     = -82810
+           FRAME_-82810_CENTER       = -82
+           TKFRAME_-82810_SPEC       = 'ANGLES'
+           TKFRAME_-82810_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82810_ANGLES     = ( 177.8,     0.0,     0.0 )
+           TKFRAME_-82810_AXES       = (     1,       2,       3 )
+           TKFRAME_-82810_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+RADAR Beam 2 (RADAR_2)
+ 
+   RADAR Beam 2 is directed nominally 0.85 degrees off of the -Z axis of the
+   spacecraft in the direction of the +Y axis of the spacecraft frame. The
+   following definition encapsulates this frame:
+ 
+           From [23]:
+ 
+           [     ]    [        ]  [     ]  [     ]
+           [ ROT ]  = [ 179.15 ]  [ 0.0 ]  [ 0.0 ]
+           [     ]    [        ]  [     ]  [     ]
+                                X        Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           FRAME_CASSINI_RADAR_2     = -82811
+           FRAME_-82811_NAME         = 'CASSINI_RADAR_2'
+           FRAME_-82811_CLASS        = 4
+           FRAME_-82811_CLASS_ID     = -82811
+           FRAME_-82811_CENTER       = -82
+           TKFRAME_-82811_SPEC       = 'ANGLES'
+           TKFRAME_-82811_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82811_ANGLES     = ( 179.15,     0.0,     0.0 )
+           TKFRAME_-82811_AXES       = (      1,       2,       3 )
+           TKFRAME_-82811_UNITS      = 'DEGREES'
+ 
+ 
+   From [44], the RADAR Beam 2 reference frame is to be adjusted to the
+   following:
+ 
+           [     ]    [        ]  [      ]  [     ]
+           [ ROT ]  = [ 179.15 ]  [ -1.2 ]  [ 0.0 ]
+           [     ]    [        ]  [      ]  [     ]
+                                X         Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_RADAR_2     = -82811
+           FRAME_-82811_NAME         = 'CASSINI_RADAR_2'
+           FRAME_-82811_CLASS        = 4
+           FRAME_-82811_CLASS_ID     = -82811
+           FRAME_-82811_CENTER       = -82
+           TKFRAME_-82811_SPEC       = 'ANGLES'
+           TKFRAME_-82811_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82811_ANGLES     = ( 179.15,    -1.2,     0.0 )
+           TKFRAME_-82811_AXES       = (      1,       2,       3 )
+           TKFRAME_-82811_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+RADAR Beam 3 (RADAR_3)
+ 
+   RADAR Beam 3 is directed nominally along the -Z axis of the spacecraft
+   frame. The following definition encapsulates this frame:
+ 
+           From [23]:
+ 
+           [     ]    [       ]  [     ]  [     ]
+           [ ROT ]  = [ 180.0 ]  [ 0.0 ]  [ 0.0 ]
+           [     ]    [       ]  [     ]  [     ]
+                               X        Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_RADAR_3     = -82812
+           FRAME_-82812_NAME         = 'CASSINI_RADAR_3'
+           FRAME_-82812_CLASS        = 4
+           FRAME_-82812_CLASS_ID     = -82812
+           FRAME_-82812_CENTER       = -82
+           TKFRAME_-82812_SPEC       = 'ANGLES'
+           TKFRAME_-82812_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82812_ANGLES     = ( 180.0,     0.0,     0.0 )
+           TKFRAME_-82812_AXES       = (     1,       2,       3 )
+           TKFRAME_-82812_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+RADAR Beam 4 (RADAR_4)
+ 
+   RADAR Beam 4 is directed nominally 0.85 degrees off of the -Z axis of the
+   spacecraft in the direction of the -Y axis of the spacecraft frame. The
+   following definition encapsulates this frame:
+ 
+           From [23]:
+ 
+           [     ]    [        ]  [     ]  [     ]
+           [ ROT ]  = [ 180.85 ]  [ 0.0 ]  [ 0.0 ]
+           [     ]    [        ]  [     ]  [     ]
+                                X        Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_RADAR_4     = -82813
+           FRAME_-82813_NAME         = 'CASSINI_RADAR_4'
+           FRAME_-82813_CLASS        = 4
+           FRAME_-82813_CLASS_ID     = -82813
+           FRAME_-82813_CENTER       = -82
+           TKFRAME_-82813_SPEC       = 'ANGLES'
+           TKFRAME_-82813_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82813_ANGLES     = ( 180.85,     0.0,     0.0 )
+           TKFRAME_-82813_AXES       = (      1,       2,       3 )
+           TKFRAME_-82813_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+   From [44], the RADAR Beam 4 reference frame is to be adjusted to the
+   following:
+ 
+           [     ]    [        ]  [      ]  [     ]
+           [ ROT ]  = [ 180.85 ]  [ -1.2 ]  [ 0.0 ]
+           [     ]    [        ]  [      ]  [     ]
+                                X         Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           \begindata
+ 
+           FRAME_CASSINI_RADAR_4     = -82813
+           FRAME_-82813_NAME         = 'CASSINI_RADAR_4'
+           FRAME_-82813_CLASS        = 4
+           FRAME_-82813_CLASS_ID     = -82813
+           FRAME_-82813_CENTER       = -82
+           TKFRAME_-82813_SPEC       = 'ANGLES'
+           TKFRAME_-82813_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82813_ANGLES     = ( 180.85,    -1.2,     0.0 )
+           TKFRAME_-82813_AXES       = (      1,       2,       3 )
+           TKFRAME_-82813_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+RADAR Beam 5 (RADAR_5)
+ 
+   RADAR Beam 5 is directed nominally 2.2 degrees off of the -Z axis of the
+   spacecraft in the direction of the -Y axis of the spacecraft frame. The
+   following definition encapsulates this frame:
+ 
+           From [23]:
+ 
+           [     ]    [       ]  [     ]  [     ]
+           [ ROT ]  = [ 182.2 ]  [ 0.0 ]  [ 0.0 ]
+           [     ]    [       ]  [     ]  [     ]
+                               X        Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_RADAR_5     = -82814
+           FRAME_-82814_NAME         = 'CASSINI_RADAR_5'
+           FRAME_-82814_CLASS        = 4
+           FRAME_-82814_CLASS_ID     = -82814
+           FRAME_-82814_CENTER       = -82
+           TKFRAME_-82814_SPEC       = 'ANGLES'
+           TKFRAME_-82814_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82814_ANGLES     = ( 182.2,     0.0,     0.0 )
+           TKFRAME_-82814_AXES       = (     1,       2,       3 )
+           TKFRAME_-82814_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+RPWS Frames
+----------------------------------------------------------
+ 
+   The RPWS antennae are located roughly on the +Y side of the Cassini
+   orbiter, while the RPWS Langmuir Probe is roughly located on the -X side.
+ 
+   Note the angles in the frame definitions are specified for the ``from
+   instrument to (relative to) base frame'' transformation.
+ 
+ 
+Radio and Plasma Wave Science (RPWS)
+ 
+   As [17] indicates, the ``collective'' RPWS boresight is nominally directed
+   along the spacecraft +Y axis. Utilizing the Euler angles specified in this
+   email, we obtain the following frame definition:
+ 
+           From [17]:
+ 
+           [     ]    [       ]  [       ]  [     ]
+           [ ROT ]  = [ 180.0 ]  [ -90.0 ]  [ 0.0 ]
+           [     ]    [       ]  [       ]  [     ]
+                               X          Y        Z
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_RPWS        = -82730
+           FRAME_-82730_NAME         = 'CASSINI_RPWS'
+           FRAME_-82730_CLASS        = 4
+           FRAME_-82730_CLASS_ID     = -82730
+           FRAME_-82730_CENTER       = -82
+           TKFRAME_-82730_SPEC       = 'ANGLES'
+           TKFRAME_-82730_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82730_ANGLES     = ( 180.0,   -90.0,     0.0 )
+           TKFRAME_-82730_AXES       = (     3,       1,       3 )
+           TKFRAME_-82730_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Radio and Plasma Wave Science Electric Antenna System (RPWS_E[AXIS][SIGN])
+ 
+   From [24]:
+ 
+   ``The RPWS electric antenna system is a triad of 10-meter conducting
+   monopoles, symmetric about the Y-Z plane. Two of the elements are extended
+   in a 120-degree "V" on either side of the magnetometer boom (i.e., the S/C
+   Y-axis) and in a plane which is rotated up from the S/C X-Y plane
+   containing the magnetometer boom by 37 degrees. These two elements are
+   referred to as the EXPLUS and EXMINUS sensors. The third element is
+   extended downward in the S/C Y-Z plane at an angle of 37 degrees from the
+   S/C +Z axis. That said, it now should be explained that the "electrical"
+   characteristics of these three antennas deviate from the physical alignment
+   and lengths of the elements due to the complex ground plane provided by the
+   spacecraft. It is these electrical characteristics that the three RPWS
+   Frame definitions RPWS_EXPLUS, RPWS_EXMINUS, and RPWS_EZPLUS are intended
+   to specify. Based upon model rheometry experiments, in which a model of the
+   Cassini Spacecraft with fully extended RPWS antennas was immersed in a tank
+   filled with an electrolytic, the following estimates have been made for the
+   electrical axes of the three antenna elements:
+ 
+           Frame                 Frame Z-Axis in CASSINI_SC_COORD "boresight"
+           ------                --------------------------------
+           RPWS_EXPLUS           [  0.91202578,  0.27709462, -0.30236989 ]
+           RPWS_EXMINUS          [ -0.91202578,  0.27709462, -0.30236989 ]
+           RPWS_EZPLUS           [ -0.01091120,  0.52089537,  0.85355080 ]
+ 
+   These numbers may change after the RPWS Jupiter Calibrations.''
+ 
+   Antenna Frame Definitions:
+ 
+           From [14]:
+ 
+           [     ]    [       ]  [        ]  [     ]
+           [ ROT ]  = [ -16.9 ]  [ -107.6 ]  [ 0.0 ]
+           [     ]    [       ]  [        ]  [     ]
+                               Z           Y        X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_RPWS_EXPLUS = -82731
+           FRAME_-82731_NAME         = 'CASSINI_RPWS_EXPLUS'
+           FRAME_-82731_CLASS        = 4
+           FRAME_-82731_CLASS_ID     = -82731
+           FRAME_-82731_CENTER       = -82
+           TKFRAME_-82731_SPEC       = 'ANGLES'
+           TKFRAME_-82731_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82731_ANGLES     = ( -16.9,  -107.6,     0.0 )
+           TKFRAME_-82731_AXES       = (     3,       2,       1 )
+           TKFRAME_-82731_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+           From [14]:
+ 
+           [     ]    [        ]  [        ]  [     ]
+           [ ROT ]  = [ -163.1 ]  [ -107.6 ]  [ 0.0 ]
+           [     ]    [        ]  [        ]  [     ]
+                                Z           Y        X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_RPWS_EXMINUS= -82732
+           FRAME_-82732_NAME         = 'CASSINI_RPWS_EXMINUS'
+           FRAME_-82732_CLASS        = 4
+           FRAME_-82732_CLASS_ID     = -82732
+           FRAME_-82732_CENTER       = -82
+           TKFRAME_-82732_SPEC       = 'ANGLES'
+           TKFRAME_-82732_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82732_ANGLES     = (-163.1,  -107.6,     0.0 )
+           TKFRAME_-82732_AXES       = (     3,       2,       1 )
+           TKFRAME_-82732_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+           From [14]:
+ 
+           [     ]    [       ]  [       ]  [     ]
+           [ ROT ]  = [ -91.2 ]  [ -31.4 ]  [ 0.0 ]
+           [     ]    [       ]  [       ]  [     ]
+                               Z          Y        X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_RPWS_EZPLUS = -82733
+           FRAME_-82733_NAME         = 'CASSINI_RPWS_EZPLUS'
+           FRAME_-82733_CLASS        = 4
+           FRAME_-82733_CLASS_ID     = -82733
+           FRAME_-82733_CENTER       = -82
+           TKFRAME_-82733_SPEC       = 'ANGLES'
+           TKFRAME_-82733_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82733_ANGLES     = ( -91.2,   -31.4,     0.0 )
+           TKFRAME_-82733_AXES       = (     3,       2,       1 )
+           TKFRAME_-82733_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
+ 
+Radio and Plasma Wave Science Langmuir Probe (RPWS_LP)
+ 
+   From [24]:
+ 
+   ``The RPWS Langmuir Probe is on the -X side of the spacecraft and can sense
+   roughly the entire hemisphere defined by the RPWS_LP Frame.''
+ 
+           From [14]:
+ 
+           [     ]    [       ]  [       ]  [     ]
+           [ ROT ]  = [ 180.0 ]  [ -90.0 ]  [ 0.0 ]
+           [     ]    [       ]  [       ]  [     ]
+                               Z          Y        X
+ 
+           where [x]  represents the rotation matrix of a given angle x about
+                    i
+           axis i.
+ 
+           Nominal Frame Definition:
+ 
+           \begindata
+ 
+           FRAME_CASSINI_RPWS_LP     = -82734
+           FRAME_-82734_NAME         = 'CASSINI_RPWS_LP'
+           FRAME_-82734_CLASS        = 4
+           FRAME_-82734_CLASS_ID     = -82734
+           FRAME_-82734_CENTER       = -82
+           TKFRAME_-82734_SPEC       = 'ANGLES'
+           TKFRAME_-82734_RELATIVE   = 'CASSINI_SC_COORD'
+           TKFRAME_-82734_ANGLES     = ( 180.0,   -90.0,     0.0 )
+           TKFRAME_-82734_AXES       = (     3,       2,       1 )
+           TKFRAME_-82734_UNITS      = 'DEGREES'
+ 
+           \begintext
+ 
diff --git a/tests/pytests/data/N1702360370_1/cpck15Dec2017.tpc b/tests/pytests/data/N1702360370_1/cpck15Dec2017.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..320214d7c46daeb7b76806db49b35bedf93d4e85
--- /dev/null
+++ b/tests/pytests/data/N1702360370_1/cpck15Dec2017.tpc
@@ -0,0 +1,6229 @@
+KPL/PCK
+
+\begindata
+   CASSINI_PCK_VERSION                        =  ( '2017-DEC-15' )
+\begintext
+
+
+P_constants (PcK) SPICE kernel file
+
+Refer to the notes at the bottom of the file for help, contacts, version history,
+references, and Cassini-specific parameter descriptions. 
+                                     
+                                     
+
+--------                                                                                                                 SUN
+ 
+      BODY10_GM		[162].
+
+      \begindata 
+      BODY10_GM  =  ( +1.327124400419e+11  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 VENUS
+ 
+      BODY2_GM		[64].
+      BODY299_GM		[162].
+
+      \begindata 
+      BODY2_GM  =  ( 324858.592000001  ) 
+      BODY299_GM  =  ( +3.248585920000e+05  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 EARTH
+ 
+      BODY3_GM		[162].
+      BODY399_GM		[162].
+
+      \begindata 
+      BODY3_GM  =  ( +4.035032355023e+05  ) 
+      BODY399_GM  =  ( +3.986004353851e+05  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 JUPITER
+ 
+      BODY5_GM		[162].
+      BODY599_GM		[107].
+
+      \begindata 
+      BODY5_GM  =  ( +1.267127641334e+08  ) 
+      BODY599_GM  =  ( +1.267127654544e+08  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 SATURN
+ 
+      BODY6_GM		[162].
+      BODY699_POLE_RA(3)		[1].
+      BODY699_POLE_RA(2)		[142].
+      BODY699_POLE_RA(1)		[162].
+      BODY699_POLE_DEC(3)		[1].
+      BODY699_POLE_DEC(2)		[142].
+      BODY699_POLE_DEC(1)		[162].
+      BODY699_JCOEF(9)		[162].
+      BODY699_JCOEF(8)		[162].
+      BODY699_JCOEF(7)		[162].
+      BODY699_JCOEF(6)		[162].
+      BODY699_JCOEF(5)		[162].
+      BODY699_JCOEF(4)		[162].
+      BODY699_JCOEF(3)		[162].
+      BODY699_JCOEF(2)		[162].
+      BODY699_JCOEF(14)		[162].
+      BODY699_JCOEF(13)		[162].
+      BODY699_JCOEF(12)		[162].
+      BODY699_JCOEF(11)		[162].
+      BODY699_JCOEF(10)		[162].
+      BODY699_JCOEF(1)		[1].
+      BODY699_GM		[162].
+      BODY699_CCOEF(3)		[1].
+      BODY699_CCOEF(2)		[1].
+      BODY699_CCOEF(1)		[1].
+
+      \begindata 
+      BODY6_GM  =  ( +3.794058443092e+07  ) 
+      BODY699_GM  =  ( +3.793120689736e+07  ) 
+      BODY699_POLE_RA  =  ( +4.058386928634e+01  ,  -3.099714786917e-02  ,  0.  ) 
+      BODY699_POLE_DEC  =  ( +8.353795862295e+01  ,  -7.584170141686e-03  ,  0.  ) 
+      BODY699_JCOEF  =  ( 0.0  ,  
+			+1.629071819646e-02  ,  
+			-1.719725091833e-07  ,  
+			-9.355171512888e-04  ,  
+			+9.385669376989e-07  ,  
+			+8.696709053146e-05  ,  
+			-2.265811401077e-06  ,  
+			-1.359656452114e-05  ,  
+			+2.810564746209e-06  ,  
+			+1.655341282022e-07  ,  
+			+2.684326453530e-07  ,  
+			-8.942151312331e-07  ,  
+			-2.123089169715e-06  ,  
+			-1.305944904496e-06  ) 
+      BODY699_CCOEF  =  ( 0.0  ,  0.0  ,  0.0000000000000  ) 
+      BODY699_SCOEF  =  ( 0.0  ,  0.0  ,  0.00000000  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 URANUS
+ 
+      BODY7_GM		[162].
+
+      \begindata 
+      BODY7_GM  =  ( +5.794556465752e+06  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 MOON
+ 
+      BODY301_GM		[162].
+
+      \begindata 
+      BODY301_GM  =  ( +4.902800117136e+03  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 MIMAS
+ 
+      BODY601_GM		[158].
+
+      \begindata 
+      BODY601_GM  =  ( +2.502817739550e+00  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 ENCELADUS
+ 
+      BODY602_JCOEF(2)		[142].
+      BODY602_JCOEF(1)		[23].
+      BODY602_GM		[158].
+      BODY602_CCOEF(3)		[142].
+      BODY602_CCOEF(2)		[23].
+      BODY602_CCOEF(1)		[23].
+
+      \begindata 
+      BODY602_GM  =  ( +7.211777492985e+00  ) 
+      BODY602_JCOEF  =  ( 0.0  ,  +5.435200000000e-03  ) 
+      BODY602_CCOEF  =  ( 0.0  ,  0.0  ,  +1.549800000000e-03  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 TETHYS
+ 
+      BODY603_GM		[162].
+
+      \begindata 
+      BODY603_GM  =  ( +4.120850186975e+01  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 DIONE
+ 
+      BODY604_JCOEF(3)		[23].
+      BODY604_JCOEF(2)		[142].
+      BODY604_JCOEF(1)		[23].
+      BODY604_GM		[162].
+      BODY604_CCOEF(3)		[142].
+      BODY604_CCOEF(2)		[23].
+      BODY604_CCOEF(1)		[23].
+
+      \begindata 
+      BODY604_GM  =  ( +7.311605842130e+01  ) 
+      BODY604_JCOEF  =  ( 0.0  ,  +1.436865258838e-03  ) 
+      BODY604_CCOEF  =  ( 0.0  ,  0.0  ,  +3.651494811184e-04  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 RHEA
+ 
+      BODY605_JCOEF(3)		[23].
+      BODY605_JCOEF(2)		[142].
+      BODY605_JCOEF(1)		[23].
+      BODY605_GM		[162].
+      BODY605_CCOEF(3)		[142].
+      BODY605_CCOEF(2)		[23].
+      BODY605_CCOEF(1)		[23].
+
+      \begindata 
+      BODY605_GM  =  ( +1.539500870013e+02  ) 
+      BODY605_JCOEF  =  ( 0.0  ,  +9.496088222042e-04  ) 
+      BODY605_CCOEF  =  ( 0.0  ,  0.0  ,  +2.366835799998e-04  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 TITAN
+ 
+      BODY606_SCOEF(3)		[152].
+      BODY606_SCOEF(2)		[41].
+      BODY606_SCOEF(1)		[41].
+      BODY606_JCOEF(2)		[152].
+      BODY606_JCOEF(1)		[41].
+      BODY606_GM		[162].
+      BODY606_CCOEF(3)		[152].
+      BODY606_CCOEF(2)		[41].
+      BODY606_CCOEF(1)		[41].
+
+      \begindata 
+      BODY606_GM  =  ( +8.978130958559e+03  ) 
+      BODY606_JCOEF  =  ( 0.0  ,  +3.341349498806e-05  ) 
+      BODY606_CCOEF  =  ( 0.0  ,  0.0  ,  +1.046258225998e-05  ) 
+      BODY606_SCOEF  =  ( 0.0  ,  0.0  ,  +3.915574411619e-07  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 HYPERION
+ 
+      BODY607_GM		[158].
+
+      \begindata 
+      BODY607_GM  =  ( +3.713685396357e-01  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 IAPETUS
+ 
+      BODY608_GM		[162].
+
+      \begindata 
+      BODY608_GM  =  ( +1.204890219402e+02  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+--------                                                                                                                 PHOEBE
+ 
+      BODY609_GM		[158].
+
+      \begindata 
+      BODY609_GM  =  ( +5.527094668508e-01  ) 
+
+      \begintext 
+                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
+
+
+         Note that GM values >= 1.0 are packaged as is into 7CONIC_VEC 
+         commands for AACS to propagate the body's ephemeris. 
+         For GM values < 1.0, the value in the G_MASS parameter 
+         of the 7CONIC_VEC command is set to 1.0.  One is the minimum 
+         value for the G_MASS parameter. The resetting of the G_MASS 
+         parameter to the minimum acceptable where the actual 
+         GM is < 1.0 is acceptable since Cassini will not pass close enough 
+         to any of the affected bodies for the gravitational mass 
+         to have an effect.
+         
+
+--------                                                                                                                 CONSTANTS AND NOTES FOR CASPER USERS
+
+
+         \begindata
+         BODY601_GM/PRIMARY  =  (              6.59087D-08             )
+         BODY602_GM/PRIMARY  =  (              1.29181D-07             )
+         BODY603_GM/PRIMARY  =  (              1.1022D-06              )
+         BODY604_GM/PRIMARY  =  (              1.92865D-06             )
+         BODY605_GM/PRIMARY  =  (              4.05998D-06             )
+         BODY606_GM/PRIMARY  =  (              2.36697D-04             )
+         BODY607_GM/PRIMARY  =  (              2.60998D-08             )
+         BODY608_GM/PRIMARY  =  (              2.79453D-06             )
+         BODY609_GM/PRIMARY  =  (              1.26545D-08             )
+         BODY610_GM/PRIMARY  =  (              3.38507D-09             )
+         BODY611_GM/PRIMARY  =  (              9.41176D-10             )
+         BODY612_GM/PRIMARY  =  (              4.48179D-11             )
+         BODY613_GM/PRIMARY  =  (              1.26545D-11            )
+         BODY614_GM/PRIMARY  =  (              6.32723D-12            )
+         BODY615_GM/PRIMARY  =  (              1.89817D-11             )
+         BODY616_GM/PRIMARY  =  (              5.79996D-10             )
+         BODY617_GM/PRIMARY  =  (              3.42725D-10             )
+         BODY618_GM/PRIMARY  =  (              4.74543D-12             )
+         \begintext
+         
+--------                                                                                                                 URLS AND CONTACTS
+
+
+Description of PCK format and contents can be found in NAIF's PCK "required
+reading" document, at:
+
+ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/ascii/individual_docs/pck.req
+
+
+NAIF tutorial on PCK formatting and use at:
+
+ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/Tutorials/office/individual_docs/16_pck.ppt
+ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/Tutorials/office/packages/
+SPICE_Tutorials_Office.zip
+
+
+The Cassini PCK & ephemeris files can be found on the DOM, and at:
+
+ftp://naif.jpl.nasa.gov/pub/naif/CASSINI/kernels/
+
+
+Questions regarding this file can be directed to:
+
+Adrian Tinio (818)393-5995 Adrian.Tinio@jpl.nasa.gov
+ 
+
+ 
+
+ 
+
+ 
+--------                         VERSION HISTORY
+
+2017-Dec-15 (published)
+Automated Process
+
+Applicable current Ephemeris = 171214R_SCPSE_17224_17258.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170915_1_288GF
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY603_GM            +4.120850186975e+01    +4.120850186975e+01
+BODY604_GM            +7.311605842130e+01    +7.311605842130e+01
+BODY605_GM            +1.539500870013e+02    +1.539500870013e+02
+BODY606_GM            +8.978130958559e+03    +8.978130958559e+03
+BODY608_GM            +1.204890219402e+02    +1.204890219402e+02
+BODY699_GM            +3.793120689736e+07    +3.793120689736e+07
+BODY699_JCOEF(10)     +3.786000947517e-06    +1.655341282022e-07
+BODY699_JCOEF(11)     +6.616273947210e-08    +2.684326453530e-07
+BODY699_JCOEF(12)     -2.311925417381e-06    -8.942151312331e-07
+BODY699_JCOEF(13)     -6.130127942069e-08    -2.123089169715e-06
+BODY699_JCOEF(14)     -1.163170055382e-06    -1.305944904496e-06
+BODY699_JCOEF(2)      +1.629057982688e-02    +1.629071819646e-02
+BODY699_JCOEF(3)      +2.884389291908e-07    -1.719725091833e-07
+BODY699_JCOEF(4)      -9.353674705844e-04    -9.355171512888e-04
+BODY699_JCOEF(5)      +4.643582928107e-08    +9.385669376989e-07
+BODY699_JCOEF(6)      +8.614756119106e-05    +8.696709053146e-05
+BODY699_JCOEF(7)      +5.084433057059e-07    -2.265811401077e-06
+BODY699_JCOEF(8)      -1.508059888260e-05    -1.359656452114e-05
+BODY699_JCOEF(9)      +8.338320981889e-07    +2.810564746209e-06
+BODY699_POLE_DEC(1)   +8.353795996624e+01    +8.353795862295e+01
+BODY699_POLE_RA(1)    +4.058384124232e+01    +4.058386928634e+01
+BODY6_GM              +3.794058443092e+07    +3.794058443092e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2017-Oct-31 (published)
+Automated Process
+
+Applicable current Ephemeris = 171031R_SCPSE_17177_17226.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170813_281GF
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY603_GM            +4.120850186975e+01    +4.120850186975e+01
+BODY604_GM            +7.311605842130e+01    +7.311605842130e+01
+BODY605_GM            +1.539500870013e+02    +1.539500870013e+02
+BODY606_GM            +8.978130958559e+03    +8.978130958559e+03
+BODY608_GM            +1.204890219402e+02    +1.204890219402e+02
+BODY699_GM            +3.793120689736e+07    +3.793120689736e+07
+BODY699_JCOEF(10)     +3.748382572185e-06    +3.786000947517e-06
+BODY699_JCOEF(11)     +2.886182422314e-08    +6.616273947210e-08
+BODY699_JCOEF(12)     -2.332907321960e-06    -2.311925417381e-06
+BODY699_JCOEF(13)     -8.423790343048e-08    -6.130127942069e-08
+BODY699_JCOEF(14)     -1.172747659727e-06    -1.163170055382e-06
+BODY699_JCOEF(2)      +1.629056935466e-02    +1.629057982688e-02
+BODY699_JCOEF(3)      +2.965003945711e-07    +2.884389291908e-07
+BODY699_JCOEF(4)      -9.353714329544e-04    -9.353674705844e-04
+BODY699_JCOEF(5)      +4.685956775618e-09    +4.643582928107e-08
+BODY699_JCOEF(6)      +8.610467107942e-05    +8.614756119106e-05
+BODY699_JCOEF(7)      +4.738809141506e-07    +5.084433057059e-07
+BODY699_JCOEF(8)      -1.511356193045e-05    -1.508059888260e-05
+BODY699_JCOEF(9)      +8.047857413151e-07    +8.338320981889e-07
+BODY699_POLE_DEC(1)   +8.353796209170e+01    +8.353795996624e+01
+BODY699_POLE_RA(1)    +4.058381078301e+01    +4.058384124232e+01
+BODY6_GM              +3.794058443092e+07    +3.794058443092e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2017-Oct-30 (published)
+Automated Process
+
+Applicable current Ephemeris = 171024R_SCPSE_17146_17177.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170714_276GF
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY603_GM            +4.120850186975e+01    +4.120850186975e+01
+BODY604_GM            +7.311605842130e+01    +7.311605842130e+01
+BODY605_GM            +1.539500870013e+02    +1.539500870013e+02
+BODY606_GM            +8.978130958559e+03    +8.978130958559e+03
+BODY608_GM            +1.204890219402e+02    +1.204890219402e+02
+BODY699_GM            +3.793120689736e+07    +3.793120689736e+07
+BODY699_JCOEF(10)     +3.641907938036e-06    +3.748382572185e-06
+BODY699_JCOEF(11)     -1.155312580876e-08    +2.886182422314e-08
+BODY699_JCOEF(12)     -2.437044743424e-06    -2.332907321960e-06
+BODY699_JCOEF(13)     -1.120617107914e-07    -8.423790343048e-08
+BODY699_JCOEF(14)     -1.219002171382e-06    -1.172747659727e-06
+BODY699_JCOEF(2)      +1.629057491353e-02    +1.629056935466e-02
+BODY699_JCOEF(3)      +2.833112343228e-07    +2.965003945711e-07
+BODY699_JCOEF(4)      -9.354181192562e-04    -9.353714329544e-04
+BODY699_JCOEF(5)      +1.110932646324e-08    +4.685956775618e-09
+BODY699_JCOEF(6)      +8.607405457832e-05    +8.610467107942e-05
+BODY699_JCOEF(7)      +4.545482178452e-07    +4.738809141506e-07
+BODY699_JCOEF(8)      -1.520674082639e-05    -1.511356193045e-05
+BODY699_JCOEF(9)      +7.664061761364e-07    +8.047857413151e-07
+BODY699_POLE_DEC(1)   +8.353796123271e+01    +8.353796209170e+01
+BODY699_POLE_RA(1)    +4.058382745190e+01    +4.058381078301e+01
+BODY6_GM              +3.794058443092e+07    +3.794058443092e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2017-Oct-21 (published)
+Automated Process
+
+Applicable current Ephemeris = 171017R_SCPSE_17117_17146.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170608_271GF
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY603_GM            +4.120850186975e+01    +4.120850186975e+01
+BODY604_GM            +7.311605842130e+01    +7.311605842130e+01
+BODY605_GM            +1.539500870013e+02    +1.539500870013e+02
+BODY606_GM            +8.978130958559e+03    +8.978130958559e+03
+BODY608_GM            +1.204890219402e+02    +1.204890219402e+02
+BODY699_GM            +3.793120689736e+07    +3.793120689736e+07
+BODY699_JCOEF(2)      +1.629090771061e-02    +1.629057491353e-02
+BODY699_JCOEF(3)      +0.000000000000e+00    +2.833112343228e-07
+BODY699_JCOEF(4)      -9.338214217045e-04    -9.354181192562e-04
+BODY699_JCOEF(5)      +0.000000000000e+00    +1.110932646324e-08
+BODY699_JCOEF(6)      +8.325055333031e-05    +8.607405457832e-05
+BODY699_JCOEF(7)      +0.000000000000e+00    +4.545482178452e-07
+BODY699_JCOEF(8)      +0.000000000000e+00    -1.520674082639e-05
+BODY699_JCOEF(9)      +0.000000000000e+00    +7.664061761364e-07
+BODY699_JCOEF(10)     +0.000000000000e+00    +3.641907938036e-06
+BODY699_JCOEF(11)     +0.000000000000e+00    -1.155312580876e-08
+BODY699_JCOEF(12)     +0.000000000000e+00    -2.437044743424e-06
+BODY699_JCOEF(13)     +0.000000000000e+00    -1.120617107914e-07
+BODY699_JCOEF(14)     +0.000000000000e+00    -1.219002171382e-06
+BODY699_POLE_DEC(1)   +8.353795895203e+01    +8.353796123271e+01
+BODY699_POLE_RA(1)    +4.058386992768e+01    +4.058382745190e+01
+BODY6_GM              +3.794058443092e+07    +3.794058443092e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2017-Aug-14 (published)
+Automated Process
+
+Applicable current Ephemeris = 170811R_SCPSE_17104_17117.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170507_269GF
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY601_GM            +2.504168531168e+00    +2.502817739550e+00
+BODY602_GM            +7.210642146844e+00    +7.211777492985e+00
+BODY603_GM            +4.120886351384e+01    +4.120850186975e+01
+BODY604_GM            +7.311578204704e+01    +7.311605842130e+01
+BODY605_GM            +1.539457695021e+02    +1.539500870013e+02
+BODY606_GM            +8.978136802358e+03    +8.978130958559e+03
+BODY607_GM            +3.716779497898e-01    +3.713685396357e-01
+BODY608_GM            +1.205406980395e+02    +1.204890219402e+02
+BODY609_GM            +5.480161786740e-01    +5.527094668508e-01
+BODY699_GM            +3.793120689522e+07    +3.793120689736e+07
+BODY699_JCOEF(2)      +1.629055618674e-02    +1.629090771061e-02
+BODY699_JCOEF(4)      -9.366851917272e-04    -9.338214217045e-04
+BODY699_JCOEF(6)      +8.280896942075e-05    +8.325055333031e-05
+BODY699_POLE_DEC(1)   +8.353795234454e+01    +8.353795895203e+01
+BODY699_POLE_RA(1)    +4.058613626293e+01    +4.058386992768e+01
+BODY6_GM              +3.794058447810e+07    +3.794058443092e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2017-Jul-25 (published)
+Automated Process
+
+Applicable current Ephemeris = 170720R_SCPSE_17061_17104.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170421_264T126
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY601_GM            +2.504081870687e+00    +2.504168531168e+00
+BODY602_GM            +7.210772616182e+00    +7.210642146844e+00
+BODY603_GM            +4.120887177496e+01    +4.120886351384e+01
+BODY604_GM            +7.311572411683e+01    +7.311578204704e+01
+BODY605_GM            +1.539444655259e+02    +1.539457695021e+02
+BODY606_GM            +8.978138039097e+03    +8.978136802358e+03
+BODY607_GM            +3.716711120483e-01    +3.716779497898e-01
+BODY608_GM            +1.205402752867e+02    +1.205406980395e+02
+BODY609_GM            +5.505747898310e-01    +5.480161786740e-01
+BODY699_GM            +3.793120741278e+07    +3.793120689522e+07
+BODY699_JCOEF(2)      +1.629053435909e-02    +1.629055618674e-02
+BODY699_JCOEF(4)      -9.373092086599e-04    -9.366851917272e-04
+BODY699_JCOEF(6)      +7.540511809128e-05    +8.280896942075e-05
+BODY699_POLE_DEC(1)   +8.353795237942e+01    +8.353795234454e+01
+BODY699_POLE_RA(1)    +4.058613580121e+01    +4.058613626293e+01
+BODY6_GM              +3.794058499768e+07    +3.794058447810e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2017-May-09 (published)
+Automated Process
+
+Applicable current Ephemeris = 170509R_SCPSE_16363_17061.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170423_254T126
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY601_GM            +2.503522356085e+00    +2.504081870687e+00
+BODY602_GM            +7.211029015103e+00    +7.210772616182e+00
+BODY603_GM            +4.120902759359e+01    +4.120887177496e+01
+BODY604_GM            +7.311571724805e+01    +7.311572411683e+01
+BODY605_GM            +1.539445703042e+02    +1.539444655259e+02
+BODY606_GM            +8.978134397405e+03    +8.978138039097e+03
+BODY607_GM            +3.713890479231e-01    +3.716711120483e-01
+BODY608_GM            +1.205778163298e+02    +1.205402752867e+02
+BODY609_GM            +5.537034401022e-01    +5.505747898310e-01
+BODY699_GM            +3.793120714676e+07    +3.793120741278e+07
+BODY699_JCOEF(2)      +1.629088427394e-02    +1.629053435909e-02
+BODY699_JCOEF(4)      -9.337629884495e-04    -9.373092086599e-04
+BODY699_JCOEF(6)      +7.614739101940e-05    +7.540511809128e-05
+BODY699_POLE_DEC(1)   +8.353795251735e+01    +8.353795237942e+01
+BODY699_POLE_RA(1)    +4.058611775960e+01    +4.058613580121e+01
+BODY6_GM              +3.794058476830e+07    +3.794058499768e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2017-Mar-27 (published)
+Automated Process
+
+Applicable current Ephemeris = 170323R_SCPSE_16329_16363.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170105_251T126
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY601_GM            +2.503458199931e+00    +2.503522356085e+00
+BODY602_GM            +7.211216857327e+00    +7.211029015103e+00
+BODY603_GM            +4.120862437003e+01    +4.120902759359e+01
+BODY604_GM            +7.311579178242e+01    +7.311571724805e+01
+BODY605_GM            +1.539424333799e+02    +1.539445703042e+02
+BODY606_GM            +8.978137827385e+03    +8.978134397405e+03
+BODY607_GM            +3.713969352243e-01    +3.713890479231e-01
+BODY608_GM            +1.204756561849e+02    +1.205778163298e+02
+BODY609_GM            +5.533648326496e-01    +5.537034401022e-01
+BODY699_GM            +3.793120704269e+07    +3.793120714676e+07
+BODY699_JCOEF(2)      +1.629098177296e-02    +1.629088427394e-02
+BODY699_JCOEF(4)      -9.313711046683e-04    -9.337629884495e-04
+BODY699_JCOEF(6)      +8.878694316872e-05    +7.614739101940e-05
+BODY699_POLE_DEC(1)   +8.353809821829e+01    +8.353795251735e+01
+BODY699_POLE_RA(1)    +4.058409635443e+01    +4.058611775960e+01
+BODY6_GM              +3.794058456266e+07    +3.794058476830e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2017-Mar-20 (published)
+Automated Process
+
+Applicable current Ephemeris = 170315R_SCPSE_16310_16329.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 161202_1_249T125
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY601_GM            +2.503429819565e+00    +2.503458199931e+00
+BODY602_GM            +7.211263331665e+00    +7.211216857327e+00
+BODY603_GM            +4.120807865783e+01    +4.120862437003e+01
+BODY604_GM            +7.311565440283e+01    +7.311579178242e+01
+BODY605_GM            +1.539422768490e+02    +1.539424333799e+02
+BODY606_GM            +8.978138421746e+03    +8.978137827385e+03
+BODY607_GM            +3.713250481181e-01    +3.713969352243e-01
+BODY608_GM            +1.205443628610e+02    +1.204756561849e+02
+BODY609_GM            +5.541420472080e-01    +5.533648326496e-01
+BODY699_GM            +3.793120752586e+07    +3.793120704269e+07
+BODY699_JCOEF(2)      +1.629105265841e-02    +1.629098177296e-02
+BODY699_JCOEF(4)      -9.307532830389e-04    -9.313711046683e-04
+BODY699_JCOEF(6)      +8.821178266851e-05    +8.878694316872e-05
+BODY699_POLE_DEC(1)   +8.353813668628e+01    +8.353809821829e+01
+BODY699_POLE_RA(1)    +4.058322932675e+01    +4.058409635443e+01
+BODY6_GM              +3.794058511503e+07    +3.794058456266e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2017-Mar-01 (published)
+Automated Process
+
+Applicable current Ephemeris = 170301R_SCPSE_16282_16310.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 161116_246T124
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY601_GM            +2.503458199931e+00    +2.503429819565e+00
+BODY602_GM            +7.211438886407e+00    +7.211263331665e+00
+BODY603_GM            +4.120859857122e+01    +4.120807865783e+01
+BODY604_GM            +7.311579502939e+01    +7.311565440283e+01
+BODY605_GM            +1.539421951727e+02    +1.539422768490e+02
+BODY606_GM            +8.978136177723e+03    +8.978138421746e+03
+BODY607_GM            +3.713209987014e-01    +3.713250481181e-01
+BODY608_GM            +1.205222816678e+02    +1.205443628610e+02
+BODY609_GM            +5.540640303818e-01    +5.541420472080e-01
+BODY699_GM            +3.793120731501e+07    +3.793120752586e+07
+BODY699_JCOEF(2)      +1.629113494099e-02    +1.629105265841e-02
+BODY699_JCOEF(4)      -9.300312200208e-04    -9.307532830389e-04
+BODY699_JCOEF(6)      +8.990159020464e-05    +8.821178266851e-05
+BODY699_POLE_DEC(1)   +8.353813708379e+01    +8.353813668628e+01
+BODY699_POLE_RA(1)    +4.058321003407e+01    +4.058322932675e+01
+BODY6_GM              +3.794058488055e+07    +3.794058511503e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2017-Feb-28 (published)
+Automated Process
+
+Applicable current Ephemeris = 170228R_SCPSE_16262_16282.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 161019_244T124
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY602_GM            +7.211357133168e+00    +7.211438886407e+00
+BODY603_GM            +4.120838587263e+01    +4.120859857122e+01
+BODY604_GM            +7.311580066353e+01    +7.311579502939e+01
+BODY605_GM            +1.539433188040e+02    +1.539421951727e+02
+BODY606_CCOEF(3)      +1.029534469634e-05    +1.046258225998e-05
+BODY606_GM            +8.978132593546e+03    +8.978136177723e+03
+BODY606_JCOEF(2)      +3.546380755853e-05    +3.341349498806e-05
+BODY606_SCOEF(3)      +2.322168281218e-07    +3.915574411619e-07
+BODY607_GM            +3.714099091721e-01    +3.713209987014e-01
+BODY608_GM            +1.204848222541e+02    +1.205222816678e+02
+BODY609_GM            +5.553928427732e-01    +5.540640303818e-01
+BODY699_GM            +3.793120718935e+07    +3.793120731501e+07
+BODY699_JCOEF(2)      +1.629106986990e-02    +1.629113494099e-02
+BODY699_JCOEF(4)      -9.307706047161e-04    -9.300312200208e-04
+BODY699_JCOEF(6)      +8.839867540967e-05    +8.990159020464e-05
+BODY699_POLE_DEC(1)   +8.353812798747e+01    +8.353813708379e+01
+BODY699_POLE_RA(1)    +4.058378023140e+01    +4.058321003407e+01
+BODY6_GM              +3.794058471609e+07    +3.794058488055e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2016-Dec-15 (published)
+Automated Process
+
+Applicable current Ephemeris = 161214R_SCPSE_16217_16262.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160926_240T123
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY602_GM            +7.211402764994e+00    +7.211357133168e+00
+BODY603_GM            +4.120828173203e+01    +4.120838587263e+01
+BODY604_GM            +7.311578550158e+01    +7.311580066353e+01
+BODY605_GM            +1.539427209498e+02    +1.539433188040e+02
+BODY606_CCOEF(3)      +1.035135894910e-05    +1.029534469634e-05
+BODY606_GM            +8.978131430064e+03    +8.978132593546e+03
+BODY606_JCOEF(2)      +3.453993520201e-05    +3.546380755853e-05
+BODY606_SCOEF(3)      -1.328779671011e-08    +2.322168281218e-07
+BODY607_GM            +3.713269422707e-01    +3.714099091721e-01
+BODY608_GM            +1.205497924859e+02    +1.204848222541e+02
+BODY609_GM            +5.540358787579e-01    +5.553928427732e-01
+BODY699_GM            +3.793120736644e+07    +3.793120718935e+07
+BODY699_JCOEF(2)      +1.629111982374e-02    +1.629106986990e-02
+BODY699_JCOEF(4)      -9.300983689047e-04    -9.307706047161e-04
+BODY699_JCOEF(6)      +9.027570812799e-05    +8.839867540967e-05
+BODY699_POLE_DEC(1)   +8.353813363065e+01    +8.353812798747e+01
+BODY699_POLE_RA(1)    +4.058357784587e+01    +4.058378023140e+01
+BODY6_GM              +3.794058495488e+07    +3.794058471609e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2016-Dec-12 (published)
+Automated Process
+
+Applicable current Ephemeris = 161208R_SCPSE_16201_16217.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160810_1_239T122
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY602_GM            +7.211703581579e+00    +7.211402764994e+00
+BODY603_GM            +4.120843806343e+01    +4.120828173203e+01
+BODY604_GM            +7.311584179385e+01    +7.311578550158e+01
+BODY605_GM            +1.539428752140e+02    +1.539427209498e+02
+BODY606_CCOEF(3)      +1.046258225998e-05    +1.035135894910e-05
+BODY606_GM            +8.978134655522e+03    +8.978131430064e+03
+BODY606_JCOEF(2)      +3.341349498806e-05    +3.453993520201e-05
+BODY606_SCOEF(3)      +3.915574411619e-07    -1.328779671011e-08
+BODY607_GM            +3.713075782150e-01    +3.713269422707e-01
+BODY608_GM            +1.204605259223e+02    +1.205497924859e+02
+BODY609_GM            +5.527880806141e-01    +5.540358787579e-01
+BODY699_GM            +3.793120695506e+07    +3.793120736644e+07
+BODY699_JCOEF(2)      +1.629112234313e-02    +1.629111982374e-02
+BODY699_JCOEF(4)      -9.297728263461e-04    -9.300983689047e-04
+BODY699_JCOEF(6)      +9.114243475253e-05    +9.027570812799e-05
+BODY699_POLE_DEC(1)   +8.353815470019e+01    +8.353813363065e+01
+BODY699_POLE_RA(1)    +4.058303844662e+01    +4.058357784587e+01
+BODY6_GM              +3.794058445686e+07    +3.794058495488e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2016-Nov-17 (published)
+Automated Process
+
+Applicable current Ephemeris = 161117R_SCPSE_16146_16201.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160724_237T121
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY601_GM            +2.503448868242e+00    +2.503458199931e+00
+BODY602_GM            +7.211325894096e+00    +7.211703581579e+00
+BODY603_GM            +4.120847806547e+01    +4.120843806343e+01
+BODY604_GM            +7.311570926715e+01    +7.311584179385e+01
+BODY605_GM            +1.539423683108e+02    +1.539428752140e+02
+BODY606_GM            +8.978134339426e+03    +8.978134655522e+03
+BODY607_GM            +3.713244675027e-01    +3.713075782150e-01
+BODY608_GM            +1.205322393914e+02    +1.204605259223e+02
+BODY609_GM            +5.543646426583e-01    +5.527880806141e-01
+BODY699_GM            +3.793120700538e+07    +3.793120695506e+07
+BODY699_JCOEF(2)      +1.629108871238e-02    +1.629112234313e-02
+BODY699_JCOEF(4)      -9.304882330717e-04    -9.297728263461e-04
+BODY699_JCOEF(6)      +8.885094992101e-05    +9.114243475253e-05
+BODY699_POLE_DEC(1)   +8.353800243639e+01    +8.353815470019e+01
+BODY699_POLE_RA(1)    +4.058439605750e+01    +4.058303844662e+01
+BODY6_GM              +3.794058457925e+07    +3.794058445686e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2016-Aug-26 (published)
+Automated Process
+
+Applicable current Ephemeris = 160725R_SCPSE_16115_16146.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160606_236T120
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY601_GM            +2.503458199931e+00    +2.503448868242e+00
+BODY602_GM            +7.211471999477e+00    +7.211325894096e+00
+BODY603_GM            +4.120844755642e+01    +4.120847806547e+01
+BODY604_GM            +7.311575497245e+01    +7.311570926715e+01
+BODY605_GM            +1.539425188714e+02    +1.539423683108e+02
+BODY606_GM            +8.978136440086e+03    +8.978134339426e+03
+BODY607_GM            +3.712817316551e-01    +3.713244675027e-01
+BODY608_GM            +1.205098029896e+02    +1.205322393914e+02
+BODY609_GM            +5.531710748936e-01    +5.543646426583e-01
+BODY699_GM            +3.793120705906e+07    +3.793120700538e+07
+BODY699_JCOEF(2)      +1.629111447570e-02    +1.629108871238e-02
+BODY699_JCOEF(4)      -9.301241563302e-04    -9.304882330717e-04
+BODY699_JCOEF(6)      +8.990943846005e-05    +8.885094992101e-05
+BODY699_POLE_DEC(1)   +8.353805038622e+01    +8.353800243639e+01
+BODY699_POLE_RA(1)    +4.058378246620e+01    +4.058439605750e+01
+BODY6_GM              +3.794058461162e+07    +3.794058457925e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2016-Jul-20 (published)
+Automated Process
+
+Applicable current Ephemeris = 160718R_SCPSE_16088_16115.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160504_235T119
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY602_GM            +7.211185066510e+00    +7.211471999477e+00
+BODY603_GM            +4.120856508659e+01    +4.120844755642e+01
+BODY604_GM            +7.311574218947e+01    +7.311575497245e+01
+BODY605_GM            +1.539419035933e+02    +1.539425188714e+02
+BODY606_GM            +8.978137030984e+03    +8.978136440086e+03
+BODY607_GM            +3.712085754472e-01    +3.712817316551e-01
+BODY608_GM            +1.205095752389e+02    +1.205098029896e+02
+BODY609_GM            +5.532371285376e-01    +5.531710748936e-01
+BODY699_GM            +3.793120723494e+07    +3.793120705906e+07
+BODY699_JCOEF(2)      +1.629111964057e-02    +1.629111447570e-02
+BODY699_JCOEF(4)      -9.305945887740e-04    -9.301241563302e-04
+BODY699_JCOEF(6)      +8.872819837009e-05    +8.990943846005e-05
+BODY699_POLE_DEC(1)   +8.353776999027e+01    +8.353805038622e+01
+BODY699_POLE_RA(1)    +4.058252338374e+01    +4.058378246620e+01
+BODY6_GM              +3.794058478705e+07    +3.794058461162e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2016-Jun-08 (published)
+Automated Process
+
+Applicable current Ephemeris = 160608R_SCPSE_16041_16088.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160405_233T118
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY603_GM            +4.120856508659e+01    +4.120856508659e+01
+BODY604_GM            +7.311574218947e+01    +7.311574218947e+01
+BODY605_GM            +1.539419035933e+02    +1.539419035933e+02
+BODY606_GM            +8.978137030984e+03    +8.978137030984e+03
+BODY608_GM            +1.205095752389e+02    +1.205095752389e+02
+BODY699_GM            +3.793120723494e+07    +3.793120723494e+07
+BODY699_POLE_DEC(1)   +8.353776999027e+01    +8.353776999027e+01
+BODY699_POLE_RA(1)    +4.058252338374e+01    +4.058252338374e+01
+BODY6_GM              +3.794058478705e+07    +3.794058478705e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2016-May-20 (published)
+Automated Process
+
+Applicable current Ephemeris = 160519R_SCPSE_16025_16041.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160218_232T117
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY603_GM            +4.120856508659e+01    +4.120856508659e+01
+BODY604_GM            +7.311574218947e+01    +7.311574218947e+01
+BODY605_GM            +1.539419035933e+02    +1.539419035933e+02
+BODY606_GM            +8.978137030984e+03    +8.978137030984e+03
+BODY608_GM            +1.205095752389e+02    +1.205095752389e+02
+BODY699_GM            +3.793120723494e+07    +3.793120723494e+07
+BODY699_POLE_DEC(1)   +8.353776999027e+01    +8.353776999027e+01
+BODY699_POLE_RA(1)    +4.058252338374e+01    +4.058252338374e+01
+BODY6_GM              +3.794058478705e+07    +3.794058478705e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2016-Apr-13 (published)
+Automated Process
+
+Applicable current Ephemeris = 160413R_SCPSE_16007_16025.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160203_231T116
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY603_GM            +4.120856508659e+01    +4.120856508659e+01
+BODY604_GM            +7.311574218947e+01    +7.311574218947e+01
+BODY605_GM            +1.539419035933e+02    +1.539419035933e+02
+BODY606_GM            +8.978137030984e+03    +8.978137030984e+03
+BODY608_GM            +1.205095752389e+02    +1.205095752389e+02
+BODY699_GM            +3.793120723494e+07    +3.793120723494e+07
+BODY699_POLE_DEC(1)   +8.353776999027e+01    +8.353776999027e+01
+BODY699_POLE_RA(1)    +4.058252338374e+01    +4.058252338374e+01
+BODY6_GM              +3.794058478705e+07    +3.794058478705e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2016-Mar-30 (published)
+Automated Process
+
+Applicable current Ephemeris = 160330R_SCPSE_15347_16007.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160118_229T115
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400419e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800117136e+03    +4.902800117136e+03
+BODY399_GM            +3.986004353851e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641334e+08    +1.267127641334e+08
+BODY603_GM            +4.120856508659e+01    +4.120856508659e+01
+BODY604_GM            +7.311574218947e+01    +7.311574218947e+01
+BODY605_GM            +1.539419035933e+02    +1.539419035933e+02
+BODY606_GM            +8.978137030984e+03    +8.978137030984e+03
+BODY608_GM            +1.205095752389e+02    +1.205095752389e+02
+BODY699_GM            +3.793120723494e+07    +3.793120723494e+07
+BODY699_POLE_DEC(1)   +8.353776999027e+01    +8.353776999027e+01
+BODY699_POLE_RA(1)    +4.058252338374e+01    +4.058252338374e+01
+BODY6_GM              +3.794058478705e+07    +3.794058478705e+07
+BODY7_GM              +5.794556465752e+06    +5.794556465752e+06
+
+2016-Mar-24 (published)
+Automated Process
+
+Applicable current Ephemeris = 160323R_SCPSE_15310_15347.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 151222_226E22
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327132332639e+11    +1.327124400419e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800117136e+03
+BODY399_GM            +3.986004354361e+05    +3.986004353851e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY5_GM              +1.267127641000e+08    +1.267127641334e+08
+BODY601_GM            +2.503523763302e+00    +2.503458199931e+00
+BODY602_CCOEF(3)      +1.229502218138e-03    +1.549800000000e-03
+BODY602_GM            +7.211176947682e+00    +7.211185066510e+00
+BODY602_JCOEF(2)      +6.055594538600e-03    +5.435200000000e-03
+BODY603_GM            +4.121082693902e+01    +4.120856508659e+01
+BODY604_CCOEF(3)      +3.858211235156e-04    +3.651494811184e-04
+BODY604_GM            +7.311671566552e+01    +7.311574218947e+01
+BODY604_JCOEF(2)      +1.294156214342e-03    +1.436865258838e-03
+BODY605_CCOEF(3)      +2.548409590520e-04    +2.366835799998e-04
+BODY605_GM            +1.539427914458e+02    +1.539419035933e+02
+BODY605_JCOEF(2)      +8.496490377952e-04    +9.496088222042e-04
+BODY606_CCOEF(3)      +9.968773423301e-06    +1.046258225998e-05
+BODY606_GM            +8.978137900462e+03    +8.978137030984e+03
+BODY606_JCOEF(2)      +3.267536300237e-05    +3.341349498806e-05
+BODY606_SCOEF(3)      +2.617518846598e-07    +3.915574411619e-07
+BODY607_GM            +3.718569049967e-01    +3.712085754472e-01
+BODY608_GM            +1.205076319121e+02    +1.205095752389e+02
+BODY609_GM            +5.529409232812e-01    +5.532371285376e-01
+BODY699_GM            +3.793120738834e+07    +3.793120723494e+07
+BODY699_JCOEF(2)      +1.629070151853e-02    +1.629111964057e-02
+BODY699_JCOEF(4)      -9.340278799551e-04    -9.305945887740e-04
+BODY699_JCOEF(6)      +8.929667654105e-05    +8.872819837009e-05
+BODY699_POLE_DEC(1)   +8.353760844394e+01    +8.353776999027e+01
+BODY699_POLE_DEC(2)   -5.382911302100e-03    -7.584170141686e-03
+BODY699_POLE_RA(1)    +4.058262053545e+01    +4.058252338374e+01
+BODY699_POLE_RA(2)    -2.715273573990e-02    -3.099714786917e-02
+BODY6_GM              +3.794058494370e+07    +3.794058478705e+07
+BODY7_GM              +5.794556400000e+06    +5.794556465752e+06
+
+2016-Jan-29 (published)
+Automated Process
+
+Applicable current Ephemeris = 160129R_SCPSE_15295_15310.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 151115_225T114
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY601_GM            +2.503524000000e+00    +2.503523763302e+00
+BODY602_GM            +7.211140136327e+00    +7.211176947682e+00
+BODY603_GM            +4.121081982359e+01    +4.121082693902e+01
+BODY604_GM            +7.311672244985e+01    +7.311671566552e+01
+BODY605_GM            +1.539427790614e+02    +1.539427914458e+02
+BODY606_GM            +8.978137874425e+03    +8.978137900462e+03
+BODY607_GM            +3.718562949332e-01    +3.718569049967e-01
+BODY608_GM            +1.205073858074e+02    +1.205076319121e+02
+BODY609_GM            +5.529278065380e-01    +5.529409232812e-01
+BODY699_GM            +3.793120738517e+07    +3.793120738834e+07
+BODY699_JCOEF(2)      +1.629070068016e-02    +1.629070151853e-02
+BODY699_JCOEF(4)      -9.340207297950e-04    -9.340278799551e-04
+BODY699_JCOEF(6)      +8.933577374593e-05    +8.929667654105e-05
+BODY699_POLE_DEC(1)   +8.353760430989e+01    +8.353760844394e+01
+BODY699_POLE_RA(1)    +4.058259729361e+01    +4.058262053545e+01
+BODY6_GM              +3.794058494020e+07    +3.794058494370e+07
+
+2015-Nov-16 (published)
+Automated Process
+
+Applicable current Ephemeris = 151116R_SCPSE_15280_15295.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 151030_224E21
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY604_GM            +7.311672244985e+01    +7.311672244985e+01
+BODY605_GM            +1.539427790614e+02    +1.539427790614e+02
+BODY606_GM            +8.978137874425e+03    +8.978137874425e+03
+BODY608_GM            +1.205073858074e+02    +1.205073858074e+02
+BODY699_GM            +3.793120738517e+07    +3.793120738517e+07
+BODY699_POLE_DEC(1)   +8.353760430989e+01    +8.353760430989e+01
+BODY699_POLE_RA(1)    +4.058259729361e+01    +4.058259729361e+01
+BODY6_GM              +3.794058494020e+07    +3.794058494020e+07
+
+2015-Nov-13 (published)
+Automated Process
+
+Applicable current Ephemeris = 151112R_SCPSE_15261_15280.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 151018_223E20
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY601_GM            +2.503525621473e+00    +2.503524000000e+00
+BODY602_GM            +7.211277847563e+00    +7.211140136327e+00
+BODY603_GM            +4.121092050918e+01    +4.121081982359e+01
+BODY604_CCOEF(3)      +4.096610907190e-04    +3.858211235156e-04
+BODY604_GM            +7.311659144214e+01    +7.311672244985e+01
+BODY604_JCOEF(2)      +1.158244618125e-03    +1.294156214342e-03
+BODY605_GM            +1.539428611851e+02    +1.539427790614e+02
+BODY606_GM            +8.978137957021e+03    +8.978137874425e+03
+BODY607_GM            +3.718596409938e-01    +3.718562949332e-01
+BODY608_GM            +1.205088668399e+02    +1.205073858074e+02
+BODY609_GM            +5.529684179873e-01    +5.529278065380e-01
+BODY699_GM            +3.793120740439e+07    +3.793120738517e+07
+BODY699_JCOEF(2)      +1.629070657850e-02    +1.629070068016e-02
+BODY699_JCOEF(4)      -9.340015407952e-04    -9.340207297950e-04
+BODY699_JCOEF(6)      +8.967524235871e-05    +8.933577374593e-05
+BODY699_POLE_DEC(1)   +8.353763029055e+01    +8.353760430989e+01
+BODY699_POLE_RA(1)    +4.058273005421e+01    +4.058259729361e+01
+BODY6_GM              +3.794058496122e+07    +3.794058494020e+07
+
+2015-Nov-02 (published)
+Automated Process
+
+Applicable current Ephemeris = 151102R_SCPSE_15222_15261.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 151001_221T113
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY601_GM            +2.503526767032e+00    +2.503525621473e+00
+BODY602_GM            +7.211670352602e+00    +7.211277847563e+00
+BODY603_GM            +4.121092931739e+01    +4.121092050918e+01
+BODY604_CCOEF(3)      +4.006810364134e-04    +4.096610907190e-04
+BODY604_GM            +7.311657574990e+01    +7.311659144214e+01
+BODY604_JCOEF(2)      +1.216580827110e-03    +1.158244618125e-03
+BODY605_GM            +1.539427263983e+02    +1.539428611851e+02
+BODY606_GM            +8.978138400547e+03    +8.978137957021e+03
+BODY607_GM            +3.718604278380e-01    +3.718596409938e-01
+BODY608_GM            +1.205086493624e+02    +1.205088668399e+02
+BODY609_GM            +5.529652914648e-01    +5.529684179873e-01
+BODY699_GM            +3.793120740278e+07    +3.793120740439e+07
+BODY699_JCOEF(2)      +1.629070431501e-02    +1.629070657850e-02
+BODY699_JCOEF(4)      -9.340751123226e-04    -9.340015407952e-04
+BODY699_JCOEF(6)      +9.105902884329e-05    +8.967524235871e-05
+BODY699_POLE_DEC(1)   +8.353762187255e+01    +8.353763029055e+01
+BODY699_POLE_RA(1)    +4.058273932144e+01    +4.058273005421e+01
+BODY6_GM              +3.794058496009e+07    +3.794058496122e+07
+
+2015-Oct-14 (published)
+Automated Process
+
+Applicable current Ephemeris = 151014R_SCPSE_15180_15222.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 150819_219D5
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY601_GM            +2.503525907247e+00    +2.503526767032e+00
+BODY602_GM            +7.211467207431e+00    +7.211670352602e+00
+BODY603_GM            +4.121094716824e+01    +4.121092931739e+01
+BODY604_CCOEF(3)      +3.900331957120e-04    +4.006810364134e-04
+BODY604_GM            +7.311609968736e+01    +7.311657574990e+01
+BODY604_JCOEF(2)      +1.318240936309e-03    +1.216580827110e-03
+BODY605_GM            +1.539427595960e+02    +1.539427263983e+02
+BODY606_GM            +8.978138174255e+03    +8.978138400547e+03
+BODY607_GM            +3.718568794227e-01    +3.718604278380e-01
+BODY608_GM            +1.205072126963e+02    +1.205086493624e+02
+BODY609_GM            +5.528208458989e-01    +5.529652914648e-01
+BODY699_GM            +3.793120738081e+07    +3.793120740278e+07
+BODY699_JCOEF(2)      +1.629070068016e-02    +1.629070431501e-02
+BODY699_JCOEF(4)      -9.340207297950e-04    -9.340751123226e-04
+BODY699_JCOEF(6)      +8.933577374593e-05    +9.105902884329e-05
+BODY699_POLE_DEC(1)   +8.353760430989e+01    +8.353762187255e+01
+BODY699_POLE_RA(1)    +4.058259729361e+01    +4.058273932144e+01
+BODY6_GM              +3.794058493568e+07    +3.794058496009e+07
+
+2015-Oct-13 (published)
+Automated Process
+
+Applicable current Ephemeris = 151013R_SCPSE_15161_15180.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 150709_218T112
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY601_GM            +2.503514004827e+00    +2.503525907247e+00
+BODY602_GM            +7.211311315180e+00    +7.211467207431e+00
+BODY603_GM            +4.121081532906e+01    +4.121094716824e+01
+BODY604_CCOEF(3)      +3.858211235156e-04    +3.900331957120e-04
+BODY604_GM            +7.311665769360e+01    +7.311609968736e+01
+BODY604_JCOEF(2)      +1.294156214342e-03    +1.318240936309e-03
+BODY605_GM            +1.539425601163e+02    +1.539427595960e+02
+BODY606_GM            +8.978136872551e+03    +8.978138174255e+03
+BODY607_GM            +3.718576178624e-01    +3.718568794227e-01
+BODY608_GM            +1.205072036005e+02    +1.205072126963e+02
+BODY609_GM            +5.524056306757e-01    +5.528208458989e-01
+BODY699_GM            +3.793120737315e+07    +3.793120738081e+07
+BODY699_POLE_DEC(1)   +8.353760430989e+01    +8.353760430989e+01
+BODY699_POLE_RA(1)    +4.058259729361e+01    +4.058259729361e+01
+BODY6_GM              +3.794058492635e+07    +3.794058493568e+07
+
+2015-Oct-12 (published)
+Automated Process
+
+Applicable current Ephemeris = 151009R_SCPSE_15116_15161.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 150618_216D4
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY601_GM            +2.503524000000e+00    +2.503514004827e+00
+BODY602_GM            +7.211140136327e+00    +7.211311315180e+00
+BODY603_GM            +4.121081982359e+01    +4.121081532906e+01
+BODY604_GM            +7.311672244985e+01    +7.311665769360e+01
+BODY605_GM            +1.539427790614e+02    +1.539425601163e+02
+BODY606_CCOEF(3)      +1.026987704003e-05    +9.968773423301e-06
+BODY606_GM            +8.978137874425e+03    +8.978136872551e+03
+BODY606_JCOEF(2)      +2.836955902317e-05    +3.267536300237e-05
+BODY606_SCOEF(3)      +1.626257999633e-07    +2.617518846598e-07
+BODY607_GM            +3.718562949332e-01    +3.718576178624e-01
+BODY608_GM            +1.205073858074e+02    +1.205072036005e+02
+BODY609_GM            +5.529278065380e-01    +5.524056306757e-01
+BODY699_GM            +3.793120738517e+07    +3.793120737315e+07
+BODY699_POLE_DEC(1)   +8.353760430989e+01    +8.353760430989e+01
+BODY699_POLE_RA(1)    +4.058259729361e+01    +4.058259729361e+01
+BODY6_GM              +3.794058494020e+07    +3.794058492635e+07
+
+2015-Aug-28 (published)
+Automated Process
+
+Applicable current Ephemeris = 150828R_SCPSE_15066_15116.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 150507_214T111
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY601_GM            +2.503451908819e+00    +2.503524000000e+00
+BODY602_CCOEF(3)      +1.549800000000e-03    +1.229502218138e-03
+BODY602_GM            +7.211233789589e+00    +7.211140136327e+00
+BODY602_JCOEF(2)      +5.435200000000e-03    +6.055594538600e-03
+BODY603_GM            +4.120932250035e+01    +4.121081982359e+01
+BODY604_CCOEF(3)      +4.042630633858e-04    +3.858211235156e-04
+BODY604_GM            +7.311592012061e+01    +7.311672244985e+01
+BODY604_JCOEF(2)      +1.092458014279e-03    +1.294156214342e-03
+BODY605_CCOEF(3)      +2.209984559363e-04    +2.548409590520e-04
+BODY605_GM            +1.539439497209e+02    +1.539427790614e+02
+BODY605_JCOEF(2)      +9.688723938907e-04    +8.496490377952e-04
+BODY606_CCOEF(3)      +1.036457861987e-05    +1.026987704003e-05
+BODY606_GM            +8.978138015653e+03    +8.978137874425e+03
+BODY606_JCOEF(2)      +3.393754680271e-05    +2.836955902317e-05
+BODY606_SCOEF(3)      +3.214252359006e-07    +1.626257999633e-07
+BODY607_GM            +3.715249700202e-01    +3.718562949332e-01
+BODY608_GM            +1.205006955067e+02    +1.205073858074e+02
+BODY609_GM            +5.539027499377e-01    +5.529278065380e-01
+BODY699_GM            +3.793120683754e+07    +3.793120738517e+07
+BODY699_JCOEF(2)      +1.629116884116e-02    +1.629070068016e-02
+BODY699_JCOEF(4)      -9.304692658710e-04    -9.340207297950e-04
+BODY699_JCOEF(6)      +9.120788665605e-05    +8.933577374593e-05
+BODY699_POLE_DEC(1)   +8.353741023979e+01    +8.353760430989e+01
+BODY699_POLE_DEC(2)   -3.198913258906e-03    -5.382911302100e-03
+BODY699_POLE_RA(1)    +4.058445039396e+01    +4.058259729361e+01
+BODY699_POLE_RA(2)    -4.463634918787e-02    -2.715273573990e-02
+BODY6_GM              +3.794058438556e+07    +3.794058494020e+07
+
+2015-Aug-03 (published)
+Automated Process
+
+Applicable current Ephemeris = 150803R_SCPSE_15033_15066.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 150318_213T110
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY601_GM            +2.503524000000e+00    +2.503451908819e+00
+BODY602_CCOEF(3)      +1.229502218138e-03    +1.549800000000e-03
+BODY602_GM            +7.211454165826e+00    +7.211233789589e+00
+BODY602_JCOEF(2)      +6.055594538600e-03    +5.435200000000e-03
+BODY603_GM            +4.121107782641e+01    +4.120932250035e+01
+BODY604_CCOEF(3)      +3.858211235156e-04    +4.042630633858e-04
+BODY604_GM            +7.311636648732e+01    +7.311592012061e+01
+BODY604_JCOEF(2)      +1.294156214342e-03    +1.092458014279e-03
+BODY605_CCOEF(3)      +2.548409590520e-04    +2.209984559363e-04
+BODY605_GM            +1.539424643535e+02    +1.539439497209e+02
+BODY605_JCOEF(2)      +8.496490377952e-04    +9.688723938907e-04
+BODY606_CCOEF(3)      +9.968773423301e-06    +1.036457861987e-05
+BODY606_GM            +8.978138376543e+03    +8.978138015653e+03
+BODY606_JCOEF(2)      +3.267536300237e-05    +3.393754680271e-05
+BODY606_SCOEF(3)      +2.617518846598e-07    +3.214252359006e-07
+BODY607_GM            +3.718742808951e-01    +3.715249700202e-01
+BODY608_GM            +1.205120887033e+02    +1.205006955067e+02
+BODY609_GM            +5.528989950538e-01    +5.539027499377e-01
+BODY699_GM            +3.793120747608e+07    +3.793120683754e+07
+BODY699_JCOEF(2)      +1.629069817036e-02    +1.629116884116e-02
+BODY699_JCOEF(4)      -9.343344679290e-04    -9.304692658710e-04
+BODY699_JCOEF(6)      +9.003499615840e-05    +9.120788665605e-05
+BODY699_POLE_DEC(1)   +8.353763861569e+01    +8.353741023979e+01
+BODY699_POLE_DEC(2)   -6.782331809658e-03    -3.198913258906e-03
+BODY699_POLE_RA(1)    +4.058271311699e+01    +4.058445039396e+01
+BODY699_POLE_RA(2)    -5.744235301067e-02    -4.463634918787e-02
+BODY6_GM              +3.794058503620e+07    +3.794058438556e+07
+BODY7_GM              +5.794548600000e+06    +5.794556400000e+06
+
+2015-Jun-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 150609R_SCPSE_14365_15033.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 150214_212T109
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY603_GM            +4.121107782641e+01    +4.121107782641e+01
+BODY604_GM            +7.311636648732e+01    +7.311636648732e+01
+BODY605_GM            +1.539424643535e+02    +1.539424643535e+02
+BODY606_GM            +8.978138376543e+03    +8.978138376543e+03
+BODY608_GM            +1.205120887033e+02    +1.205120887033e+02
+BODY699_GM            +3.793120747608e+07    +3.793120747608e+07
+BODY699_POLE_RA(1)    +4.058271311699e+01    +4.058271311699e+01
+BODY6_GM              +3.794058503620e+07    +3.794058503620e+07
+
+2015-Mar-04 (published)
+Automated Process
+
+Applicable current Ephemeris = 150304R_SCPSE_14283_14327.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 141210_210T107
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY603_GM            +4.121107782641e+01    +4.121107782641e+01
+BODY604_GM            +7.311636648732e+01    +7.311636648732e+01
+BODY605_GM            +1.539424643535e+02    +1.539424643535e+02
+BODY606_GM            +8.978138376543e+03    +8.978138376543e+03
+BODY608_GM            +1.205120887033e+02    +1.205120887033e+02
+BODY699_GM            +3.793120747608e+07    +3.793120747608e+07
+BODY699_POLE_RA(1)    +4.058271311699e+01    +4.058271311699e+01
+BODY6_GM              +3.794058503620e+07    +3.794058503620e+07
+
+2015-Jan-22 (published)
+Automated Process
+
+Applicable current Ephemeris = 150122R_SCPSE_14251_14283.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 141023_1_209T106
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY603_GM            +4.121107782641e+01    +4.121107782641e+01
+BODY604_GM            +7.311636648732e+01    +7.311636648732e+01
+BODY605_GM            +1.539424643535e+02    +1.539424643535e+02
+BODY606_GM            +8.978138376543e+03    +8.978138376543e+03
+BODY608_GM            +1.205120887033e+02    +1.205120887033e+02
+BODY699_GM            +3.793120747608e+07    +3.793120747608e+07
+BODY699_POLE_RA(1)    +4.058271311699e+01    +4.058271311699e+01
+BODY6_GM              +3.794058503620e+07    +3.794058503620e+07
+
+2015-Jan-08 (published)
+Automated Process
+
+Applicable current Ephemeris = 150107R_SCPSE_14222_14251.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 140923_1_208T105
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY601_GM            +2.503522884662e+00    +2.503524000000e+00
+BODY602_GM            +7.211292085480e+00    +7.211454165826e+00
+BODY603_GM            +4.121117207701e+01    +4.121107782641e+01
+BODY604_GM            +7.311635322923e+01    +7.311636648732e+01
+BODY605_GM            +1.539422045545e+02    +1.539424643535e+02
+BODY606_GM            +8.978138845307e+03    +8.978138376543e+03
+BODY607_GM            +3.718791714192e-01    +3.718742808951e-01
+BODY608_GM            +1.205134781724e+02    +1.205120887033e+02
+BODY609_GM            +5.531110414633e-01    +5.528989950538e-01
+BODY699_GM            +3.793120749865e+07    +3.793120747608e+07
+BODY699_JCOEF(2)      +1.629069546360e-02    +1.629069817036e-02
+BODY699_JCOEF(4)      -9.343510777890e-04    -9.343344679290e-04
+BODY699_JCOEF(6)      +8.959557103495e-05    +9.003499615840e-05
+BODY699_POLE_DEC(1)   +8.353764728832e+01    +8.353763861569e+01
+BODY699_POLE_DEC(2)   -5.841335281700e-03    -6.782331809658e-03
+BODY699_POLE_RA(1)    +4.058270059426e+01    +4.058271311699e+01
+BODY699_POLE_RA(2)    -2.896108850840e-02    -5.744235301067e-02
+BODY6_GM              +3.794058506051e+07    +3.794058503620e+07
+
+2014-Nov-12 (published)
+Automated Process
+
+Applicable current Ephemeris = 141107R_SCPSE_14187_14222.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 140820_207T104
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY603_GM            +4.121117207701e+01    +4.121117207701e+01
+BODY604_GM            +7.311635322923e+01    +7.311635322923e+01
+BODY605_GM            +1.539422045545e+02    +1.539422045545e+02
+BODY606_GM            +8.978138845307e+03    +8.978138845307e+03
+BODY608_GM            +1.205134781724e+02    +1.205134781724e+02
+BODY699_GM            +3.793120749865e+07    +3.793120749865e+07
+BODY699_POLE_DEC(1)   +8.353764728832e+01    +8.353764728832e+01
+BODY699_POLE_RA(1)    +4.058270059426e+01    +4.058270059426e+01
+BODY6_GM              +3.794058506051e+07    +3.794058506051e+07
+
+2014-Sep-09 (published)
+Automated Process
+
+Applicable current Ephemeris = 140909R_SCPSE_14118_14156.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 140621_205T102
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800066164e+03    +4.902800066164e+03
+BODY399_GM            +3.986004354361e+05    +3.986004354361e+05
+BODY3_GM              +4.035032355023e+05    +4.035032355023e+05
+BODY603_GM            +4.121117207701e+01    +4.121117207701e+01
+BODY604_GM            +7.311635322923e+01    +7.311635322923e+01
+BODY605_GM            +1.539422045545e+02    +1.539422045545e+02
+BODY606_GM            +8.978138845307e+03    +8.978138845307e+03
+BODY608_GM            +1.205134781724e+02    +1.205134781724e+02
+BODY699_GM            +3.793120749865e+07    +3.793120749865e+07
+BODY699_POLE_DEC(1)   +8.353764728832e+01    +8.353764728832e+01
+BODY699_POLE_RA(1)    +4.058270059426e+01    +4.058270059426e+01
+BODY6_GM              +3.794058506051e+07    +3.794058506051e+07
+
+2014-Sep-08 (published)
+Automated Process
+
+Applicable current Ephemeris = 140907R_SCPSE_14083_14118.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 140520_204T101
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800066164e+03
+BODY399_GM            +3.986004362961e+05    +3.986004354361e+05
+BODY3_GM              +4.035032417380e+05    +4.035032355023e+05
+BODY603_GM            +4.121117207701e+01    +4.121117207701e+01
+BODY604_GM            +7.311635322923e+01    +7.311635322923e+01
+BODY605_GM            +1.539422045545e+02    +1.539422045545e+02
+BODY606_GM            +8.978138845307e+03    +8.978138845307e+03
+BODY608_GM            +1.205134781724e+02    +1.205134781724e+02
+BODY699_GM            +3.793120749865e+07    +3.793120749865e+07
+BODY699_POLE_DEC(1)   +8.353764728832e+01    +8.353764728832e+01
+BODY699_POLE_RA(1)    +4.058270059426e+01    +4.058270059426e+01
+BODY6_GM              +3.794058506051e+07    +3.794058506051e+07
+
+2014-Jul-30 (published)
+Automated Process
+
+Applicable current Ephemeris = 140730R_SCPSE_14051_14083.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 140406_1_203T100
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327132332630e+11    +1.327132332639e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY5_GM              +1.267127648000e+08    +1.267127641000e+08
+BODY601_GM            +2.503364720729e+00    +2.503522884662e+00
+BODY602_GM            +7.210993899856e+00    +7.211292085480e+00
+BODY603_GM            +4.121581541110e+01    +4.121117207701e+01
+BODY604_GM            +7.311557283053e+01    +7.311635322923e+01
+BODY605_GM            +1.539406284855e+02    +1.539422045545e+02
+BODY606_GM            +8.978139578101e+03    +8.978138845307e+03
+BODY607_GM            +3.717916399235e-01    +3.718791714192e-01
+BODY608_GM            +1.205114136810e+02    +1.205134781724e+02
+BODY609_GM            +5.534147464623e-01    +5.531110414633e-01
+BODY699_GM            +3.793120752438e+07    +3.793120749865e+07
+BODY699_JCOEF(2)      +1.629072646994e-02    +1.629069546360e-02
+BODY699_JCOEF(4)      -9.344250974340e-04    -9.343510777890e-04
+BODY699_JCOEF(6)      +8.813632975019e-05    +8.959557103495e-05
+BODY699_POLE_DEC(1)   +8.353762188214e+01    +8.353764728832e+01
+BODY699_POLE_DEC(2)   -5.270052700000e-03    -5.841335281700e-03
+BODY699_POLE_RA(1)    +4.058216280703e+01    +4.058270059426e+01
+BODY699_POLE_RA(2)    -2.613331560000e-02    -2.896108850840e-02
+BODY6_GM              +3.794058508695e+07    +3.794058506051e+07
+
+2014-Apr-16 (published)
+Automated Process
+
+Applicable current Ephemeris = 131212R_SCPSE_13273_13314.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 131203_199T96
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.503364720729e+00    +2.503364720729e+00
+BODY602_GM            +7.210993899856e+00    +7.210993899856e+00
+BODY603_GM            +4.121581541110e+01    +4.121581541110e+01
+BODY604_GM            +7.311557283053e+01    +7.311557283053e+01
+BODY605_GM            +1.539406284855e+02    +1.539406284855e+02
+BODY606_GM            +8.978139578101e+03    +8.978139578101e+03
+BODY607_GM            +3.717916399235e-01    +3.717916399235e-01
+BODY608_GM            +1.205114136810e+02    +1.205114136810e+02
+BODY609_GM            +5.534147464623e-01    +5.534147464623e-01
+BODY699_GM            +3.793120752438e+07    +3.793120752438e+07
+BODY699_POLE_RA(1)    +4.058216280703e+01    +4.058216280703e+01
+BODY6_GM              +3.794058508695e+07    +3.794058508695e+07
+
+2013-Nov-05 (published)
+Automated Process
+
+Applicable current Ephemeris = 131105R_SCPSE_13241_13273.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 131015_198T95
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.503374984937e+00    +2.503364720729e+00
+BODY602_GM            +7.210314573106e+00    +7.210993899856e+00
+BODY603_GM            +4.121574151061e+01    +4.121581541110e+01
+BODY604_GM            +7.311549677532e+01    +7.311557283053e+01
+BODY605_GM            +1.539342977601e+02    +1.539406284855e+02
+BODY606_GM            +8.978138842275e+03    +8.978139578101e+03
+BODY607_GM            +3.713760834192e-01    +3.717916399235e-01
+BODY608_GM            +1.206203311620e+02    +1.205114136810e+02
+BODY609_GM            +5.517032680985e-01    +5.534147464623e-01
+BODY699_GM            +3.793120685564e+07    +3.793120752438e+07
+BODY699_POLE_RA(1)    +4.058216280703e+01    +4.058216280703e+01
+BODY6_GM              +3.794058451712e+07    +3.794058508695e+07
+
+2013-Oct-24 (published)
+Automated Process
+
+Applicable current Ephemeris = 131024R_SCPSE_13200_13241.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130911_1_196T94
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.503374776631e+00    +2.503374984937e+00
+BODY602_GM            +7.210337723506e+00    +7.210314573106e+00
+BODY603_GM            +4.121575887463e+01    +4.121574151061e+01
+BODY604_GM            +7.311550199907e+01    +7.311549677532e+01
+BODY605_GM            +1.539347521641e+02    +1.539342977601e+02
+BODY606_GM            +8.978138821641e+03    +8.978138842275e+03
+BODY607_GM            +3.713736540033e-01    +3.713760834192e-01
+BODY608_GM            +1.206179856883e+02    +1.206203311620e+02
+BODY609_GM            +5.517634486963e-01    +5.517032680985e-01
+BODY699_GM            +3.793120686211e+07    +3.793120685564e+07
+BODY699_POLE_RA(1)    +4.058216280703e+01    +4.058216280703e+01
+BODY6_GM              +3.794058452178e+07    +3.794058451712e+07
+
+2013-Aug-07 (published)
+Automated Process
+
+Applicable current Ephemeris = 130807R_SCPSE_13182_13200.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130728_195T93
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.503429813962e+00    +2.503374776631e+00
+BODY602_GM            +7.210840769838e+00    +7.210337723506e+00
+BODY603_GM            +4.121595253499e+01    +4.121575887463e+01
+BODY604_GM            +7.311551677682e+01    +7.311550199907e+01
+BODY605_GM            +1.539413218607e+02    +1.539347521641e+02
+BODY606_GM            +8.978138475460e+03    +8.978138821641e+03
+BODY607_GM            +3.716489921802e-01    +3.713736540033e-01
+BODY608_GM            +1.205296586416e+02    +1.206179856883e+02
+BODY609_GM            +5.531893969084e-01    +5.517634486963e-01
+BODY699_GM            +3.793120725180e+07    +3.793120686211e+07
+BODY699_POLE_RA(1)    +4.058216280703e+01    +4.058216280703e+01
+BODY6_GM              +3.794058483184e+07    +3.794058452178e+07
+
+2013-Aug-06 (published)
+Automated Process
+
+Applicable current Ephemeris = 130805R_SCPSE_13137_13182.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130713_191T92
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.503362278258e+00    +2.503429813962e+00
+BODY602_GM            +7.211043999269e+00    +7.210840769838e+00
+BODY603_GM            +4.121588570561e+01    +4.121595253499e+01
+BODY604_GM            +7.311557954726e+01    +7.311551677682e+01
+BODY605_GM            +1.539414301615e+02    +1.539413218607e+02
+BODY606_GM            +8.978138967275e+03    +8.978138475460e+03
+BODY607_GM            +3.718388169205e-01    +3.716489921802e-01
+BODY608_GM            +1.205022472133e+02    +1.205296586416e+02
+BODY609_GM            +5.535607118676e-01    +5.531893969084e-01
+BODY699_GM            +3.793120749789e+07    +3.793120725180e+07
+BODY699_POLE_RA(1)    +4.058216280703e+01    +4.058216280703e+01
+BODY6_GM              +3.794058505181e+07    +3.794058483184e+07
+
+2013-Jul-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 130710R_SCPSE_13087_13137.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130523_186T91
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.503368098279e+00    +2.503362278258e+00
+BODY602_GM            +7.210949360765e+00    +7.211043999269e+00
+BODY603_GM            +4.121585654735e+01    +4.121588570561e+01
+BODY604_GM            +7.311557703862e+01    +7.311557954726e+01
+BODY605_GM            +1.539411472541e+02    +1.539414301615e+02
+BODY606_GM            +8.978139224038e+03    +8.978138967275e+03
+BODY607_GM            +3.717757415270e-01    +3.718388169205e-01
+BODY608_GM            +1.205185887895e+02    +1.205022472133e+02
+BODY609_GM            +5.533386917621e-01    +5.535607118676e-01
+BODY699_GM            +3.793120742331e+07    +3.793120749789e+07
+BODY699_POLE_RA(1)    +4.058216280703e+01    +4.058216280703e+01
+BODY6_GM              +3.794058499314e+07    +3.794058505181e+07
+
+2013-Apr-17 (published)
+Automated Process
+
+Applicable current Ephemeris = 130417R_SCPSE_13063_13087.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130408_184T90
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.503389125014e+00    +2.503368098279e+00
+BODY602_GM            +7.210824055520e+00    +7.210949360765e+00
+BODY603_GM            +4.121646992503e+01    +4.121585654735e+01
+BODY604_GM            +7.311567610646e+01    +7.311557703862e+01
+BODY605_GM            +1.539423900165e+02    +1.539411472541e+02
+BODY606_GM            +8.978137632912e+03    +8.978139224038e+03
+BODY607_GM            +3.711283610021e-01    +3.717757415270e-01
+BODY608_GM            +1.205659185921e+02    +1.205185887895e+02
+BODY609_GM            +5.528757716183e-01    +5.533386917621e-01
+BODY699_GM            +3.793120691303e+07    +3.793120742331e+07
+BODY699_POLE_RA(1)    +4.058216280703e+01    +4.058216280703e+01
+BODY6_GM              +3.794058452933e+07    +3.794058499314e+07
+
+2013-Mar-21 (published)
+Automated Process
+
+Applicable current Ephemeris = 130321R_SCPSE_13038_13063.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130313_182R4
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.502932588485e+00    +2.503389125014e+00
+BODY602_CCOEF(3)      +1.176812733860e-03    +1.229502218138e-03
+BODY602_GM            +7.210896041606e+00    +7.210824055520e+00
+BODY602_JCOEF(2)      +6.162878919072e-03    +6.055594538600e-03
+BODY603_GM            +4.121933431551e+01    +4.121646992503e+01
+BODY604_CCOEF(3)      +3.855939046889e-04    +3.858211235156e-04
+BODY604_GM            +7.311632825840e+01    +7.311567610646e+01
+BODY604_JCOEF(2)      +1.293263547580e-03    +1.294156214342e-03
+BODY605_CCOEF(3)      +2.571480059012e-04    +2.548409590520e-04
+BODY605_GM            +1.539385013507e+02    +1.539423900165e+02
+BODY605_JCOEF(2)      +8.573276471275e-04    +8.496490377952e-04
+BODY606_CCOEF(3)      +9.903199565258e-06    +9.968773423301e-06
+BODY606_GM            +8.978138963512e+03    +8.978137632912e+03
+BODY606_JCOEF(2)      +3.134349728982e-05    +3.267536300237e-05
+BODY606_SCOEF(3)      +2.488942346963e-07    +2.617518846598e-07
+BODY607_GM            +3.718387203243e-01    +3.711283610021e-01
+BODY608_GM            +1.205399337324e+02    +1.205659185921e+02
+BODY609_GM            +5.542009195944e-01    +5.528757716183e-01
+BODY699_GM            +3.793120747903e+07    +3.793120691303e+07
+BODY699_JCOEF(2)      +1.629070978718e-02    +1.629072646994e-02
+BODY699_JCOEF(4)      -9.345542285460e-04    -9.344250974340e-04
+BODY699_JCOEF(6)      +9.038698194879e-05    +8.813632975019e-05
+BODY699_POLE_DEC(1)   +8.353763359470e+01    +8.353762188214e+01
+BODY699_POLE_DEC(2)   -5.393363540000e-03    -5.270052700000e-03
+BODY699_POLE_RA(1)    +4.058220675714e+01    +4.058216280703e+01
+BODY699_POLE_RA(2)    -2.674382740000e-02    -2.613331560000e-02
+BODY6_GM              +3.794058507196e+07    +3.794058452933e+07
+
+2013-Mar-19 (published)
+Automated Process
+
+Applicable current Ephemeris = 130319R_SCPSE_12328_13038.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130216_176T89
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.502945581381e+00    +2.502932588485e+00
+BODY602_GM            +7.211023433546e+00    +7.210896041606e+00
+BODY603_GM            +4.121952415934e+01    +4.121933431551e+01
+BODY604_GM            +7.311641175079e+01    +7.311632825840e+01
+BODY605_GM            +1.539431652765e+02    +1.539385013507e+02
+BODY606_GM            +8.978139479506e+03    +8.978138963512e+03
+BODY607_GM            +3.716481784171e-01    +3.718387203243e-01
+BODY608_GM            +1.205238623917e+02    +1.205399337324e+02
+BODY609_GM            +5.531853006318e-01    +5.542009195944e-01
+BODY699_GM            +3.793120733707e+07    +3.793120747903e+07
+BODY699_POLE_DEC(1)   +8.353763359470e+01    +8.353763359470e+01
+BODY699_POLE_RA(1)    +4.058220675714e+01    +4.058220675714e+01
+BODY6_GM              +3.794058491832e+07    +3.794058507196e+07
+
+2013-Mar-18 (published)
+Automated Process
+
+Applicable current Ephemeris = 130318R_SCPSE_12304_12328.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 121201_1_175T88
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.502939495793e+00    +2.502945581381e+00
+BODY602_GM            +7.211025890027e+00    +7.211023433546e+00
+BODY603_GM            +4.121934071627e+01    +4.121952415934e+01
+BODY604_GM            +7.311635183417e+01    +7.311641175079e+01
+BODY605_GM            +1.539401771918e+02    +1.539431652765e+02
+BODY606_GM            +8.978139786579e+03    +8.978139479506e+03
+BODY607_GM            +3.717985592397e-01    +3.716481784171e-01
+BODY608_GM            +1.205178807361e+02    +1.205238623917e+02
+BODY609_GM            +5.532217008470e-01    +5.531853006318e-01
+BODY699_GM            +3.793120749695e+07    +3.793120733707e+07
+BODY699_POLE_DEC(1)   +8.353763359470e+01    +8.353763359470e+01
+BODY699_POLE_RA(1)    +4.058220675714e+01    +4.058220675714e+01
+BODY6_GM              +3.794058506948e+07    +3.794058491832e+07
+
+2013-Jan-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 130109R_SCPSE_12304_12328.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 121201_175T88
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.502940780953e+00    +2.502939495793e+00
+BODY602_GM            +7.211029263108e+00    +7.211025890027e+00
+BODY603_GM            +4.121939803881e+01    +4.121934071627e+01
+BODY604_GM            +7.311638721527e+01    +7.311635183417e+01
+BODY605_GM            +1.539412620568e+02    +1.539401771918e+02
+BODY606_GM            +8.978139854664e+03    +8.978139786579e+03
+BODY607_GM            +3.717873741716e-01    +3.717985592397e-01
+BODY608_GM            +1.205176869455e+02    +1.205178807361e+02
+BODY609_GM            +5.531786201455e-01    +5.532217008470e-01
+BODY699_GM            +3.793120740273e+07    +3.793120749695e+07
+BODY699_POLE_DEC(1)   +8.353763359470e+01    +8.353763359470e+01
+BODY699_POLE_RA(1)    +4.058220675714e+01    +4.058220675714e+01
+BODY6_GM              +3.794058497625e+07    +3.794058506948e+07
+
+2012-Dec-07 (published)
+Automated Process
+
+Applicable current Ephemeris = 121204R_SCPSE_12257_12304.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 121112_173T87
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.502953915374e+00    +2.502940780953e+00
+BODY602_GM            +7.210903693776e+00    +7.211029263108e+00
+BODY603_GM            +4.121983674110e+01    +4.121939803881e+01
+BODY604_GM            +7.311642657552e+01    +7.311638721527e+01
+BODY605_GM            +1.539430345777e+02    +1.539412620568e+02
+BODY606_GM            +8.978138873141e+03    +8.978139854664e+03
+BODY607_GM            +3.718066068942e-01    +3.717873741716e-01
+BODY608_GM            +1.205411087412e+02    +1.205176869455e+02
+BODY609_GM            +5.534220101256e-01    +5.531786201455e-01
+BODY699_GM            +3.793120714779e+07    +3.793120740273e+07
+BODY699_POLE_DEC(1)   +8.353763359470e+01    +8.353763359470e+01
+BODY699_POLE_RA(1)    +4.058220675714e+01    +4.058220675714e+01
+BODY6_GM              +3.794058474615e+07    +3.794058497625e+07
+
+2012-Dec-01 (published)
+Automated Process
+
+Applicable current Ephemeris = 121130R_SCPSE_12199_12257.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120926_170T86
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327132332632e+11    +1.327132332630e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.502896232927e+00    +2.502953915374e+00
+BODY602_CCOEF(3)      +1.571853686210e-03    +1.176812733860e-03
+BODY602_GM            +7.211586963839e+00    +7.210903693776e+00
+BODY602_JCOEF(2)      +5.058062033063e-03    +6.162878919072e-03
+BODY603_GM            +4.121708815158e+01    +4.121983674110e+01
+BODY604_CCOEF(3)      +3.851393798411e-04    +3.855939046889e-04
+BODY604_GM            +7.311722849064e+01    +7.311642657552e+01
+BODY604_JCOEF(2)      +1.304894043103e-03    +1.293263547580e-03
+BODY605_CCOEF(3)      +2.568688346349e-04    +2.571480059012e-04
+BODY605_GM            +1.539395355110e+02    +1.539430345777e+02
+BODY605_JCOEF(2)      +8.563886910818e-04    +8.573276471275e-04
+BODY606_CCOEF(3)      +9.910925261286e-06    +9.903199565258e-06
+BODY606_GM            +8.978142647138e+03    +8.978138873141e+03
+BODY606_JCOEF(2)      +3.406863224874e-05    +3.134349728982e-05
+BODY606_SCOEF(3)      +6.096328895348e-07    +2.488942346963e-07
+BODY607_GM            +3.720941692925e-01    +3.718066068942e-01
+BODY608_GM            +1.205067470663e+02    +1.205411087412e+02
+BODY609_GM            +5.520151854476e-01    +5.534220101256e-01
+BODY699_GM            +3.793120704106e+07    +3.793120714779e+07
+BODY699_JCOEF(2)      +1.629085324163e-02    +1.629070978718e-02
+BODY699_JCOEF(4)      -9.338162877618e-04    -9.345542285460e-04
+BODY699_JCOEF(6)      +9.442465978731e-05    +9.038698194879e-05
+BODY699_POLE_DEC(1)   +8.353760495079e+01    +8.353763359470e+01
+BODY699_POLE_DEC(2)   -5.720607940000e-03    -5.393363540000e-03
+BODY699_POLE_RA(1)    +4.058219911002e+01    +4.058220675714e+01
+BODY699_POLE_RA(2)    -2.837023140000e-02    -2.674382740000e-02
+BODY6_GM              +3.794058460290e+07    +3.794058474615e+07
+BODY7_GM              +5.794557000000e+06    +5.794548600000e+06
+
+2012-Aug-30 (published)
+Automated Process
+
+Applicable current Ephemeris = 120829R_SCPSE_12151_12199.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120723_168T85
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327132332632e+11    +1.327132332632e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.502789688410e+00    +2.502896232927e+00
+BODY602_GM            +7.211762869370e+00    +7.211586963839e+00
+BODY603_GM            +4.121695168687e+01    +4.121708815158e+01
+BODY604_GM            +7.311780375743e+01    +7.311722849064e+01
+BODY605_GM            +1.539399400530e+02    +1.539395355110e+02
+BODY606_GM            +8.978142779511e+03    +8.978142647138e+03
+BODY607_GM            +3.721163085468e-01    +3.720941692925e-01
+BODY608_GM            +1.205058816639e+02    +1.205067470663e+02
+BODY609_GM            +5.517235059199e-01    +5.520151854476e-01
+BODY699_GM            +3.793120704905e+07    +3.793120704106e+07
+BODY699_JCOEF(2)      +1.629083792178e-02    +1.629085324163e-02
+BODY699_JCOEF(4)      -9.337437981265e-04    -9.338162877618e-04
+BODY699_JCOEF(6)      +9.371990144597e-05    +9.442465978731e-05
+BODY699_POLE_DEC(1)   +8.353765343003e+01    +8.353760495079e+01
+BODY699_POLE_RA(1)    +4.058242679916e+01    +4.058219911002e+01
+BODY6_GM              +3.794058461080e+07    +3.794058460290e+07
+
+2012-Jun-29 (published)
+Automated Process
+
+Applicable current Ephemeris = 120628R_SCPSE_12116_12136.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120523_166T83
+
+Parameter              Superseded Value       New Value
+
+BODY10_GM             +1.327124400409e+11    +1.327132332632e+11
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY601_GM            +2.502732557135e+00    +2.502789688410e+00
+BODY602_GM            +7.212055044568e+00    +7.211762869370e+00
+BODY603_GM            +4.121681151664e+01    +4.121695168687e+01
+BODY604_GM            +7.311689571825e+01    +7.311780375743e+01
+BODY605_GM            +1.539392032247e+02    +1.539399400530e+02
+BODY606_GM            +8.978142890321e+03    +8.978142779511e+03
+BODY607_GM            +3.720234351039e-01    +3.721163085468e-01
+BODY608_GM            +1.205064232644e+02    +1.205058816639e+02
+BODY609_GM            +5.515085378325e-01    +5.517235059199e-01
+BODY699_GM            +3.793120714983e+07    +3.793120704905e+07
+BODY699_JCOEF(2)      +1.629086364882e-02    +1.629083792178e-02
+BODY699_JCOEF(4)      -9.337992318066e-04    -9.337437981265e-04
+BODY699_JCOEF(6)      +9.596024651605e-05    +9.371990144597e-05
+BODY699_POLE_DEC(1)   +8.353757612142e+01    +8.353765343003e+01
+BODY699_POLE_DEC(2)   -5.862042770000e-03    -5.720607940000e-03
+BODY699_POLE_RA(1)    +4.058203525207e+01    +4.058242679916e+01
+BODY699_POLE_RA(2)    -2.976086740000e-02    -2.837023140000e-02
+BODY6_GM              +3.794058471037e+07    +3.794058461080e+07
+BODY7_GM              +5.794548600000e+06    +5.794557000000e+06
+
+2012-May-23 (published)
+Automated Process
+
+Applicable current Ephemeris = 120523R_SCPSE_12098_12116.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120502_1_165E19
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362961e+05
+BODY5_GM              +1.267127648000e+08    +1.267127648000e+08
+BODY601_GM            +2.502757050877e+00    +2.502732557135e+00
+BODY602_GM            +7.211707954300e+00    +7.212055044568e+00
+BODY603_GM            +4.121671259700e+01    +4.121681151664e+01
+BODY604_GM            +7.311712862180e+01    +7.311689571825e+01
+BODY605_GM            +1.539390197027e+02    +1.539392032247e+02
+BODY606_GM            +8.978142876094e+03    +8.978142890321e+03
+BODY607_GM            +3.720107081501e-01    +3.720234351039e-01
+BODY608_GM            +1.205077782502e+02    +1.205064232644e+02
+BODY609_GM            +5.514776081161e-01    +5.515085378325e-01
+BODY699_GM            +3.793120712313e+07    +3.793120714983e+07
+BODY699_JCOEF(2)      +1.629087428832e-02    +1.629086364882e-02
+BODY699_JCOEF(4)      -9.338877596813e-04    -9.337992318066e-04
+BODY699_JCOEF(6)      +9.363764244073e-05    +9.596024651605e-05
+BODY699_POLE_DEC(1)   +8.353755491179e+01    +8.353757612142e+01
+BODY699_POLE_DEC(2)   -5.720607940000e-03    -5.862042770000e-03
+BODY699_POLE_RA(1)    +4.058192715365e+01    +4.058203525207e+01
+BODY699_POLE_RA(2)    -2.837023140000e-02    -2.976086740000e-02
+BODY6_GM              +3.794058468460e+07    +3.794058471037e+07
+BODY7_GM              +5.794548600000e+06    +5.794548600000e+06
+
+2012-Apr-26 (published)
+Automated Process
+
+Applicable current Ephemeris = 120426R_SCPSE_12077_12098.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120416_164E18
+
+Parameter              Superseded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800076228e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362333e+05    +3.986004362961e+05
+BODY5_GM              +1.267127648000e+08    +1.267127648000e+08
+BODY601_GM            +2.502781809124e+00    +2.502757050877e+00
+BODY602_GM            +7.211929911319e+00    +7.211707954300e+00
+BODY603_GM            +4.121700270136e+01    +4.121671259700e+01
+BODY604_GM            +7.311735484700e+01    +7.311712862180e+01
+BODY605_GM            +1.539394541121e+02    +1.539390197027e+02
+BODY606_GM            +8.978142978805e+03    +8.978142876094e+03
+BODY607_GM            +3.720046795694e-01    +3.720107081501e-01
+BODY608_GM            +1.205116677867e+02    +1.205077782502e+02
+BODY609_GM            +5.515442127428e-01    +5.514776081161e-01
+BODY699_GM            +3.793120714229e+07    +3.793120712313e+07
+BODY699_JCOEF(2)      +1.629083239718e-02    +1.629087428832e-02
+BODY699_JCOEF(4)      -9.339199266817e-04    -9.338877596813e-04
+BODY699_JCOEF(6)      +9.407948941470e-05    +9.363764244073e-05
+BODY699_POLE_DEC(1)   +8.353765707880e+01    +8.353755491179e+01
+BODY699_POLE_RA(1)    +4.058232152654e+01    +4.058192715365e+01
+BODY6_GM              +3.794058470900e+07    +3.794058468460e+07
+BODY7_GM              +5.794557000000e+06    +5.794548600000e+06
+
+2012-Apr-18 (published)
+Automated Process
+
+Applicable current Ephemeris = 120416R_SCPSE_12042_12061.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120329_162E17
+
+Parameter              Superceded Value       New Value
+
+BODY299_GM            +3.248585920000e+05    +3.248585920000e+05
+BODY301_GM            +4.902800013433e+03    +4.902800076228e+03
+BODY399_GM            +3.986004362961e+05    +3.986004362333e+05
+BODY599_GM            +1.266865339033e+08    +1.267127654544e+08
+BODY5_GM              +1.267127648000e+08    +1.267127648000e+08
+BODY601_GM            +2.502576360130e+00    +2.502781809124e+00
+BODY602_CCOEF(3)      +1.401126121569e-03    +1.571853686210e-03
+BODY602_GM            +7.211620392608e+00    +7.211929911319e+00
+BODY602_JCOEF(2)      +5.180894509760e-03    +5.058062033063e-03
+BODY603_GM            +4.121701834062e+01    +4.121700270136e+01
+BODY604_CCOEF(3)      +3.792220000000e-04    +3.851393798411e-04
+BODY604_GM            +7.311625775155e+01    +7.311735484700e+01
+BODY604_JCOEF(2)      +1.262860000000e-03    +1.304894043103e-03
+BODY605_CCOEF(3)      +2.193468165357e-04    +2.568688346349e-04
+BODY605_GM            +1.539397404411e+02    +1.539394541121e+02
+BODY605_JCOEF(2)      +9.541798988345e-04    +8.563886910818e-04
+BODY606_CCOEF(3)      +9.955883795748e-06    +9.910925261286e-06
+BODY606_GM            +8.978137947298e+03    +8.978142978805e+03
+BODY606_JCOEF(2)      +3.346401469529e-05    +3.406863224874e-05
+BODY606_SCOEF(3)      +2.817024724065e-07    +6.096328895348e-07
+BODY607_GM            +3.717797526598e-01    +3.720046795694e-01
+BODY608_GM            +1.205457671731e+02    +1.205116677867e+02
+BODY609_GM            +5.530284459514e-01    +5.515442127428e-01
+BODY699_GM            +3.793120680764e+07    +3.793120714229e+07
+BODY699_JCOEF(2)      +1.629088162435e-02    +1.629083239718e-02
+BODY699_JCOEF(4)      -9.341612482702e-04    -9.339199266817e-04
+BODY699_JCOEF(6)      +8.936911675694e-05    +9.407948941470e-05
+BODY699_POLE_DEC(1)   +8.353758489860e+01    +8.353765707880e+01
+BODY699_POLE_DEC(2)   -5.862042770000e-03    -5.720607940000e-03
+BODY699_POLE_RA(1)    +4.058274178768e+01    +4.058232152654e+01
+BODY699_POLE_RA(2)    -2.976086740000e-02    -2.837023140000e-02
+BODY6_GM              +3.794058440338e+07    +3.794058470900e+07
+BODY7_GM              +5.794548600000e+06    +5.794557000000e+06
+
+2012-Feb-28 (published)
+Automated Process
+
+Applicable current Ephemeris = 120227R_SCPSE_11357_12016.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120203_160T81
+
+Parameter              Superceded Value       New Value
+
+BODY299_GM            +3.248585988265e+05    +3.248585920000e+05
+BODY301_GM            +4.902800076228e+03    +4.902800013433e+03
+BODY399_GM            +3.986004362333e+05    +3.986004362961e+05
+BODY3_GM              +4.035032363096e+05    +4.035032417380e+05
+BODY601_GM            +2.502609373501e+00    +2.502576360130e+00
+BODY602_CCOEF(3)      +1.401126100000e-03    +1.401126121569e-03
+BODY602_GM            +7.211505727025e+00    +7.211620392608e+00
+BODY602_JCOEF(2)      +5.180890000000e-03    +5.180894509760e-03
+BODY603_GM            +4.121695859535e+01    +4.121701834062e+01
+BODY604_GM            +7.311631631847e+01    +7.311625775155e+01
+BODY605_CCOEF(3)      +2.193468000000e-04    +2.193468165357e-04
+BODY605_GM            +1.539396945672e+02    +1.539397404411e+02
+BODY605_JCOEF(2)      +9.541800000000e-04    +9.541798988345e-04
+BODY606_CCOEF(3)      +9.955900000000e-06    +9.955883795748e-06
+BODY606_GM            +8.978138479967e+03    +8.978137947298e+03
+BODY606_JCOEF(2)      +3.346000000000e-05    +3.346401469529e-05
+BODY606_SCOEF(3)      +2.817000000000e-07    +2.817024724065e-07
+BODY607_GM            +3.717583184521e-01    +3.717797526598e-01
+BODY608_GM            +1.205487491162e+02    +1.205457671731e+02
+BODY609_GM            +5.524333193119e-01    +5.530284459514e-01
+BODY699_GM            +3.793120690270e+07    +3.793120680764e+07
+BODY699_JCOEF(2)      +1.629087423500e-02    +1.629088162435e-02
+BODY699_JCOEF(4)      -9.342391790000e-04    -9.341612482702e-04
+BODY699_JCOEF(6)      +8.883146500000e-05    +8.936911675694e-05
+BODY699_POLE_DEC(1)   +8.353758200000e+01    +8.353758489860e+01
+BODY699_POLE_DEC(2)   -5.862000000000e-03    -5.862042770000e-03
+BODY699_POLE_RA(1)    +4.058264200000e+01    +4.058274178768e+01
+BODY699_POLE_RA(2)    -2.976100000000e-02    -2.976086740000e-02
+BODY6_GM              +3.794058450123e+07    +3.794058440338e+07
+
+2012-Jan-19 (published)
+Automated Process
+
+Applicable current Ephemeris = 120119R_SCPSE_11337_11357.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120105_159T80
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.51701198      37940584.50122525     
+BODY699_GM             37931206.9198          37931206.9027         
+BODY699_POLE_RA(1)     40.582648              40.582642             
+BODY699_POLE_DEC(1)    83.537576              83.537582             
+BODY699_JCOEF(2)       0.016290873808         0.016290874235        
+BODY699_JCOEF(4)       -0.000934271084        -0.000934239179       
+BODY699_JCOEF(6)       0.000088937374         0.000088831465        
+BODY601_GM             2.502701109172617      2.502609373500557     
+BODY602_GM             7.211289386801197      7.211505727024772     
+BODY603_GM             41.21702746886321      41.21695859535338     
+BODY604_GM             73.11634639889347      73.11631631847311     
+BODY604_JCOEF(2)       0.0012                 0.00126286            
+BODY604_CCOEF(3)       0.000361               0.0003792220          
+BODY605_GM             153.9395644216691      153.9396945671801     
+BODY606_GM             8978.138517075671      8978.138479966845     
+BODY607_GM             0.371740933989066      0.371758318452143     
+BODY608_GM             120.5475434022670      120.5487491162408     
+BODY609_GM             0.5524404151635458     0.5524333193118883    
+
+2012-Jan-17 (published)
+Automated Process
+
+Applicable current Ephemeris = 120117R_SCPSE_11303_11337.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 111216_157T79
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.72898314      37940584.51701198     
+BODY699_GM             37931207.1187          37931206.9198         
+BODY699_POLE_RA(1)     40.582382              40.582648             
+BODY699_POLE_DEC(1)    83.537590              83.537576             
+BODY699_JCOEF(2)       0.016290899375         0.016290873808        
+BODY699_JCOEF(4)       -0.000934474971        -0.000934271084       
+BODY699_JCOEF(6)       0.000087083293         0.000088937374        
+BODY601_GM             2.502748619543429      2.502701109172617     
+BODY602_GM             7.211444887614973      7.211289386801197     
+BODY603_GM             41.21721833070302      41.21702746886321     
+BODY604_GM             73.11637880800029      73.11634639889347     
+BODY605_GM             153.9515313553848      153.9395644216691     
+BODY606_GM             8978.140251410228      8978.138517075671     
+BODY607_GM             0.371745584012855      0.371740933989066     
+BODY608_GM             120.5458907932224      120.5475434022670     
+BODY609_GM             0.5531157026177208     0.5524404151635458    
+
+2011-Oct-14 (published)
+Automated Process
+
+Applicable current Ephemeris = 111014R_SCPSE_11246_11267.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 111003_154E14
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.48265366      37940584.72898314     
+BODY699_GM             37931207.9045          37931207.1187         
+BODY699_POLE_RA(1)     40.582396              40.582382             
+BODY699_POLE_RA(2)     -0.033859              -0.029761             
+BODY699_POLE_DEC(1)    83.537615              83.537590             
+BODY699_POLE_DEC(2)    -0.006348              -0.005862             
+BODY699_JCOEF(2)       0.016290821650         0.016290899375        
+BODY699_JCOEF(4)       -0.000934481091        -0.000934474971       
+BODY699_JCOEF(6)       0.000089178356         0.000087083293        
+BODY601_GM             2.502709995086387      2.502748619543429     
+BODY602_GM             7.211349287191156      7.211444887614973     
+BODY602_JCOEF(2)       0.00527772             0.00518089            
+BODY602_CCOEF(3)       0.0013095931           0.0014011261          
+BODY603_GM             41.21699261797900      41.21721833070302     
+BODY604_GM             73.11610656099036      73.11637880800029     
+BODY605_GM             153.9403316477660      153.9515313553848     
+BODY605_JCOEF(2)       0.00095018             0.00095418            
+BODY605_CCOEF(3)       0.0002230468           0.0002193468          
+BODY606_GM             8978.142487268824      8978.140251410228     
+BODY606_JCOEF(2)       0.00003216             0.00003346            
+BODY606_CCOEF(3)       0.0000099392           0.0000099559          
+BODY606_SCOEF(3)       -0.0000003327          0.0000002817          
+BODY607_GM             0.371862776487706      0.371745584012855     
+BODY608_GM             120.5236609628246      120.5458907932224     
+BODY609_GM             0.5526712667564784     0.5531157026177208    
+
+2011-Oct-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 111010R_SCPSE_11150_11246.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 110915_150T78
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.79162857      37940585.48265366     
+BODY699_GM             37931207.2153          37931207.9045         
+BODY699_POLE_RA(1)     40.582683              40.582396             
+BODY699_POLE_DEC(1)    83.537662              83.537615             
+BODY699_JCOEF(2)       0.016290924417         0.016290821650        
+BODY699_JCOEF(4)       -0.000934268461        -0.000934481091       
+BODY699_JCOEF(6)       0.000087694639         0.000089178356        
+BODY601_GM             2.502718654443902      2.502709995086387     
+BODY602_GM             7.211415535267963      7.211349287191156     
+BODY603_GM             41.21680348050685      41.21699261797900     
+BODY604_GM             73.11620149768477      73.11610656099036     
+BODY605_GM             153.9429277851216      153.9403316477660     
+BODY606_GM             8978.141512182867      8978.142487268824     
+BODY607_GM             0.371559508106878      0.371862776487706     
+BODY608_GM             120.5206701212654      120.5236609628246     
+BODY609_GM             0.5525429652386353     0.5526712667564784    
+
+2011-Aug-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 110721R_SCPSE_11119_11150.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 110623_149T77
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.41564407      37940584.79162857     
+BODY699_GM             37931207.8379          37931207.2153         
+BODY699_POLE_RA(1)     40.582735              40.582683             
+BODY699_POLE_DEC(1)    83.537640              83.537662             
+BODY699_JCOEF(2)       0.016290769033         0.016290924417        
+BODY699_JCOEF(4)       -0.000934828924        -0.000934268461       
+BODY699_JCOEF(6)       0.000089541641         0.000087694639        
+BODY601_GM             2.502712463799070      2.502718654443902     
+BODY602_GM             7.211309707003353      7.211415535267963     
+BODY603_GM             41.21694923358992      41.21680348050685     
+BODY604_GM             73.11602896866832      73.11620149768477     
+BODY605_GM             153.9421876166184      153.9429277851216     
+BODY606_GM             8978.141233205604      8978.141512182867     
+BODY607_GM             0.371894539491829      0.371559508106878     
+BODY608_GM             120.5228618777735      120.5206701212654     
+BODY609_GM             0.5525905733729537     0.5525429652386353    
+
+2011-May-20 (published)
+Automated Process
+
+Applicable current Ephemeris = 110519R_SCPSE_11093_11119.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 110511_148T76
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.28449907      37940585.41564407     
+BODY699_GM             37931207.7016          37931207.8379         
+BODY699_POLE_RA(1)     40.583101              40.582735             
+BODY699_POLE_DEC(1)    83.537606              83.537640             
+BODY699_JCOEF(2)       0.016290745825         0.016290769033        
+BODY699_JCOEF(4)       -0.000934907419        -0.000934828924       
+BODY699_JCOEF(6)       0.000090097813         0.000089541641        
+BODY601_GM             2.502684587752144      2.502712463799070     
+BODY602_GM             7.211270538055901      7.211309707003353     
+BODY602_JCOEF(2)       0.00549329             0.00527772            
+BODY602_CCOEF(3)       0.0011903952           0.0013095931          
+BODY603_GM             41.21712026405778      41.21694923358992     
+BODY604_GM             73.11608291566047      73.11602896866832     
+BODY605_GM             153.9428904917647      153.9421876166184     
+BODY605_JCOEF(2)       0.00095268             0.00095018            
+BODY605_CCOEF(3)       0.0002222901           0.0002230468          
+BODY606_GM             8978.141550256330      8978.141233205604     
+BODY607_GM             0.372068900451880      0.371894539491829     
+BODY608_GM             120.5266601781686      120.5228618777735     
+BODY609_GM             0.5525857916664789     0.5525905733729537    
+
+2011-Feb-04 (published)
+Automated Process
+
+Applicable current Ephemeris = 110204R_SCPSE_10344_11003.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 110113_143R3
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.37187426      37940585.28449907     
+BODY699_GM             37931207.7852          37931207.7016         
+BODY699_POLE_RA(1)     40.581500              40.583101             
+BODY699_POLE_RA(2)     -0.028733              -0.033859             
+BODY699_POLE_DEC(1)    83.537730              83.537606             
+BODY699_POLE_DEC(2)    -0.005948              -0.006348             
+BODY699_JCOEF(2)       0.016290633224         0.016290745825        
+BODY699_JCOEF(4)       -0.000935195652        -0.000934907419       
+BODY699_JCOEF(6)       0.000085459485         0.000090097813        
+BODY601_GM             2.502626327561335      2.502684587752144     
+BODY602_GM             7.210536994915831      7.211270538055901     
+BODY602_JCOEF(2)       0.00531842             0.00549329            
+BODY602_CCOEF(3)       0.0015976821           0.0011903952          
+BODY603_GM             41.22349707074201      41.21712026405778     
+BODY604_GM             73.11665319608169      73.11608291566047     
+BODY605_GM             153.9442354209173      153.9428904917647     
+BODY605_JCOEF(2)       0.00095295             0.00095268            
+BODY605_CCOEF(3)       0.0002228052           0.0002222901          
+BODY606_GM             8978.139216940886      8978.141550256330     
+BODY606_JCOEF(2)       0.00003269             0.00003216            
+BODY606_CCOEF(3)       0.0000100419           0.0000099392          
+BODY606_SCOEF(3)       0.0000003039           -0.0000003327         
+BODY607_GM             0.371282156229949      0.372068900451880     
+BODY608_GM             120.5253274797591      120.5266601781686     
+BODY609_GM             0.5532663617110715     0.5525857916664789    
+
+2011-Jan-19 (published)
+Automated Process
+
+Applicable current Ephemeris = 110119R_SCPSE_10326_10358.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 101223_142E13
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.41238648      37940585.37187426     
+BODY699_GM             37931207.8284          37931207.7852         
+BODY699_POLE_RA(1)     40.581689              40.581500             
+BODY699_POLE_DEC(1)    83.537707              83.537730             
+BODY699_JCOEF(2)       0.016290633969         0.016290633224        
+BODY699_JCOEF(4)       -0.000935277266        -0.000935195652       
+BODY699_JCOEF(6)       0.000084635225         0.000085459485        
+BODY601_GM             2.502628566850901      2.502626327561335     
+BODY602_GM             7.210415677503655      7.210536994915831     
+BODY602_JCOEF(2)       0.00523040             0.00531842            
+BODY602_CCOEF(3)       0.0015737859           0.0015976821          
+BODY603_GM             41.22320902398944      41.22349707074201     
+BODY604_GM             73.11651456573139      73.11665319608169     
+BODY605_GM             153.9443320892218      153.9442354209173     
+BODY606_GM             8978.139152894189      8978.139216940886     
+BODY607_GM             0.371399737059410      0.371282156229949     
+BODY608_GM             120.5230847276307      120.5253274797591     
+BODY609_GM             0.5532448793302067     0.5532663617110715    
+
+2010-Dec-17 (published)
+Automated Process
+
+Applicable current Ephemeris = 101215R_SCPSE_10302_10326.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 101201_141E12
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.83653561      37940585.41238648     
+BODY699_GM             37931207.2536          37931207.8284         
+BODY699_POLE_RA(1)     40.582631              40.581689             
+BODY699_POLE_RA(2)     -0.032774              -0.028733             
+BODY699_POLE_DEC(1)    83.537547              83.537707             
+BODY699_POLE_DEC(2)    -0.004597              -0.005948             
+BODY699_JCOEF(2)       0.016290651320         0.016290633969        
+BODY699_JCOEF(4)       -0.000935096688        -0.000935277266       
+BODY699_JCOEF(6)       0.000085352909         0.000084635225        
+BODY601_GM             2.502663111473977      2.502628566850901     
+BODY602_GM             7.211324203674568      7.210415677503655     
+BODY602_JCOEF(2)       0.00557036             0.00523040            
+BODY602_CCOEF(3)       0.0016663335           0.0015737859          
+BODY603_GM             41.22170043283749      41.22320902398944     
+BODY604_GM             73.11568875704903      73.11651456573139     
+BODY605_GM             153.9440126920278      153.9443320892218     
+BODY606_GM             8978.138814840953      8978.139152894189     
+BODY607_GM             0.371969905643023      0.371399737059410     
+BODY608_GM             120.5236408456456      120.5230847276307     
+BODY609_GM             0.5531308887862909     0.5532448793302067    
+
+2010-Oct-14 (published)
+Automated Process
+
+Applicable current Ephemeris = 101013R_SCPSE_10216_10256.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100927_137T72
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.61433598      37940584.83653561     
+BODY699_GM             37931207.0322          37931207.2536         
+BODY699_POLE_RA(1)     40.582809              40.582631             
+BODY699_POLE_DEC(1)    83.537558              83.537547             
+BODY699_JCOEF(2)       0.016290678471         0.016290651320        
+BODY699_JCOEF(4)       -0.000935178263        -0.000935096688       
+BODY699_JCOEF(6)       0.000084369889         0.000085352909        
+BODY601_GM             2.502663309378276      2.502663111473977     
+BODY602_GM             7.211042948930951      7.211324203674568     
+BODY603_GM             41.22306832898998      41.22170043283749     
+BODY604_GM             73.11573158578534      73.11568875704903     
+BODY605_GM             153.9434257917183      153.9440126920278     
+BODY606_GM             8978.138489543775      8978.138814840953     
+BODY607_GM             0.372089441130883      0.371969905643023     
+BODY608_GM             120.5225430884476      120.5236408456456     
+BODY609_GM             0.5530596352942014     0.5531308887862909    
+
+2010-Sep-13 (published)
+Automated Process
+
+Applicable current Ephemeris = 100913R_SCPSE_10178_10216.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100816_135E11
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.19103519      37940584.61433598     
+BODY699_GM             37931207.6129          37931207.0322         
+BODY699_POLE_RA(1)     40.582746              40.582809             
+BODY699_POLE_DEC(1)    83.537530              83.537558             
+BODY699_JCOEF(2)       0.016290713275         0.016290678471        
+BODY699_JCOEF(4)       -0.000934907426        -0.000935178263       
+BODY699_JCOEF(6)       0.000086813940         0.000084369889        
+BODY601_GM             2.502649735590598      2.502663309378276     
+BODY602_GM             7.210755807081804      7.211042948930951     
+BODY603_GM             41.22385281006390      41.22306832898998     
+BODY604_GM             73.11577260830295      73.11573158578534     
+BODY605_GM             153.9434705372475      153.9434257917183     
+BODY606_GM             8978.138947128351      8978.138489543775     
+BODY607_GM             0.372093053243830      0.372089441130883     
+BODY608_GM             120.5174460416719      120.5225430884476     
+BODY609_GM             0.5531061101745497     0.5530596352942014    
+
+2010-Jul-27 (published)
+Automated Process
+
+Applicable current Ephemeris = 100726R_SCPSE_10164_10178.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100709_134T71
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.18590788      37940585.19103519     
+BODY699_GM             37931207.6077          37931207.6129         
+BODY699_POLE_RA(1)     40.582679              40.582746             
+BODY699_POLE_DEC(1)    83.537533              83.537530             
+BODY699_JCOEF(2)       0.016290699821         0.016290713275        
+BODY699_JCOEF(4)       -0.000934908417        -0.000934907426       
+BODY699_JCOEF(6)       0.000086154394         0.000086813940        
+BODY601_GM             2.502653854130373      2.502649735590598     
+BODY602_GM             7.210753192578406      7.210755807081804     
+BODY603_GM             41.22399120522562      41.22385281006390     
+BODY604_GM             73.11575812534798      73.11577260830295     
+BODY605_GM             153.9434658935521      153.9434705372475     
+BODY606_GM             8978.138877124944      8978.138947128351     
+BODY607_GM             0.372092758433870      0.372093053243830     
+BODY608_GM             120.5175109354886      120.5174460416719     
+BODY609_GM             0.5531033330031904     0.5531061101745497    
+
+2010-Jul-06 (published)
+Automated Process
+
+Applicable current Ephemeris = 100706R_SCPSE_10146_10164.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100623_133T70
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.29031831      37940585.18590788     
+BODY699_GM             37931207.7190          37931207.6077         
+BODY699_POLE_RA(1)     40.582751              40.582679             
+BODY699_POLE_DEC(1)    83.537526              83.537533             
+BODY699_JCOEF(2)       0.016290754606         0.016290699821        
+BODY699_JCOEF(4)       -0.000934784018        -0.000934908417       
+BODY699_JCOEF(6)       0.000086160455         0.000086154394        
+BODY601_GM             2.502656688609775      2.502653854130373     
+BODY602_GM             7.210856063224142      7.210753192578406     
+BODY603_GM             41.22385484916347      41.22399120522562     
+BODY604_GM             73.11579543141077      73.11575812534798     
+BODY605_GM             153.9435729984046      153.9434658935521     
+BODY606_GM             8978.138935580162      8978.138877124944     
+BODY606_JCOEF(2)       0.00003264             0.00003269            
+BODY606_CCOEF(3)       0.0000101074           0.0000100419          
+BODY606_SCOEF(3)       0.0000002976           0.0000003039          
+BODY607_GM             0.371810410430814      0.372092758433870     
+BODY608_GM             120.5108312160242      120.5175109354886     
+BODY609_GM             0.5530318826600191     0.5531033330031904    
+
+2010-Jun-25 (published)
+Automated Process
+
+Applicable current Ephemeris = 100625R_SCPSE_10132_10146.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100608_132T69
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.37753170      37940585.29031831     
+BODY699_GM             37931207.8020          37931207.7190         
+BODY699_POLE_RA(1)     40.583044              40.582751             
+BODY699_POLE_RA(2)     -0.051079              -0.032774             
+BODY699_POLE_DEC(1)    83.537392              83.537526             
+BODY699_POLE_DEC(2)    -0.003848              -0.004597             
+BODY699_JCOEF(2)       0.016290743445         0.016290754606        
+BODY699_JCOEF(4)       -0.000934656136        -0.000934784018       
+BODY699_JCOEF(6)       0.000089478120         0.000086160455        
+BODY601_GM             2.502671606225361      2.502656688609775     
+BODY602_GM             7.215820873505562      7.210856063224142     
+BODY603_GM             41.22377302913180      41.22385484916347     
+BODY604_GM             73.11608477740288      73.11579543141077     
+BODY605_GM             153.9425885951420      153.9435729984046     
+BODY606_GM             8978.139647304321      8978.138935580162     
+BODY606_JCOEF(2)       0.00003269             0.00003264            
+BODY606_CCOEF(3)       0.0000100419           0.0000101074          
+BODY606_SCOEF(3)       0.0000003039           0.0000002976          
+BODY607_GM             0.371579902841404      0.371810410430814     
+BODY608_GM             120.5103570301357      120.5108312160242     
+BODY609_GM             0.5530290115183746     0.5530318826600191    
+
+2010-Jun-16 (published)
+Automated Process
+
+Applicable current Ephemeris = 100616R_SCPSE_10110_10132.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100523_131T68
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.06567518      37940585.37753170     
+BODY699_GM             37931207.5024          37931207.8020         
+BODY699_POLE_RA(1)     40.583171              40.583044             
+BODY699_POLE_RA(2)     -0.049286              -0.051079             
+BODY699_POLE_DEC(1)    83.537659              83.537392             
+BODY699_POLE_DEC(2)    -0.003661              -0.003848             
+BODY699_JCOEF(2)       0.016290772029         0.016290743445        
+BODY699_JCOEF(4)       -0.000934694303        -0.000934656136       
+BODY699_JCOEF(6)       0.000089880248         0.000089478120        
+BODY601_GM             2.502694107602816      2.502671606225361     
+BODY602_GM             7.200063329536838      7.215820873505562     
+BODY602_JCOEF(2)       0.00897000             0.00557036            
+BODY602_CCOEF(3)       0.0020800000           0.0016663335          
+BODY603_GM             41.22407969389818      41.22377302913180     
+BODY604_GM             73.11530489083277      73.11608477740288     
+BODY605_GM             153.9438092585369      153.9425885951420     
+BODY605_JCOEF(2)       0.00094296             0.00095295            
+BODY605_CCOEF(3)       0.0002311116           0.0002228052          
+BODY606_GM             8978.139811476925      8978.139647304321     
+BODY606_JCOEF(2)       0.00003345             0.00003269            
+BODY606_CCOEF(3)       0.0000100225           0.0000100419          
+BODY606_SCOEF(3)       0.0000002649           0.0000003039          
+BODY607_GM             0.371472830275555      0.371579902841404     
+BODY608_GM             120.5130217227762      120.5103570301357     
+BODY609_GM             0.5530242922746966     0.5530290115183746    
+
+2010-Apr-20 (published)
+Automated Process
+
+Applicable current Ephemeris = 100420R_SCPSE_10055_10085.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100409_128T67
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.21575641      37940585.06567518     
+BODY699_GM             37931207.6474          37931207.5024         
+BODY699_POLE_RA(1)     40.583800              40.583171             
+BODY699_POLE_DEC(1)    83.537637              83.537659             
+BODY699_JCOEF(2)       0.016290761372         0.016290772029        
+BODY699_JCOEF(4)       -0.000935041843        -0.000934694303       
+BODY699_JCOEF(6)       0.000088218547         0.000089880248        
+BODY601_GM             2.502664059914654      2.502694107602816     
+BODY602_GM             7.206088184897235      7.200063329536838     
+BODY603_GM             41.22395894571505      41.22407969389818     
+BODY604_GM             73.11537306097487      73.11530489083277     
+BODY605_GM             153.9437119917676      153.9438092585369     
+BODY605_JCOEF(2)       0.00094265             0.00094296            
+BODY605_CCOEF(3)       0.0002312426           0.0002311116          
+BODY606_GM             8978.139838625968      8978.139811476925     
+BODY607_GM             0.371514037767062      0.371472830275555     
+BODY608_GM             120.5121181800631      120.5130217227762     
+BODY609_GM             0.5530860071780509     0.5530242922746966    
+
+2010-Mar-25 (published)
+Automated Process
+
+Applicable current Ephemeris = 100325R_SCPSE_10021_10055.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100306_126R2
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.09552705      37940585.21575641     
+BODY699_GM             37931207.5284          37931207.6474         
+BODY699_POLE_RA(1)     40.585300              40.583800             
+BODY699_POLE_RA(2)     -0.078714              -0.049286             
+BODY699_POLE_DEC(1)    83.537587              83.537637             
+BODY699_POLE_DEC(2)    -0.002593              -0.003661             
+BODY699_JCOEF(2)       0.016290745623         0.016290761372        
+BODY699_JCOEF(4)       -0.000935314074        -0.000935041843       
+BODY699_JCOEF(6)       0.000087992940         0.000088218547        
+BODY601_GM             2.502460898333089      2.502664059914654     
+BODY602_GM             7.214445984477930      7.206088184897235     
+BODY603_GM             41.22381705804884      41.22395894571505     
+BODY604_GM             73.11541481976771      73.11537306097487     
+BODY605_GM             153.9435622399753      153.9437119917676     
+BODY605_JCOEF(2)       0.000941               0.00094265            
+BODY605_CCOEF(3)       0.000232               0.0002312426          
+BODY606_GM             8978.139471964878      8978.139838625968     
+BODY607_GM             0.371794454208596      0.371514037767062     
+BODY608_GM             120.5028737124517      120.5121181800631     
+BODY609_GM             0.5533175139508248     0.5530860071780509    
+
+2010-Feb-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 100209R_SCPSE_10003_10021.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100131_125T66
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.22578886      37940585.09552705     
+BODY699_GM             37931207.6569          37931207.5284         
+BODY699_POLE_RA(1)     40.585759              40.585300             
+BODY699_POLE_DEC(1)    83.537556              83.537587             
+BODY699_JCOEF(2)       0.016290741015         0.016290745623        
+BODY699_JCOEF(4)       -0.000935387473        -0.000935314074       
+BODY699_JCOEF(6)       0.000088500228         0.000087992940        
+BODY601_GM             2.502446043296527      2.502460898333089     
+BODY602_GM             7.215994919166206      7.214445984477930     
+BODY603_GM             41.22362671256990      41.22381705804884     
+BODY604_GM             73.11544724167149      73.11541481976771     
+BODY605_GM             153.9435653494335      153.9435622399753     
+BODY606_GM             8978.139773741363      8978.139471964878     
+BODY607_GM             0.371704406193575      0.371794454208596     
+BODY608_GM             120.5029631980470      120.5028737124517     
+BODY609_GM             0.5533689173792706     0.5533175139508248    
+
+2010-Jan-14 (published)
+Automated Process
+
+Applicable current Ephemeris = 100114R_SCPSE_09339_09355.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100103_123T64
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.15858903      37940585.22578886     
+BODY699_GM             37931207.5900          37931207.6569         
+BODY699_POLE_RA(1)     40.585776              40.585759             
+BODY699_POLE_DEC(1)    83.537549              83.537556             
+BODY699_JCOEF(2)       0.016290740684         0.016290741015        
+BODY699_JCOEF(4)       -0.000935384506        -0.000935387473       
+BODY699_JCOEF(6)       0.000088616052         0.000088500228        
+BODY601_GM             2.502444361443687      2.502446043296527     
+BODY602_GM             7.216019322193621      7.215994919166206     
+BODY603_GM             41.22364199485792      41.22362671256990     
+BODY604_GM             73.11544873759908      73.11544724167149     
+BODY605_GM             153.9436018626194      153.9435653494335     
+BODY606_GM             8978.139733770831      8978.139773741363     
+BODY607_GM             0.371729621214713      0.371704406193575     
+BODY608_GM             120.5026255303498      120.5029631980470     
+BODY609_GM             0.5533749729146867     0.5533689173792706    
+
+2010-Jan-13 (published)
+Automated Process
+
+Applicable current Ephemeris = 100113R_SCPSE_09317_09339.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 091214_122T63
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.16056534      37940585.15858903     
+BODY699_GM             37931207.5928          37931207.5900         
+BODY699_POLE_RA(1)     40.585833              40.585776             
+BODY699_POLE_DEC(1)    83.537546              83.537549             
+BODY699_JCOEF(2)       0.016290730583         0.016290740684        
+BODY699_JCOEF(4)       -0.000935329227        -0.000935384506       
+BODY699_JCOEF(6)       0.000089137743         0.000088616052        
+BODY601_GM             2.502448263194753      2.502444361443687     
+BODY602_GM             7.215373106036623      7.216019322193621     
+BODY602_JCOEF(2)       0.00860000             0.00897000            
+BODY602_CCOEF(3)       0.0020000000           0.0020800000          
+BODY603_GM             41.22365223268523      41.22364199485792     
+BODY604_GM             73.11544209566517      73.11544873759908     
+BODY605_GM             153.9428691775221      153.9436018626194     
+BODY606_GM             8978.139780362366      8978.139733770831     
+BODY607_GM             0.371729681348213      0.371729621214713     
+BODY608_GM             120.5030146074768      120.5026255303498     
+BODY609_GM             0.5534091650364432     0.5533749729146867    
+
+2010-Jan-07 (published)
+Automated Process
+
+Applicable current Ephemeris = 100107R_SCPSE_09296_09317.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 091122_121E8
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.09116724      37940585.16056534     
+BODY699_GM             37931207.5249          37931207.5928         
+BODY699_POLE_RA(1)     40.585508              40.585833             
+BODY699_POLE_DEC(1)    83.537554              83.537546             
+BODY699_JCOEF(2)       0.016290731107         0.016290730583        
+BODY699_JCOEF(4)       -0.000935289052        -0.000935329227       
+BODY699_JCOEF(6)       0.000089393653         0.000089137743        
+BODY601_GM             2.502454613265376      2.502448263194753     
+BODY602_GM             7.213717239668965      7.215373106036623     
+BODY602_JCOEF(2)       0.00897000             0.00860000            
+BODY602_CCOEF(3)       0.0020800000           0.0020000000          
+BODY603_GM             41.22368226514975      41.22365223268523     
+BODY604_GM             73.11541351216987      73.11544209566517     
+BODY605_GM             153.9428287523109      153.9428691775221     
+BODY606_GM             8978.139735367682      8978.139780362366     
+BODY607_GM             0.371723892177733      0.371729681348213     
+BODY608_GM             120.5033436971190      120.5030146074768     
+BODY609_GM             0.5534119652050336     0.5534091650364432    
+
+2009-Dec-09 (published)
+Automated Process
+
+Applicable current Ephemeris = 091208R_SCPSE_09275_09296.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 091105_120E7
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.03276838      37940585.09116724     
+BODY699_GM             37931207.4714          37931207.5249         
+BODY699_POLE_RA(1)     40.585279              40.585508             
+BODY699_POLE_DEC(1)    83.537547              83.537554             
+BODY699_JCOEF(2)       0.016290735072         0.016290731107        
+BODY699_JCOEF(4)       -0.000935111838        -0.000935289052       
+BODY699_JCOEF(6)       0.000090315814         0.000089393653        
+BODY601_GM             2.502475635558650      2.502454613265376     
+BODY602_GM             7.208253760083588      7.213717239668965     
+BODY603_GM             41.22378316253346      41.22368226514975     
+BODY604_GM             73.11535293474266      73.11541351216987     
+BODY605_GM             153.9428336666086      153.9428287523109     
+BODY606_GM             8978.139773285628      8978.139735367682     
+BODY607_GM             0.371665390265868      0.371723892177733     
+BODY608_GM             120.5038438413984      120.5033436971190     
+BODY609_GM             0.5533933559394255     0.5534119652050336    
+
+2009-Nov-18 (published)
+Automated Process
+
+Applicable current Ephemeris = 091116R_SCPSE_09231_09275.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 091016_118T62
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.02015772      37940585.03276838     
+BODY699_GM             37931207.4585          37931207.4714         
+BODY699_POLE_RA(1)     40.585339              40.585279             
+BODY699_POLE_DEC(1)    83.537538              83.537547             
+BODY699_JCOEF(2)       0.016290728848         0.016290735072        
+BODY699_JCOEF(4)       -0.000935100646        -0.000935111838       
+BODY699_JCOEF(6)       0.000090361294         0.000090315814        
+BODY601_GM             2.502473662855939      2.502475635558650     
+BODY602_GM             7.207829867198577      7.208253760083588     
+BODY603_GM             41.22376135313479      41.22378316253346     
+BODY604_GM             73.11534875998363      73.11535293474266     
+BODY605_GM             153.9428426421361      153.9428336666086     
+BODY606_GM             8978.139712993554      8978.139773285628     
+BODY607_GM             0.371706132043968      0.371665390265868     
+BODY608_GM             120.5046024195398      120.5038438413984     
+BODY609_GM             0.5533978648353445     0.5533933559394255  
+
+2009-Oct-07 (published)
+Automated Process
+
+Applicable current Ephemeris = 091005AP_SCPSE_09248_17265.XSP
+Restrictions/Limitations = Used for planning for the duration of the file.
+Reference/Source of new values = 090903_118T62
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.65797564      37940585.02015772     
+BODY699_GM             37931207.1063          37931207.4585         
+BODY699_POLE_RA(1)     40.584440              40.585339             
+BODY699_POLE_RA(2)     -0.077682              -0.078714             
+BODY699_POLE_DEC(1)    83.537474              83.537538             
+BODY699_POLE_DEC(2)    -0.002560              -0.002593             
+BODY699_JCOEF(2)       0.016290772291         0.016290728848        
+BODY699_JCOEF(4)       -0.000934349536        -0.000935100646       
+BODY699_JCOEF(6)       0.000092641174         0.000090361294        
+BODY601_GM             2.502540299154720      2.502473662855939     
+BODY602_GM             7.199143776956102      7.207829867198577     
+BODY603_GM             41.21630049528812      41.22376135313479     
+BODY604_GM             73.11462427344662      73.11534875998363     
+BODY605_GM             153.9429961290159      153.9428426421361     
+BODY606_GM             8978.139098895999      8978.139712993554     
+BODY607_GM             0.371336843250265      0.371706132043968     
+BODY608_GM             120.5121366316792      120.5046024195398     
+BODY609_GM             0.5535358693227870     0.5533978648353445    
+
+2009-Sep-24 (published)
+Automated Process
+
+Applicable current Ephemeris = 090924R_SCPSE_09215_09231.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090828_117T61
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.66693778      37940584.65797564     
+BODY699_GM             37931207.1203          37931207.1063         
+BODY699_POLE_RA(1)     40.584460              40.584440             
+BODY699_POLE_DEC(1)    83.537511              83.537474             
+BODY699_JCOEF(2)       0.016290819768         0.016290772291        
+BODY699_JCOEF(4)       -0.000934423051        -0.000934349536       
+BODY699_JCOEF(6)       0.000091378573         0.000092641174        
+BODY601_GM             2.502529277804900      2.502540299154720     
+BODY602_GM             7.201941809221156      7.199143776956102     
+BODY603_GM             41.21647784535888      41.21630049528812     
+BODY604_GM             73.11465326768231      73.11462427344662     
+BODY605_GM             153.9430787943620      153.9429961290159     
+BODY606_GM             8978.139238159505      8978.139098895999     
+BODY607_GM             0.371323170984844      0.371336843250265     
+BODY608_GM             120.5039064835442      120.5121366316792     
+BODY609_GM             0.5534758495938736     0.5535358693227870    
+
+2009-Sep-22 (published)
+Automated Process
+
+Applicable current Ephemeris = 090921R_SCPSE_09200_09215.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090810_116T60
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.70866594      37940584.66693778     
+BODY699_GM             37931207.1597          37931207.1203         
+BODY699_POLE_RA(1)     40.584646              40.584460             
+BODY699_POLE_DEC(1)    83.537510              83.537511             
+BODY699_JCOEF(2)       0.016290820193         0.016290819768        
+BODY699_JCOEF(4)       -0.000934488379        -0.000934423051       
+BODY699_JCOEF(6)       0.000091048774         0.000091378573        
+BODY601_GM             2.502526714253576      2.502529277804900     
+BODY602_GM             7.204128393822666      7.201941809221156     
+BODY603_GM             41.21643705156555      41.21647784535888     
+BODY604_GM             73.11467812476211      73.11465326768231     
+BODY605_GM             153.9430863480677      153.9430787943620     
+BODY606_GM             8978.139270340744      8978.139238159505     
+BODY607_GM             0.371283234316610      0.371323170984844     
+BODY608_GM             120.5040974359097      120.5039064835442     
+BODY609_GM             0.5534910265088943     0.5534758495938736    
+
+2009-Aug-17 (published)
+Automated Process
+
+Applicable current Ephemeris = 090817R_SCPSE_09184_09200.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090727_115T59
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.69981475      37940584.70866594     
+BODY699_GM             37931207.1530          37931207.1597         
+BODY699_POLE_RA(1)     40.584632              40.584646             
+BODY699_POLE_DEC(1)    83.537505              83.537510             
+BODY699_JCOEF(2)       0.016290814989         0.016290820193        
+BODY699_JCOEF(4)       -0.000934442184        -0.000934488379       
+BODY699_JCOEF(6)       0.000091417534         0.000091048774        
+BODY601_GM             2.502527494064343      2.502526714253576     
+BODY602_GM             7.202142639487098      7.204128393822666     
+BODY603_GM             41.21646288247825      41.21643705156555     
+BODY604_GM             73.11464936300638      73.11467812476211     
+BODY605_GM             153.9430565154396      153.9430863480677     
+BODY606_GM             8978.139419438765      8978.139270340744     
+BODY607_GM             0.371355483637583      0.371283234316610     
+BODY608_GM             120.5037677365865      120.5040974359097     
+BODY609_GM             0.5534816653469494     0.5534910265088943    
+
+2009-Aug-06 (published)
+Automated Process
+
+Applicable current Ephemeris = 090806R_SCPSE_09168_09184.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090710_114T58
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.53093457      37940584.69981475     
+BODY699_GM             37931206.9833          37931207.1530         
+BODY699_POLE_RA(1)     40.584685              40.584632             
+BODY699_POLE_DEC(1)    83.537493              83.537505             
+BODY699_JCOEF(2)       0.016290815947         0.016290814989        
+BODY699_JCOEF(4)       -0.000934359844        -0.000934442184       
+BODY699_JCOEF(6)       0.000091606222         0.000091417534        
+BODY601_GM             2.502537156770620      2.502527494064343     
+BODY602_GM             7.201056306132469      7.202142639487098     
+BODY603_GM             41.21648344845686      41.21646288247825     
+BODY604_GM             73.11463634344963      73.11464936300638     
+BODY605_GM             153.9430477770478      153.9430565154396     
+BODY606_GM             8978.139168628506      8978.139419438765     
+BODY607_GM             0.371496424973641      0.371355483637583     
+BODY608_GM             120.5056888490891      120.5037677365865     
+BODY609_GM             0.5534819048142049     0.5534816653469494    
+
+2009-Jul-08 (published)
+Automated Process
+
+Applicable current Ephemeris = 090708R_SCPSE_09153_09168.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090626_113T57
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.71483988      37940584.53093457     
+BODY699_GM             37931207.1673          37931206.9833         
+BODY699_POLE_RA(1)     40.584923              40.584685             
+BODY699_POLE_DEC(1)    83.537522              83.537493             
+BODY699_JCOEF(2)       0.016290793712         0.016290815947        
+BODY699_JCOEF(4)       -0.000934709423        -0.000934359844       
+BODY699_JCOEF(6)       0.000090908483         0.000091606222        
+BODY601_GM             2.502492017198180      2.502537156770620     
+BODY602_GM             7.204291351372671      7.201056306132469     
+BODY603_GM             41.21637470288032      41.21648344845686     
+BODY604_GM             73.11467949836259      73.11463634344963     
+BODY605_GM             153.9431111979202      153.9430477770478     
+BODY606_GM             8978.139491416670      8978.139168628506     
+BODY607_GM             0.370991166709194      0.371496424973641     
+BODY608_GM             120.5026713407083      120.5056888490891     
+BODY609_GM             0.5534654353131513     0.5534819048142049    
+
+2009-Jul-01 (published)
+Automated Process
+
+Applicable current Ephemeris = 090701R_SCPSE_09136_09153.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090609_112T56
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.72257956      37940584.71483988     
+BODY699_GM             37931207.1765          37931207.1673         
+BODY699_POLE_RA(1)     40.584630              40.584923             
+BODY699_POLE_DEC(1)    83.537540              83.537522             
+BODY699_JCOEF(2)       0.016290787250         0.016290793712        
+BODY699_JCOEF(4)       -0.000934733160        -0.000934709423       
+BODY699_JCOEF(6)       0.000091418329         0.000090908483        
+BODY601_GM             2.502479294868557      2.502492017198180     
+BODY602_GM             7.202798775360185      7.204291351372671     
+BODY603_GM             41.21624413197247      41.21637470288032     
+BODY604_GM             73.11466057947915      73.11467949836259     
+BODY605_GM             153.9430434766724      153.9431111979202     
+BODY606_GM             8978.139573866585      8978.139491416670     
+BODY607_GM             0.370832695912033      0.370991166709194     
+BODY608_GM             120.5030445679196      120.5026713407083     
+BODY609_GM             0.5534401160635997     0.5534654353131513    
+
+2009-Jun-24 (published)
+Automated Process
+
+Applicable current Ephemeris = 090624R_SCPSE_09120_09136.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090526_111T55
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.75892913      37940584.72257956     
+BODY699_GM             37931207.2088          37931207.1765         
+BODY699_POLE_RA(1)     40.582542              40.584630             
+BODY699_POLE_RA(2)     -0.037432              -0.077682             
+BODY699_POLE_DEC(1)    83.537652              83.537540             
+BODY699_POLE_DEC(2)    -0.004944              -0.002560             
+BODY699_JCOEF(2)       0.016290758527         0.016290787250        
+BODY699_JCOEF(4)       -0.000935166069        -0.000934733160       
+BODY699_JCOEF(6)       0.000089537218         0.000091418329        
+BODY601_GM             2.502480071324441      2.502479294868557     
+BODY602_GM             7.207489777875368      7.202798775360185     
+BODY603_GM             41.21590409811643      41.21624413197247     
+BODY604_GM             73.11480925384234      73.11466057947915     
+BODY605_GM             153.9430369538330      153.9430434766724     
+BODY606_GM             8978.139616255658      8978.139573866585     
+BODY607_GM             0.370625094690230      0.370832695912033     
+BODY608_GM             120.5027152141226      120.5030445679196     
+BODY609_GM             0.5534265033291642     0.5534401160635997    
+
+2009-Jun-11 (published)
+Automated Process
+
+Applicable current Ephemeris = 090609R_SCPSE_09104_09120.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090507_110T54
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.79518565      37940584.75892913     
+BODY699_GM             37931207.2468          37931207.2088         
+BODY699_POLE_RA(1)     40.582443              40.582542             
+BODY699_POLE_DEC(1)    83.537663              83.537652             
+BODY699_JCOEF(2)       0.016290749081         0.016290758527        
+BODY699_JCOEF(4)       -0.000935197591        -0.000935166069       
+BODY699_JCOEF(6)       0.000089824771         0.000089537218        
+BODY601_GM             2.502496382974899      2.502480071324441     
+BODY602_GM             7.206671212324381      7.207489777875368     
+BODY603_GM             41.21592046942041      41.21590409811643     
+BODY604_GM             73.11481317140027      73.11480925384234     
+BODY605_GM             153.9429742206838      153.9430369538330     
+BODY606_GM             8978.139782617298      8978.139616255658     
+BODY607_GM             0.370661213500527      0.370625094690230     
+BODY608_GM             120.5016238558722      120.5027152141226     
+BODY609_GM             0.5534054527005198     0.5534265033291642    
+
+2009-May-21 (published)
+Automated Process
+
+Applicable current Ephemeris = 090520R_SCPSE_09089_09104.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090422_109T53
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940583.83670486      37940584.79518565     
+BODY699_GM             37931206.2896          37931207.2468         
+BODY699_POLE_RA(1)     40.581567              40.582443             
+BODY699_POLE_RA(2)     -0.037353              -0.037432             
+BODY699_POLE_DEC(1)    83.537702              83.537663             
+BODY699_POLE_DEC(2)    -0.004933              -0.004944             
+BODY699_JCOEF(2)       0.016290750592         0.016290749081        
+BODY699_JCOEF(4)       -0.000934942751        -0.000935197591       
+BODY699_JCOEF(6)       0.000089655803         0.000089824771        
+BODY601_GM             2.502375745139359      2.502496382974899     
+BODY602_GM             7.200775737205724      7.206671212324381     
+BODY603_GM             41.21611289570998      41.21592046942041     
+BODY604_GM             73.11472484717956      73.11481317140027     
+BODY605_GM             153.9429469769423      153.9429742206838     
+BODY606_GM             8978.139106855113      8978.139782617298     
+BODY607_GM             0.371190991373805      0.370661213500527     
+BODY608_GM             120.5062324337800      120.5016238558722     
+BODY609_GM             0.5536043842359156     0.5534054527005198    
+
+2009-May-07 (published)
+Automated Process
+
+Applicable current Ephemeris = 090507R_SCPSE_09075_09089.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090407_107T52
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.04339046      37940583.83670486     
+BODY699_GM             37931206.4966          37931206.2896         
+BODY699_POLE_RA(1)     40.581934              40.581567             
+BODY699_POLE_DEC(1)    83.537693              83.537702             
+BODY699_JCOEF(2)       0.016290732957         0.016290750592        
+BODY699_JCOEF(4)       -0.000935091860        -0.000934942751       
+BODY699_JCOEF(6)       0.000089451150         0.000089655803        
+BODY601_GM             2.502415585318155      2.502375745139359     
+BODY602_GM             7.203519438374520      7.200775737205724     
+BODY603_GM             41.21599214744679      41.21611289570998     
+BODY604_GM             73.11474559066438      73.11472484717956     
+BODY605_GM             153.9427553435824      153.9429469769423     
+BODY606_GM             8978.138922629163      8978.139106855113     
+BODY607_GM             0.371620801197215      0.371190991373805     
+BODY608_GM             120.5032558591434      120.5062324337800     
+BODY609_GM             0.5535208221133412     0.5536043842359156    
+
+2009-Apr-23 (published)
+Automated Process
+
+Applicable current Ephemeris = 090423R_SCPSE_09028_09075.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090328_103T51
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.95180942      37940584.04339046     
+BODY699_GM             37931207.3882          37931206.4966         
+BODY699_POLE_RA(1)     40.582774              40.581934             
+BODY699_POLE_RA(2)     -0.036427              -0.037353             
+BODY699_POLE_DEC(1)    83.537685              83.537693             
+BODY699_POLE_DEC(2)    -0.004811              -0.004933             
+BODY699_JCOEF(2)       0.016290704214         0.016290732957        
+BODY699_JCOEF(4)       -0.000935307318        -0.000935091860       
+BODY699_JCOEF(6)       0.000090619956         0.000089451150        
+BODY601_GM             2.502321711007510      2.502415585318155     
+BODY602_GM             7.208313972796445      7.203519438374520     
+BODY603_GM             41.21604378398847      41.21599214744679     
+BODY604_GM             73.11493826230807      73.11474559066438     
+BODY605_GM             153.9431057300922      153.9427553435824     
+BODY606_GM             8978.141024766712      8978.138922629163     
+BODY607_GM             0.370344781190025      0.371620801197215     
+BODY608_GM             120.5141263265947      120.5032558591434     
+BODY609_GM             0.5533540349512766     0.5535208221133412    
+
+2009-Feb-26 (published)
+Automated Process
+
+Applicable current Ephemeris = 090225R_SCPSE_08350_09028.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090209_098T50
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.89169871      37940584.95180942     
+BODY699_GM             37931207.3416          37931207.3882         
+BODY699_POLE_RA(1)     40.582649              40.582774             
+BODY699_POLE_DEC(1)    83.537663              83.537685             
+BODY699_JCOEF(2)       0.016290684865         0.016290704214        
+BODY699_JCOEF(4)       -0.000935283514        -0.000935307318       
+BODY699_JCOEF(6)       0.000090997196         0.000090619956        
+BODY601_GM             2.502352850175356      2.502321711007510     
+BODY602_GM             7.207600997452297      7.208313972796445     
+BODY603_GM             41.21601112668976      41.21604378398847     
+BODY604_GM             73.11488499625567      73.11493826230807     
+BODY605_GM             153.9430894153115      153.9431057300922     
+BODY606_GM             8978.140680747552      8978.141024766712     
+BODY607_GM             0.370996212157831      0.370344781190025     
+BODY608_GM             120.5012562767647      120.5141263265947     
+BODY609_GM             0.5532629207784916     0.5533540349512766    
+
+2009-Feb-02 (published)
+Automated Process
+
+Applicable current Ephemeris = 090202R_SCPSE_08334_08350.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 081228_096T49
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.82205020      37940584.89169871     
+BODY699_GM             37931207.2631          37931207.3416         
+BODY699_POLE_RA(1)     40.582848              40.582649             
+BODY699_POLE_DEC(1)    83.537650              83.537663             
+BODY699_JCOEF(2)       0.016290658170         0.016290684865        
+BODY699_JCOEF(4)       -0.000935427563        -0.000935283514       
+BODY699_JCOEF(6)       0.000090378797         0.000090997196        
+BODY601_GM             2.502374087988651      2.502352850175356     
+BODY602_GM             7.208518568446848      7.207600997452297     
+BODY603_GM             41.21613638955037      41.21601112668976     
+BODY604_GM             73.11487574250081      73.11488499625567     
+BODY605_GM             153.9429874323952      153.9430894153115     
+BODY606_GM             8978.140131197120      8978.140680747552     
+BODY607_GM             0.371644267058727      0.370996212157831     
+BODY608_GM             120.5090171536813      120.5012562767647     
+BODY609_GM             0.5532158104637386     0.5532629207784916    
+
+2009-Jan-20 (published)
+Automated Process
+
+Applicable current Ephemeris = 090120R_SCPSE_08319_08334.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 081208_094T48
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.81290928      37940584.82205020     
+BODY699_GM             37931207.2702          37931207.2631         
+BODY699_POLE_RA(1)     40.582892              40.582848             
+BODY699_POLE_RA(2)     -0.036197              -0.036427             
+BODY699_POLE_DEC(1)    83.537692              83.537650             
+BODY699_POLE_DEC(2)    -0.004781              -0.004811             
+BODY699_JCOEF(2)       0.016290683480         0.016290658170        
+BODY699_JCOEF(4)       -0.000935187071        -0.000935427563       
+BODY699_JCOEF(6)       0.000090351241         0.000090378797        
+BODY601_GM             2.502553353261852      2.502374087988651     
+BODY602_GM             7.198024751397580      7.208518568446848     
+BODY603_GM             41.20680547202384      41.21613638955037     
+BODY604_GM             73.11493779546134      73.11487574250081     
+BODY605_GM             153.9429514952013      153.9429874323952     
+BODY606_GM             8978.139760858710      8978.140131197120     
+BODY606_JCOEF(2)       0.00003676             0.00003345            
+BODY606_CCOEF(3)       0.0000098144           0.0000100225          
+BODY606_SCOEF(3)       0.0000000290           0.0000002649          
+BODY607_GM             0.371733822034568      0.371644267058727     
+BODY608_GM             120.5126935476018      120.5090171536813     
+BODY609_GM             0.5532268430393127     0.5532158104637386    
+
+2008-Dec-17 (published)
+Automated Process
+
+Applicable current Ephemeris = 081217R_SCPSE_08294_08319.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 081122_091T47
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.75080759      37940584.81290928     
+BODY699_GM             37931207.2159          37931207.2702         
+BODY699_POLE_RA(1)     40.583018              40.582892             
+BODY699_POLE_DEC(1)    83.537706              83.537692             
+BODY699_JCOEF(2)       0.016290787300         0.016290683480        
+BODY699_JCOEF(4)       -0.000935059549        -0.000935187071       
+BODY699_JCOEF(6)       0.000088909124         0.000090351241        
+BODY601_GM             2.502593891311248      2.502553353261852     
+BODY602_GM             7.198495850305284      7.198024751397580     
+BODY603_GM             41.20585579154643      41.20680547202384     
+BODY604_GM             73.11498772669157      73.11493779546134     
+BODY605_GM             153.9427416028387      153.9429514952013     
+BODY606_GM             8978.139141085363      8978.139760858710     
+BODY607_GM             0.372318766963366      0.371733822034568     
+BODY608_GM             120.5055433851675      120.5126935476018     
+BODY609_GM             0.5532116571684228     0.5532268430393127    
+
+2008-Dec-03 (published)
+Automated Process
+
+Applicable current Ephemeris = 081126R_SCPSE_08272_08294.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 081106_089T46
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.84323245      37940584.75080759     
+BODY699_GM             37931207.3105          37931207.2159         
+BODY699_POLE_RA(1)     40.583620              40.583018             
+BODY699_POLE_DEC(1)    83.537762              83.537706             
+BODY699_JCOEF(2)       0.016290692878         0.016290787300        
+BODY699_JCOEF(4)       -0.000935823729        -0.000935059549       
+BODY699_JCOEF(6)       0.000088632421         0.000088909124        
+BODY601_GM             2.502623200887248      2.502593891311248     
+BODY602_GM             7.205883040951948      7.198495850305284     
+BODY603_GM             41.20624377144850      41.20585579154643     
+BODY604_GM             73.11470507883155      73.11498772669157     
+BODY605_GM             153.9428866862459      153.9427416028387     
+BODY606_GM             8978.139092755462      8978.139141085363     
+BODY607_GM             0.372242134056882      0.372318766963366     
+BODY608_GM             120.4957900045622      120.5055433851675     
+BODY609_GM             0.5532380113023578     0.5532116571684228    
+
+2008-Oct-31 (published)
+Automated Process
+
+Applicable current Ephemeris = 081031R_SCPSE_08220_08272.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 081011_081E5
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.84137087      37940584.84323245     
+BODY699_GM             37931207.2963          37931207.3105         
+BODY699_POLE_RA(1)     40.582020              40.583620             
+BODY699_POLE_RA(2)     -0.032010              -0.036197             
+BODY699_POLE_DEC(1)    83.537784              83.537762             
+BODY699_POLE_DEC(2)    -0.005401              -0.004781             
+BODY699_JCOEF(2)       0.016290697495         0.016290692878        
+BODY699_JCOEF(4)       -0.000935250961        -0.000935823729       
+BODY699_JCOEF(6)       0.000091782033         0.000088632421        
+BODY601_GM             2.502706597774052      2.502623200887248     
+BODY602_GM             7.206763681178778      7.205883040951948     
+BODY603_GM             41.20803428037864      41.20624377144850     
+BODY604_GM             73.11435544930634      73.11470507883155     
+BODY605_GM             153.9427846135544      153.9428866862459     
+BODY606_GM             8978.139988036010      8978.139092755462     
+BODY606_JCOEF(2)       0.00003495             0.00003676            
+BODY606_CCOEF(3)       0.0000098881           0.0000098144          
+BODY606_SCOEF(3)       0.0000002774           0.0000000290          
+BODY607_GM             0.371532363950584      0.372242134056882     
+BODY608_GM             120.5055685912496      120.4957900045622     
+BODY609_GM             0.5533328348407409     0.5532380113023578    
+
+2008-Sep-16 (published)
+Automated Process
+
+Applicable current Ephemeris = 080916R_SCPSE_08206_08220.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080816_079E4
+
+Parameter              Superceded Value       New Value
+
+BODY10_GM              132712440044.2083      132712440040.9446     
+BODY2_GM               324858.598890645       324858.592000001      
+BODY3_GM               403503.2335605171      403503.2363095674     
+BODY399_GM             398600.4334392727      398600.4362333397     
+BODY5_GM               126712764.8582231      126712764.8000003     
+BODY599_GM             126686533.9614931      126686533.9032703     
+BODY6_GM               37940584.38475962      37940584.84137087     
+BODY699_GM             37931206.8370          37931207.2963         
+BODY699_POLE_RA(1)     40.581443              40.582020             
+BODY699_POLE_RA(2)     -0.027530              -0.032010             
+BODY699_POLE_DEC(1)    83.537728              83.537784             
+BODY699_POLE_DEC(2)    -0.004758              -0.005401             
+BODY699_JCOEF(2)       0.016290733302         0.016290697495        
+BODY699_JCOEF(4)       -0.000935178259        -0.000935250961       
+BODY699_JCOEF(6)       0.000095739859         0.000091782033        
+BODY7_GM               5794549.008216757      5794548.600000031     
+BODY301_GM             4902.800121244415      4902.800076227743     
+BODY601_GM             2.502670647164671      2.502706597774052     
+BODY602_GM             7.208136538970446      7.206763681178778     
+BODY603_GM             41.21476543489587      41.20803428037864     
+BODY604_GM             73.11300597304992      73.11435544930634     
+BODY605_GM             153.9422805538818      153.9427846135544     
+BODY606_GM             8978.139418614695      8978.139988036010     
+BODY606_JCOEF(2)       0.00003681             0.00003495            
+BODY606_CCOEF(3)       0.0000098158           0.0000098881          
+BODY606_SCOEF(3)       0.0000000344           0.0000002774          
+BODY607_GM             0.371344544273395      0.371532363950584     
+BODY608_GM             120.5027082136875      120.5055685912496     
+BODY609_GM             0.5534003114787691     0.5533328348407409    
+
+2008-Sep-05 (published)
+Automated Process
+
+Applicable current Ephemeris = 080819R_SCPSE_08141_08206.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080803_070Sa
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.15980972      37940584.38475962     
+BODY699_GM             37931206.6163          37931206.8370         
+BODY699_POLE_RA(1)     40.581466              40.581443             
+BODY699_POLE_DEC(1)    83.537709              83.537728             
+BODY699_JCOEF(2)       0.016290704643         0.016290733302        
+BODY699_JCOEF(4)       -0.000935189240        -0.000935178259       
+BODY699_JCOEF(6)       0.000096466048         0.000095739859        
+BODY601_GM             2.502881776228512      2.502670647164671     
+BODY602_GM             7.208734879056464      7.208136538970446     
+BODY603_GM             41.21355138275547      41.21476543489587     
+BODY604_GM             73.11290544686008      73.11300597304992     
+BODY605_GM             153.9422746808738      153.9422805538818     
+BODY606_GM             8978.139081588426      8978.139418614695     
+BODY606_JCOEF(2)       0.00003676             0.00003681            
+BODY606_CCOEF(3)       0.0000098144           0.0000098158          
+BODY606_SCOEF(3)       0.0000000290           0.0000000344          
+BODY607_GM             0.371434289398711      0.371344544273395     
+BODY608_GM             120.4992477407413      120.5027082136875     
+
+2008-Jun-18 (published)
+Automated Process
+
+Applicable current Ephemeris = 080618R_SCPSE_08126_08141.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080602_068T44
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.17743508      37940584.15980972     
+BODY699_GM             37931206.6349          37931206.6163         
+BODY699_POLE_RA(1)     40.581827              40.581466             
+BODY699_POLE_DEC(1)    83.537703              83.537709             
+BODY699_JCOEF(2)       0.016290716594         0.016290704643        
+BODY699_JCOEF(4)       -0.000935672409        -0.000935189240       
+BODY699_JCOEF(6)       0.000094389114         0.000096466048        
+BODY601_GM             2.502881955220740      2.502881776228512     
+BODY602_GM             7.210410824718255      7.208734879056464     
+BODY603_GM             41.21262070849623      41.21355138275547     
+BODY604_GM             73.11291911924228      73.11290544686008     
+BODY605_GM             153.9422199461879      153.9422746808738     
+BODY606_GM             8978.138986415834      8978.139081588426     
+BODY607_GM             0.371129805972588      0.371434289398711     
+BODY608_GM             120.4976975847023      120.4992477407413     
+BODY609_GM             0.5537090403439990     0.5534003114787691    
+
+2008-Jun-06 (published)
+Automated Process
+
+Applicable current Ephemeris = 080605R_SCPSE_08078_08126.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080516_063T43
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.27667402      37940584.17743508     
+BODY699_GM             37931206.7269          37931206.6349         
+BODY699_POLE_RA(1)     40.581871              40.581827             
+BODY699_POLE_DEC(1)    83.537722              83.537703             
+BODY699_JCOEF(2)       0.016290694906         0.016290716594        
+BODY699_JCOEF(4)       -0.000935647674        -0.000935672409       
+BODY699_JCOEF(6)       0.000094680606         0.000094389114        
+BODY601_GM             2.502935187158320      2.502881955220740     
+BODY602_GM             7.210716312905534      7.210410824718255     
+BODY602_JCOEF(2)       0.00880584             0.00897000            
+BODY602_CCOEF(3)       0.0014554727           0.0020800000          
+BODY603_GM             41.21188522645834      41.21262070849623     
+BODY604_GM             73.11293489316252      73.11291911924228     
+BODY605_GM             153.9422268415005      153.9422199461879     
+BODY606_GM             8978.138927320846      8978.138986415834     
+BODY607_GM             0.371120905579017      0.371129805972588     
+BODY608_GM             120.5052569914020      120.4976975847023     
+BODY609_GM             0.5537536295128821     0.5537090403439990    
+
+2008-May-15 (published)
+Automated Process
+
+Applicable current Ephemeris = 080515R_SCPSE_08067_08078.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080331_062T42
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.35143083      37940584.27667402     
+BODY699_GM             37931206.8047          37931206.7269         
+BODY699_POLE_RA(1)     40.581833              40.581871             
+BODY699_POLE_DEC(1)    83.537765              83.537722             
+BODY699_JCOEF(2)       0.016290674404         0.016290694906        
+BODY699_JCOEF(4)       -0.000935829230        -0.000935647674       
+BODY699_JCOEF(6)       0.000093971390         0.000094680606        
+BODY601_GM             2.502920537306806      2.502935187158320     
+BODY602_GM             7.211083813192880      7.210716312905534     
+BODY602_JCOEF(2)       0.00877236             0.00880584            
+BODY602_CCOEF(3)       0.0014999008           0.0014554727          
+BODY603_GM             41.21181926660137      41.21188522645834     
+BODY604_GM             73.11292310928664      73.11293489316252     
+BODY605_GM             153.9422173029270      153.9422268415005     
+BODY606_GM             8978.138994952336      8978.138927320846     
+BODY607_GM             0.370895155476839      0.371120905579017     
+BODY608_GM             120.5021858690953      120.5052569914020     
+BODY609_GM             0.5537337090249409     0.5537536295128821    
+
+2008-May-02 (published)
+Automated Process
+
+Applicable current Ephemeris = 080428R_SCPSE_08045_08067.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080313_060E3
+
+Parameter              Superceded Value       New Value
+
+BODY10_GM              132712440040.0565      132712440044.2083     
+BODY2_GM               324858.592000000       324858.598890645      
+BODY3_GM               403503.2363068672      403503.2335605171     
+BODY399_GM             398600.4362002230      398600.4334392727     
+BODY5_GM               126712764.8000000      126712764.8582231     
+BODY599_GM             126686533.9032700      126686533.9614931     
+BODY6_GM               37940585.27338909      37940584.35143083     
+BODY699_GM             37931207.7282          37931206.8047         
+BODY699_POLE_RA(1)     40.581505              40.581833             
+BODY699_POLE_DEC(1)    83.537689              83.537765             
+BODY699_JCOEF(2)       0.016290505727         0.016290674404        
+BODY699_JCOEF(4)       -0.000936733745        -0.000935829230       
+BODY699_JCOEF(6)       0.000086349193         0.000093971390        
+BODY7_GM               5794548.600000000      5794549.008216757     
+BODY301_GM             4902.800106644209      4902.800121244415     
+BODY601_GM             2.503681306799234      2.502920537306806     
+BODY602_GM             7.207438711629040      7.211083813192880     
+BODY602_JCOEF(2)       0.00897                0.00877236            
+BODY602_CCOEF(3)       0.00208                0.0014999008          
+BODY603_GM             41.21161107170069      41.21181926660137     
+BODY604_GM             73.11303912442641      73.11292310928664     
+BODY605_GM             153.9424389694393      153.9422173029270     
+BODY606_GM             8978.137465374053      8978.138994952336     
+BODY607_GM             0.372290582643009      0.370895155476839     
+BODY608_GM             120.5036261119318      120.5021858690953     
+BODY609_GM             0.5535544897385243     0.5537337090249409    
+
+2008-Mar-28 (published)
+Automated Process
+
+Applicable current Ephemeris = 080327R_SCPSE_07365_08045.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080229_056T41
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.28350117      37940585.27338909     
+BODY699_GM             37931207.7391          37931207.7282         
+BODY699_POLE_RA(1)     40.582230              40.581505             
+BODY699_POLE_DEC(1)    83.537656              83.537689             
+BODY699_JCOEF(2)       0.016290539045         0.016290505727        
+BODY699_JCOEF(4)       -0.000936841920        -0.000936733745       
+BODY699_JCOEF(6)       0.000085005705         0.000086349193        
+BODY601_GM             2.503804640631195      2.503681306799234     
+BODY602_GM             7.208113831972937      7.207438711629040     
+BODY603_GM             41.21114295507989      41.21161107170069     
+BODY604_GM             73.11294768194610      73.11303912442641     
+BODY605_GM             153.9423849400276      153.9424389694393     
+BODY606_GM             8978.137388790423      8978.137465374053     
+BODY607_GM             0.372389672138376      0.372290582643009     
+BODY608_GM             120.5026849890331      120.5036261119318     
+BODY609_GM             0.5535191880496334     0.5535544897385243    
+
+2008-Mar-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 080307R_SCPSE_07345_07365.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080108_055T40
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.27527665      37940585.28350117     
+BODY699_GM             37931207.7325          37931207.7391         
+BODY699_POLE_RA(1)     40.582098              40.582230             
+BODY699_POLE_DEC(1)    83.537705              83.537656             
+BODY699_JCOEF(2)       0.016290544651         0.016290539045        
+BODY699_JCOEF(4)       -0.000936905325        -0.000936841920       
+BODY699_JCOEF(6)       0.000084843928         0.000085005705        
+BODY601_GM             2.503914037088305      2.503804640631195     
+BODY602_GM             7.208620862251065      7.208113831972937     
+BODY603_GM             41.21095350743407      41.21114295507989     
+BODY604_GM             73.11290742978323      73.11294768194610     
+BODY605_GM             153.9424010118651      153.9423849400276     
+BODY606_GM             8978.137327428010      8978.137388790423     
+BODY607_GM             0.372366804799818      0.372389672138376     
+BODY608_GM             120.5007708643355      120.5026849890331     
+BODY609_GM             0.5535373313434467     0.5535191880496334    
+
+2008-Jan-25 (published)
+Automated Process
+
+Applicable current Ephemeris = 080123R_SCPSE_07309_07329.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 071208_053T38
+
+Parameter              Superceded Value       New Value
+
+BODY10_GM              132712440044.2083      132712440040.0565     
+BODY2_GM               324858.598890645       324858.592000000      
+BODY3_GM               403503.2335605171      403503.2363068672     
+BODY399_GM             398600.4334392727      398600.4362002230     
+BODY5_GM               126712764.8582231      126712764.8000000     
+BODY599_GM             126686533.9614931      126686533.9032700     
+BODY6_GM               37940584.44408617      37940585.27527665     
+BODY699_GM             37931206.9073          37931207.7325         
+BODY699_POLE_RA(1)     40.581521              40.582098             
+BODY699_POLE_DEC(1)    83.537644              83.537705             
+BODY699_JCOEF(2)       0.016290556604         0.016290544651        
+BODY699_JCOEF(4)       -0.000936535883        -0.000936905325       
+BODY699_JCOEF(6)       0.000087229074         0.000084843928        
+BODY7_GM               5794549.008216757      5794548.600000000     
+BODY301_GM             4902.800121244415      4902.800106644209     
+BODY601_GM             2.503962504392251      2.503914037088305     
+BODY602_GM             7.206462956405896      7.208620862251065     
+BODY603_GM             41.21053911096154      41.21095350743407     
+BODY604_GM             73.11296178124047      73.11290742978323     
+BODY605_GM             153.9420079809344      153.9424010118651     
+BODY606_GM             8978.138641652298      8978.137327428010     
+BODY606_JCOEF(2)       0.00003300             0.00003676            
+BODY606_CCOEF(3)       0.0000111800           0.0000098144          
+BODY606_SCOEF(3)       -0.0000003700          0.0000000290          
+BODY607_GM             0.370879439084761      0.372366804799818     
+BODY608_GM             120.4977883563631      120.5007708643355     
+BODY609_GM             0.5535009498398994     0.5535373313434467    
+
+2008-Jan-22 (published)
+Automated Process
+
+Applicable current Ephemeris = 080117R_SCPSE_07262_07309.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 071121_051T37
+
+
+Parameter              Superceded Value       New Value
+
+
+BODY6_GM               37940584.33316191      37940584.44408617     
+BODY699_GM             37931206.7900          37931206.9073         
+BODY699_POLE_RA(1)     40.581634              40.581521             
+BODY699_POLE_DEC(1)    83.537653              83.537644             
+BODY699_JCOEF(2)       0.016290573664         0.016290556604        
+BODY699_JCOEF(4)       -0.000936412164        -0.000936535883       
+BODY699_JCOEF(6)       0.000087338436         0.000087229074        
+BODY601_GM             2.503976507903127      2.503962504392251     
+BODY602_GM             7.206823163853062      7.206462956405896     
+BODY603_GM             41.21053825232565      41.21053911096154     
+BODY604_GM             73.11294390332988      73.11296178124047     
+BODY605_GM             153.9420572125665      153.9420079809344     
+BODY606_GM             8978.138848070126      8978.138641652298     
+BODY607_GM             0.370604084668938      0.370879439084761     
+BODY608_GM             120.5039090692674      120.4977883563631     
+BODY609_GM             0.5534188875932333     0.5535009498398994
+
+2007-Nov-27 (published)
+Automated Process
+
+Applicable current Ephemeris = 071127R_SCPSE_07221_07262.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 071004_050T36
+
+
+Parameter              Superceded Value       New Value
+
+
+BODY6_GM               37940584.84186901      37940584.33316191     
+BODY699_GM             37931207.2884          37931206.7900         
+BODY699_POLE_RA(1)     40.582641              40.581634             
+BODY699_POLE_DEC(1)    83.537724              83.537653             
+BODY699_JCOEF(2)       0.016290612479         0.016290573664        
+BODY699_JCOEF(4)       -0.000936294465        -0.000936412164       
+BODY699_JCOEF(6)       0.000085698631         0.000087338436        
+BODY601_GM             2.504049862130569      2.503976507903127     
+BODY602_GM             7.209384148992843      7.206823163853062     
+BODY603_GM             41.21155584587244      41.21053825232565     
+BODY604_GM             73.11290828235806      73.11294390332988     
+BODY605_GM             153.9424774264240      153.9420572125665     
+BODY606_GM             8978.141570596494      8978.138848070126     
+BODY607_GM             0.370570713135802      0.370604084668938     
+BODY608_GM             120.5076093230218      120.5039090692674     
+BODY609_GM             0.5533871680420684     0.5534188875932333 
+
+2007-Oct-18 (published)
+Automated Process
+
+Applicable current Ephemeris = 071017R_SCPSE_07191_07221.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070902_049T35
+
+
+Parameter              Superceded Value       New Value
+
+
+BODY6_GM               37940584.84332670      37940584.84186901     
+BODY699_GM             37931207.2932          37931207.2884         
+BODY699_POLE_RA(1)     40.582430              40.582641             
+BODY699_POLE_DEC(1)    83.537699              83.537724             
+BODY699_JCOEF(2)       0.016290600706         0.016290612479        
+BODY699_JCOEF(4)       -0.000936283456        -0.000936294465       
+BODY601_GM             2.504061092290415      2.504049862130569     
+BODY602_GM             7.208392748901111      7.209384148992843     
+BODY603_GM             41.21123661827443      41.21155584587244     
+BODY604_GM             73.11288907130644      73.11290828235806     
+BODY605_GM             153.9424024154587      153.9424774264240     
+BODY606_GM             8978.141410813654      8978.141570596494     
+BODY606_JCOEF(2)       0.00003601             0.00003300            
+BODY606_CCOEF(3)       0.0000090887           0.0000111800          
+BODY606_SCOEF(3)       0.0000006522           -0.0000003700         
+BODY607_GM             0.370732118387213      0.370570713135802     
+BODY608_GM             120.5055725066606      120.5076093230218     
+BODY609_GM             0.5534083195746095     0.5533871680420684    
+
+2007 August 23 (published)
+E. Martinez - modified by automated process
+
+Applicable current Ephemeris = 070822R_SCPSE_07170_07191.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070722_048T34
+
+
+Parameter              Superceded Value       New Value
+
+
+BODY6_GM               37940585.21293911      37940584.84332670     
+BODY699_GM             37931207.6624          37931207.2932         
+BODY699_POLE_RA(1)     40.582203              40.582430             
+BODY699_POLE_DEC(1)    83.537758              83.537699             
+BODY699_JCOEF(2)       0.016290558106         0.016290600706        
+BODY699_JCOEF(4)       -0.000936543536        -0.000936283456       
+BODY601_GM             2.504123199124006      2.504061092290415     
+BODY602_GM             7.208710372016743      7.208392748901111     
+BODY603_GM             41.21112748400978      41.21123661827443     
+BODY604_GM             73.11287036205675      73.11288907130644     
+BODY605_GM             153.9423057334808      153.9424024154587     
+BODY606_GM             8978.140644218034      8978.141410813654     
+BODY606_JCOEF(2)       0.00003886             0.00003601            
+BODY606_CCOEF(3)       0.0000090424           0.0000090887          
+BODY606_SCOEF(3)       0.0000006837           0.0000006522          
+BODY607_GM             0.371284081096715      0.370732118387213     
+BODY608_GM             120.5060708891759      120.5055725066606     
+BODY609_GM             0.5534250308405290     0.5534083195746095
+  
+
+
+2007 July 30 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070727R_SCPSE_07155_07170.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070703_047T33
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.17856981      37940585.21293911     
+BODY699_GM             37931207.6234          37931207.6624         
+BODY699_POLE_RA(1)     40.581027              40.582203             
+BODY699_POLE_DEC(1)    83.537733              83.537758             
+BODY699_JCOEF(2)       0.016290499156         0.016290558106        
+BODY699_JCOEF(4)       -0.000936368414        -0.000936543536       
+BODY699_JCOEF(6)       0.000085387817         0.000085698631        
+BODY601_GM             2.504414142228290      2.504123199124006     
+BODY602_GM             7.205528919131223      7.208710372016743     
+BODY603_GM             41.21396906165625      41.21112748400978     
+BODY604_GM             73.11211150967007      73.11287036205675     
+BODY605_GM             153.9421896011184      153.9423057334808     
+BODY606_GM             8978.144236041977      8978.140644218034     
+BODY606_JCOEF(2)       0.00003300             0.00003886            
+BODY606_CCOEF(3)       0.0000111800           0.0000090424          
+BODY606_SCOEF(3)       -0.0000003700          0.0000006837          
+BODY607_GM             0.370612570883980      0.371284081096715     
+BODY608_GM             120.5086247632435      120.5060708891759     
+BODY609_GM             0.5535133733207492     0.5534250308405290    
+
+
+2007 July 9 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070705R_SCPSE_07140_07155.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070616_046T32
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.08048513      37940585.17856981     
+BODY699_GM             37931207.5251          37931207.6234         
+BODY699_POLE_RA(1)     40.581004              40.581027             
+BODY699_JCOEF(2)       0.016290501183         0.016290499156        
+BODY699_JCOEF(4)       -0.000936480581        -0.000936368414       
+BODY601_GM             2.504411459582265      2.504414142228290     
+BODY602_GM             7.205523796006839      7.205528919131223     
+BODY603_GM             41.21397120396249      41.21396906165625     
+BODY604_GM             73.11210641361994      73.11211150967007     
+BODY605_GM             153.9421682125904      153.9421896011184     
+BODY606_GM             8978.144146129685      8978.144236041977     
+BODY607_GM             0.370679269434110      0.370612570883980     
+BODY608_GM             120.5088834664148      120.5086247632435     
+BODY609_GM             0.5535141277727101     0.5535133733207492   
+
+
+
+2007 June 25 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070625R_SCPSE_07125_07140.XSP
+ Restrictions/Limitations = Use for analysis for period of file.
+ Reference/Source of new values = 070531_045T31
+ PCK Produced by NAVT (070531_045T31) =     CASSINI_PCK_VERSION     = ( '2007-JUN-25' )
+
+
+ Parameter              Superceded Value       New Value
+
+ BODY6_GM               37940585.40297550      37940585.08048513     
+ BODY699_GM             37931207.8468          37931207.5251         
+ BODY699_POLE_RA(1)     40.581249              40.581004             
+ BODY699_POLE_DEC(1)    83.537722              83.537733             
+ BODY699_JCOEF(2)       0.016290482169         0.016290501183        
+ BODY699_JCOEF(4)       -0.000936661780        -0.000936480581       
+ BODY601_GM             2.504418526540353      2.504411459582265     
+ BODY602_GM             7.205822825717696      7.205523796006839     
+ BODY603_GM             41.21391693524110      41.21397120396249     
+ BODY604_GM             73.11210744224974      73.11210641361994     
+ BODY605_GM             153.9421724973921      153.9421682125904     
+ BODY606_GM             8978.144706785964      8978.144146129685     
+ BODY607_GM             0.370826890400237      0.370679269434110     
+ BODY608_GM             120.5086965046577      120.5088834664148     
+ BODY609_GM             0.5535193168614742     0.5535141277727101    
+
+
+
+
+2007 June 06 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070605R_SCPSE_07106_07125.BSP
+Restrictions/Limitations =
+Reference/Source of new values = 070516_044T30
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.38628557      37940585.40297550    
+BODY699_GM             37931207.8310          37931207.8468        
+BODY699_POLE_RA(1)     40.581289              40.581249            
+BODY699_POLE_DEC(1)    83.537733              83.537722            
+BODY699_JCOEF(2)       0.016290481702         0.016290482169       
+BODY699_JCOEF(4)       -0.000936637437        -0.000936661780      
+BODY601_GM             2.504419042580414      2.504418526540353    
+BODY602_GM             7.205961922976411      7.205822825717696    
+BODY603_GM             41.21392252150596      41.21391693524110    
+BODY604_GM             73.11208204909212      73.11210744224974    
+BODY605_GM             153.9421763278791      153.9421724973921    
+BODY606_GM             8978.144552352178      8978.144706785964    
+BODY607_GM             0.370847384392641      0.370826890400237    
+BODY608_GM             120.5078146418220      120.5086965046577    
+BODY609_GM             0.5535279925596653     0.5535193168614742   
+
+
+
+2007 May 17 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070517R_SCPSE_07094_07106.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070429_043T29
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.09724870      37940585.38628557
+BODY699_GM             37931207.5551          37931207.8310
+BODY699_POLE_RA(1)     40.580883              40.581289
+BODY699_POLE_RA(2)     -0.028212              -0.027530
+BODY699_POLE_DEC(1)    83.537754              83.537733
+BODY699_POLE_DEC(2)    -0.005007              -0.004758
+BODY699_JCOEF(2)       0.016290487287         0.016290481702
+BODY699_JCOEF(4)       -0.000936319857        -0.000936637437
+BODY699_JCOEF(6)       0.000085603492         0.000085387817
+BODY601_GM             2.503836439067691      2.504419042580414
+BODY602_GM             7.205091159985646      7.205961922976411
+BODY603_GM             41.21366740556955      41.21392252150596
+BODY604_GM             73.11206406733254      73.11208204909212
+BODY605_GM             153.9421167266536      153.9421763278791
+BODY606_GM             8978.139180360749      8978.144552352178
+BODY607_GM             0.370390019371346      0.370847384392641
+BODY608_GM             120.5021384592211      120.5078146418220
+BODY609_GM             0.5537054261288668     0.5535279925596653
+
+
+
+
+2007 May 8 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070507R_SCPSE_07077_07094.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070412_042T28
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.08153445      37940585.09724870
+BODY699_GM             37931207.5393          37931207.5551
+BODY699_POLE_RA(1)     40.580887              40.580883
+BODY699_POLE_DEC(1)    83.537760              83.537754
+BODY699_JCOEF(2)       0.016290487158         0.016290487287
+BODY699_JCOEF(4)       -0.000936645013        -0.000936319857
+BODY601_GM             2.503862387407351      2.503836439067691
+BODY602_GM             7.204709334179276      7.205091159985646
+BODY603_GM             41.21356636921946      41.21366740556955
+BODY604_GM             73.11207388515732      73.11206406733254
+BODY605_GM             153.9421590940140      153.9421167266536
+BODY606_GM             8978.139228648140      8978.139180360749
+BODY607_GM             0.370175811007482      0.370390019371346
+BODY608_GM             120.5026966204559      120.5021384592211
+BODY609_GM             0.5537453110625723     0.5537054261288668
+
+
+
+
+
+2007 May 1 (published)
+E.Martinez
+
+Applicable current Ephemeris = 070430R_SCPSE_07062_07077.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070328_041T27
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.17276487      37940585.08153445
+BODY699_GM             37931207.6257          37931207.5393
+BODY699_POLE_RA(1)     40.581183              40.580887
+BODY699_POLE_DEC(1)    83.537742              83.537760
+BODY699_JCOEF(2)       0.016290515129         0.016290487158
+BODY699_JCOEF(4)       -0.000936635353        -0.000936645013
+BODY601_GM             2.503852026860320      2.503862387407351
+BODY602_GM             7.204735734158900      7.204709334179276
+BODY603_GM             41.21342237725444      41.21356636921946
+BODY604_GM             73.11204651203829      73.11207388515732
+BODY605_GM             153.9422097818796      153.9421590940140
+BODY606_GM             8978.139349010102      8978.139228648140
+BODY607_GM             0.370710830099663      0.370175811007482
+BODY608_GM             120.5069073152362      120.5026966204559
+BODY609_GM             0.5537953815668963     0.5537453110625723
+
+
+
+2007 Apr. 5 (published)
+E.Martinez
+
+Applicable current Ephemeris = 070405R_SCPSE_07042_07062.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070311_040T26
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.33700632      37940585.17276487
+BODY699_GM             37931207.7897          37931207.6257
+BODY699_POLE_RA(1)     40.582138              40.581183
+BODY699_POLE_RA(2)     -0.042290              -0.028212
+BODY699_POLE_DEC(1)    83.537654              83.537742
+BODY699_POLE_DEC(2)    -0.004440              -0.005007
+BODY699_JCOEF(2)       0.016290641945         0.016290515129
+BODY699_JCOEF(4)       -0.000935668041        -0.000936635353
+BODY699_JCOEF(6)       0.000086164269         0.000085603492
+BODY601_GM             2.503876883191547      2.503852026860320
+BODY602_GM             7.204408649790674      7.204735734158900
+BODY603_GM             41.21355379903252      41.21342237725444
+BODY604_GM             73.11217921621768      73.11204651203829
+BODY605_GM             153.9423800317704      153.9422097818796
+BODY606_GM             8978.136240566020      8978.139349010102
+BODY607_GM             0.371098539685749      0.370710830099663
+BODY608_GM             120.5099185698973      120.5069073152362
+BODY609_GM             0.5536470952086257     0.5537953815668963
+
+
+
+2007 Mar. 12 (published)
+A. Tinio
+
+Applicable current Ephemeris = 070312R_SCPSE_07023_07042.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070227_039T25
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.33807337      37940585.33700632
+BODY699_GM             37931207.7915          37931207.7897
+BODY699_POLE_RA(1)     40.582215              40.582138
+BODY699_POLE_DEC(1)    83.537654              83.537655
+BODY699_JCOEF(2)       0.016290659210         0.016290641945
+BODY699_JCOEF(4)       -0.000935527451        -0.000935668041
+BODY601_GM             2.503837919690110      2.503876883191547
+BODY602_GM             7.204366436582808      7.204408649790674
+BODY603_GM             41.21350165765106      41.21355379903252
+BODY604_GM             73.11214683578255      73.11217921621768
+BODY605_GM             153.9423654046796      153.9423800317704
+BODY606_GM             8978.136205102190      8978.136240566020
+BODY607_GM             0.371098868424698      0.371098539685749
+BODY608_GM             120.5093717224557      120.5099185698973
+BODY609_GM             0.5536729212172495     0.5536470952086257
+
+
+2007 Feb. 14 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070213R_SCPSE_07008_07023.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070131_038T24
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.37672914      37940585.33807337
+BODY699_GM             37931207.8307          37931207.7915
+BODY699_POLE_RA(1)     40.582442              40.582215
+BODY699_POLE_DEC(1)    83.537638              83.537654
+BODY699_JCOEF(2)       0.016290689119         0.016290659210
+BODY699_JCOEF(4)       -0.000935639203        -0.000935527451
+BODY601_GM             2.503846655611214      2.503837919690110
+BODY602_GM             7.204437093644860      7.204366436582808
+BODY603_GM             41.21355196667208      41.21350165765106
+BODY604_GM             73.11210070783861      73.11214683578255
+BODY605_GM             153.9424390527431      153.9423654046796
+BODY606_GM             8978.134670303732      8978.136205102190
+BODY607_GM             0.372265820288520      0.371098868424698
+BODY608_GM             120.5089822796373      120.5093717224557
+BODY609_GM             0.5537139855259471     0.5536729212172495
+
+
+
+2007 Feb. 10 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070209AP_SK_06356_08222.BSP
+Restrictions/Limitations = Use for planning for span of file.
+Reference/Source of new values = 061122_034Sa
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.43553244      37940585.37672914
+BODY699_GM             37931207.8926          37931207.8307
+BODY699_POLE_RA(1)     40.582332              40.582442
+BODY699_POLE_DEC(1)    83.537646              83.537638
+BODY699_JCOEF(2)       0.016290673275         0.016290689119
+BODY699_JCOEF(4)       -0.000935553602        -0.000935639203
+BODY601_GM             2.503839997455295      2.503846655611214
+BODY602_GM             7.204479017295238      7.204437093644860
+BODY603_GM             41.21348039992097      41.21355196667208
+BODY604_GM             73.11210988012873      73.11210070783861
+BODY605_GM             153.9424056799695      153.9424390527431
+BODY606_GM             8978.134379445051      8978.134670303732
+BODY606_JCOEF(2)       0.00003174             0.00003300
+BODY606_CCOEF(3)       0.0000092806           0.0000111800
+BODY606_SCOEF(3)       0.0000000000           -0.0000003700
+BODY607_GM             0.370859756936743      0.372265820288520
+BODY608_GM             120.5077275524120      120.5089822796373
+BODY609_GM             0.5536709288276324     0.5537139855259471
+
+
+
+2007 Jan. 26 (published)2007 Jan. 26 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070125R_SCPSE_06342_06356.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061231a_036T22
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.47883564      37940585.43553244
+BODY699_GM             37931207.9327          37931207.8926
+BODY699_POLE_RA(1)     40.582379              40.582332
+BODY699_POLE_DEC(1)    83.537643              83.537646
+BODY699_JCOEF(2)       0.016290679648         0.016290673275
+BODY699_JCOEF(4)       -0.000935644640        -0.000935553602
+BODY601_GM             2.503831680306900      2.503839997455295
+BODY602_GM             7.204371760563005      7.204479017295238
+BODY603_GM             41.21355129362405      41.21348039992097
+BODY604_GM             73.11211256265864      73.11210988012873
+BODY605_GM             153.9423945784529      153.9424056799695
+BODY606_GM             8978.134682483926      8978.134379445051
+BODY606_JCOEF(2)       0.00003300             0.00003174
+BODY606_CCOEF(3)       0.0000111800           0.0000092806
+BODY606_SCOEF(3)       -0.0000003700          0.0000000000
+BODY607_GM             0.371995143043160      0.370859756936743
+BODY608_GM             120.5094986156859      120.5077275524120
+BODY609_GM             0.5537065233590567     0.5536709288276324
+
+
+
+2007 Jan. 17 ( published )
+E. Martinez
+
+Applicable current Ephemeris = 070117R_SCPSE_06332_06342.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061214_035T21
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.40103932      37940585.47883564
+BODY699_GM             37931207.8546          37931207.9327
+BODY699_POLE_RA(1)     40.582415              40.582379
+BODY699_POLE_DEC(1)    83.537640              83.537643
+BODY699_JCOEF(2)       0.016290697390         0.016290679648
+BODY699_JCOEF(4)       -0.000935496137        -0.000935644640
+BODY601_GM             2.503829742547669      2.503831680306900
+BODY602_GM             7.204465583009808      7.204371760563005
+BODY603_GM             41.21349540009213      41.21355129362405
+BODY604_GM             73.11214005633310      73.11211256265864
+BODY605_GM             153.9423658347898      153.9423945784529
+BODY606_GM             8978.134661912558      8978.134682483926
+BODY607_GM             0.372269207385233      0.371995143043160
+BODY608_GM             120.5094670844839      120.5094986156859
+BODY609_GM             0.5537061797030824     0.5537065233590567
+
+
+2007 Jan. 10 ( published )
+E. Martinez
+
+Applicable current Ephemeris = 070109R_SCPSE_06318_06332.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061211_034Sa
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.32441469      37940585.40103932
+BODY699_GM             37931207.7782          37931207.8546
+BODY699_POLE_RA(1)     40.582617              40.582415
+BODY699_POLE_DEC(1)    83.537610              83.537640
+BODY699_JCOEF(2)       0.016290678494         0.016290697390
+BODY699_JCOEF(4)       -0.000935768820        -0.000935496137
+BODY601_GM             2.503836592945681      2.503829742547669
+BODY602_GM             7.204644742649264      7.204465583009808
+BODY603_GM             41.21354261332835      41.21349540009213
+BODY604_GM             73.11209408451387      73.11214005633310
+BODY605_GM             153.9424492343117      153.9423658347898
+BODY606_GM             8978.134681720063      8978.134661912558
+BODY607_GM             0.372280925349763      0.372269207385233
+BODY608_GM             120.5090050942508      120.5094670844839
+BODY609_GM             0.5537188622437070     0.5537061797030824
+
+   
+2006 Dec. 14  ( published )
+E. Martinez
+
+Applicable current Ephemeris = 061213R_SCPSE_06308_06318.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061127a_033Sa
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.29559930      37940585.32441469
+BODY699_GM             37931207.7534          37931207.7782
+BODY699_POLE_RA(1)     40.582407              40.582617
+BODY699_POLE_DEC(1)    83.537630              83.537610
+BODY699_JCOEF(2)       0.016290705447         0.016290678494
+BODY699_JCOEF(4)       -0.000935475070        -0.000935768820
+BODY601_GM             2.503858603857476      2.503836592945681
+BODY602_GM             7.204382802668946      7.204644742649264
+BODY603_GM             41.21362206412197      41.21354261332835
+BODY604_GM             73.11209645069110      73.11209408451387
+BODY605_GM             153.9424779310557      153.9424492343117
+BODY606_GM             8978.134414593294      8978.134681720063
+BODY607_GM             0.371810775100716      0.372280925349763
+BODY608_GM             120.5058167650734      120.5090050942508
+BODY609_GM             0.5537093920200542     0.5537188622437070
+
+
+
+2006 Dec. 01  ( published )
+E. Martinez
+
+Applicable current Ephemeris = 061129R_SCPSE_06292_06307.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061114_032Sa
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.24138311      37940585.29559930
+BODY699_GM             37931207.6992          37931207.7534
+BODY699_POLE_RA(1)     40.582380              40.582407
+BODY699_POLE_DEC(1)    83.537628              83.537630
+BODY699_JCOEF(2)       0.016290694538         0.016290705447
+BODY699_JCOEF(4)       -0.000935172730        -0.000935475070
+BODY699_JCOEF(6)       0.000086032043         0.000086164269
+BODY601_GM             2.504045173937001      2.503858603857476
+BODY602_GM             7.204489862685024      7.204382802668946
+BODY603_GM             41.21355396165882      41.21362206412197
+BODY604_GM             73.11209017356970      73.11209645069110
+BODY605_GM             153.9424477351946      153.9424779310557
+BODY606_GM             8978.134479689157      8978.134414593294
+BODY607_GM             0.372161757032882      0.371810775100716
+BODY608_GM             120.5055622185648      120.5058167650734
+BODY609_GM             0.5533481483735110     0.5537093920200542
+
+
+
+2006 Nov. 16  ( published )
+E. Martinez
+
+Applicable current Ephemeris = 061116R_SCPSE_06276_06292.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061029_031T20
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.28556997      37940585.24138311
+BODY699_GM             37931207.7383          37931207.6992
+BODY699_POLE_RA(1)     40.582563              40.582380
+BODY699_POLE_DEC(1)    83.537609              83.537628
+BODY699_JCOEF(2)       0.016290723281         0.016290694538
+BODY699_JCOEF(4)       -0.000934943222        -0.000935172730
+BODY601_GM             2.504039758351044      2.504045173937001
+BODY602_GM             7.204635369705422      7.204489862685024
+BODY603_GM             41.21351788474261      41.21355396165882
+BODY604_GM             73.11206102463274      73.11209017356970
+BODY605_GM             153.9424093566678      153.9424477351946
+BODY606_GM             8978.134640768996      8978.134479689157
+BODY607_GM             0.372257378997563      0.372161757032882
+BODY608_GM             120.5103787968222      120.5055622185648
+BODY609_GM             0.5533513566819516     0.5533481483735110
+
+
+2006 Nov. 08  ( published )
+A. Tinio
+
+Applicable current Ephemeris = 061108R_SCPSE_06260_06276.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061013_030T19
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.20804367      37940585.28556997
+BODY699_GM             37931207.6506          37931207.7383
+BODY699_POLE_RA(1)     40.582917              40.582563
+BODY699_POLE_DEC(1)    83.537562              83.537609
+BODY699_JCOEF(2)       0.016290681360         0.016290723281
+BODY699_JCOEF(4)       -0.000935220317        -0.000934943222
+BODY601_GM             2.504056364254555      2.504039758351044
+BODY602_GM             7.205444446422798      7.204635369705422
+BODY603_GM             41.21340329716050      41.21351788474261
+BODY604_GM             73.11208185666693      73.11206102463274
+BODY605_GM             153.9423994589908      153.9424093566678
+BODY606_GM             8978.134885749399      8978.134640768996
+BODY607_GM             0.372103146260205      0.372257378997563
+BODY608_GM             120.5197010249014      120.5103787968222
+BODY609_GM             0.5533956626324310     0.5533513566819516
+
+2006 Oct. 16  ( published )
+A. Tinio
+
+Applicable current Ephemeris = 061013R_SCPSE_06240_06260.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060926_029T18
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.30041119      37940585.20804367
+BODY699_GM             37931207.7563          37931207.6506
+BODY699_POLE_RA(1)     40.582624              40.582917
+BODY699_POLE_DEC(1)    83.537604              83.537562
+BODY699_JCOEF(2)       0.016290700509         0.016290681360
+BODY699_JCOEF(4)       -0.000935268588        -0.000935220317
+BODY699_JCOEF(6)       0.000086306565         0.000086032043
+BODY601_GM             2.503234184380379      2.504056364254555
+BODY602_GM             7.205788388974169      7.205444446422798
+BODY603_GM             41.20921386093631      41.21340329716050
+BODY604_GM             73.11256958878700      73.11208185666693
+BODY605_GM             153.9427794181101      153.9423994589908
+BODY606_GM             8978.134842412568      8978.134885749399
+BODY607_GM             0.371655593766023      0.372103146260205
+BODY608_GM             120.5107561184160      120.5197010249014
+BODY609_GM             0.5533087871633449     0.5533956626324310
+
+2006 Sep. 26  ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060925R_SCPSE_06217_06240.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060910_028T17
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.37202547      37940585.30041119
+BODY699_GM             37931207.8298          37931207.7563
+BODY699_POLE_RA(1)     40.582733              40.582624
+BODY699_POLE_DEC(1)    83.537616              83.537604
+BODY699_JCOEF(2)       0.016290681525         0.016290700509
+BODY699_JCOEF(4)       -0.000935830959        -0.000935268588
+BODY601_GM             2.503237817457834      2.503234184380379
+BODY602_GM             7.205571530617301      7.205788388974169
+BODY603_GM             41.20912316700146      41.20921386093631
+BODY604_GM             73.11254700746446      73.11256958878700
+BODY605_GM             153.9427536730286      153.9427794181101
+BODY606_GM             8978.134866382321      8978.134842412568
+BODY607_GM             0.372358845972800      0.371655593766023
+BODY608_GM             120.5084733163531      120.5107561184160
+BODY609_GM             0.5532645857684702     0.5533087871633449
+
+2006 Sep. 07  ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060907R_SCPSE_06193_06228.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060815_027Sa
+
+Parameter              Superceded Value       New Value
+
+BODY10_GM              132712440017.9870      132712440044.2083
+BODY2_GM               324858.598826460       324858.598890645
+BODY3_GM               403503.233479087       403503.2335605171
+BODY399_GM             398600.4328969392      398600.4334392727
+BODY5_GM               126712767.8577960      126712764.8582231
+BODY599_GM             126686536.9610660      126686533.9614931
+BODY6_GM               37940585.21804788      37940585.37202547
+BODY699_GM             37931207.6691          37931207.8298
+BODY699_POLE_RA(1)     40.582843              40.582733
+BODY699_POLE_DEC(1)    83.537599              83.537616
+BODY699_JCOEF(2)       0.016290708626         0.016290681525
+BODY699_JCOEF(4)       -0.000935838573        -0.000935830959
+BODY699_JCOEF(6)       0.000086144219         0.000086306565
+BODY7_GM               5794549.007071874      5794549.008216757
+BODY301_GM             4902.800582147764      4902.800121244415
+BODY601_GM             2.502372648309949      2.503237817457834
+BODY602_GM             7.209633248592259      7.205571530617301
+BODY603_GM             41.20971288406673      41.20912316700146
+BODY604_GM             73.11266255598086      73.11254700746446
+BODY605_GM             153.9415996603182      153.9427536730286
+BODY606_GM             8978.135697583817      8978.134866382321
+BODY607_GM             0.371269445627224      0.372358845972800
+BODY608_GM             120.5126041600149      120.5084733163531
+BODY609_GM             0.5534414535788157     0.5532645857684702
+
+
+
+2006 AUG 11 ( published )
+E. Martinez, A. Tinio
+
+Applicable current Ephemeris = 060810R_SCPSE_06162_06193.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060723_026T16
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.19817787      37940585.21804788
+BODY699_GM             37931207.6481          37931207.6691
+BODY699_POLE_RA(1)     40.582804              40.582843
+BODY699_POLE_DEC(1)    83.537620              83.537599
+BODY699_JCOEF(2)       0.016290723295         0.016290708626
+BODY699_JCOEF(4)       -0.000935636528        -0.000935838573
+BODY601_GM             2.502337374431450      2.502372648309949
+BODY602_GM             7.209594537754957      7.209633248592259
+BODY603_GM             41.20980224942576      41.20971288406673
+BODY604_GM             73.11265768420897      73.11266255598086
+BODY605_GM             153.9415837936022      153.9415996603182
+BODY606_GM             8978.135361988159      8978.135697583817
+BODY607_GM             0.372568723578752      0.371269445627224
+BODY608_GM             120.5127058469105      120.5126041600149
+BODY609_GM             0.5534333052090450     0.5534414535788157
+
+
+
+2006 July 20 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060719R_SCPSE_06130_06162.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060705a_025T15
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.02377836      37940585.19817787
+BODY699_GM             37931207.4828          37931207.6481
+BODY699_POLE_RA(1)     40.582022              40.582804
+BODY699_POLE_DEC(1)    83.537664              83.537620
+BODY699_JCOEF(2)       0.016290719439         0.016290723295
+BODY699_JCOEF(4)       -0.000934406276        -0.000935636528
+BODY699_JCOEF(6)       0.000086620067         0.000086144219
+BODY601_GM             2.503149740351328      2.502337374431450
+BODY602_GM             7.208872923723865      7.209594537754957
+BODY603_GM             41.20029810761654      41.20980224942576
+BODY604_GM             73.11284780426027      73.11265768420897
+BODY605_GM             153.9402009786583      153.9415837936022
+BODY606_GM             8978.137295144839      8978.135361988159
+BODY607_GM             0.372172625164198      0.372568723578752
+BODY608_GM             120.5128842735845      120.5127058469105
+BODY609_GM             0.5532749466908186     0.5534333052090450
+
+2006 June 14 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060614R_SCPSE_06099_06130.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060521_024T14
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.00869015      37940585.02377836
+BODY699_GM             37931207.4702          37931207.4828
+BODY699_POLE_RA(1)     40.581940              40.582022
+BODY699_POLE_DEC(1)    83.537665              83.537664
+BODY699_JCOEF(2)       0.016290720625         0.016290719439
+BODY699_JCOEF(4)       -0.000934485800        -0.000934406276
+BODY601_GM             2.503155504246730      2.503149740351328
+BODY602_GM             7.208672940445637      7.208872923723865
+BODY603_GM             41.20030999725930      41.20029810761654
+BODY604_GM             73.11284902953261      73.11284780426027
+BODY605_GM             153.9401720253013      153.9402009786583
+BODY606_GM             8978.137600869284      8978.137295144839
+BODY607_GM             0.372187991611717      0.372172625164198
+BODY608_GM             120.5102865422368      120.5128842735845
+BODY609_GM             0.5532644770436360     0.5532749466908186
+
+
+
+2006 MAY 15 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060515R_SCPSE_06068_06099.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060503_023T13
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.82178953      37940585.00869015
+BODY699_GM             37931207.2824          37931207.4702
+BODY699_POLE_RA(1)     40.580240              40.581940
+BODY699_POLE_DEC(1)    83.537779              83.537665
+BODY699_JCOEF(2)       0.016290675629         0.016290720625
+BODY699_JCOEF(4)       -0.000935190949        -0.000934485800
+BODY699_JCOEF(6)       0.000086898078         0.000086620067
+BODY601_GM             2.503244068708538      2.503155504246730
+BODY602_GM             7.208175153748505      7.208672940445637
+BODY603_GM             41.20088341434613      41.20030999725930
+BODY604_GM             73.11295205736538      73.11284902953261
+BODY605_GM             153.9401465123193      153.9401720253013
+BODY606_GM             8978.135422689342      8978.137600869284
+BODY606_JCOEF(2)       0.00003301             0.00003300
+BODY606_CCOEF(3)       0.0000111790           0.0000111800
+BODY606_SCOEF(3)       -0.0000003683          -0.0000003700
+BODY607_GM             0.372225170143269      0.372187991611717
+BODY608_GM             120.5131683419617      120.5102865422368
+BODY609_GM             0.5532134715796430     0.5532644770436360
+
+2006 Apr 18 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060417R_SCPSE_06036_06068.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060320_022T12
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.02189582      37940584.82178953
+BODY699_GM             37931207.4768          37931207.2824
+BODY699_POLE_RA(1)     40.582939              40.580240
+BODY699_POLE_DEC(1)    83.537574              83.537779
+BODY699_JCOEF(2)       0.016290752164         0.016290675629
+BODY699_JCOEF(4)       -0.000935531632        -0.000935190949
+BODY699_JCOEF(6)       0.000086130696         0.000086898078
+BODY601_GM             2.503196140438530      2.503244068708538
+BODY602_GM             7.209302177761134      7.208175153748505
+BODY603_GM             41.19976930418225      41.20088341434613
+BODY604_GM             73.11284795021615      73.11295205736538
+BODY605_GM             153.9400292807456      153.9401465123193
+BODY606_GM             8978.135208156255      8978.135422689342
+BODY606_JCOEF(2)       0.00003349             0.00003301
+BODY606_CCOEF(3)       0.0000110747           0.0000111790
+BODY606_SCOEF(3)       -0.0000003502          -0.0000003683
+BODY607_GM             0.373150368272270      0.372225170143269
+BODY608_GM             120.5182054679503      120.5131683419617
+BODY609_GM             0.5533715466786809     0.5532134715796430
+
+2006 Mar 21 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060321_SCPSE_06005_06036.XSP 
+Restrictions/Limitations = Use for analysis for period of file. 
+Reference/Source of new values = 060301_021T11
+
+Parameter               Superceded Value     New Value
+BODY6_GM                37940584.95359504    37940585.02189582 
+BODY699_GM              37931207.4118        37931207.4768 
+BODY699_POLE_RA(1)      40.582515            40.582939 
+BODY699_POLE_DEC(1)     83.537604            83.537574 
+BODY699_JCOEF(2)        0.016290685585       0.016290752164 
+BODY699_JCOEF(4)        -0.000935841110      -0.000935531632 
+BODY601_GM              2.503209168287056    2.503196140438530 
+BODY602_GM              7.208811870736135    7.209302177761134 
+BODY603_GM              41.19992642786966    41.19976930418225 
+BODY604_GM              73.11284728090631    73.11284795021615 
+BODY605_GM              153.9399206434808    153.9400292807456 
+BODY606_GM              8978.134804759919    8978.135208156255 
+BODY606_JCOEF(2)        0.00003320           0.00003349 
+BODY606_CCOEF(3)        0.0000111862         0.0000110747 
+BODY606_SCOEF(3)        -0.0000003715220     -0.0000003502 
+BODY607_GM              0.372786047857714    0.373150368272270 
+BODY608_GM              120.5161788220962    120.5182054679503 
+BODY609_GM              0.5533583156478464   0.5533715466786809
+
+
+2006 Mar 15 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060323AP_SK_06082_08222.XSP
+Restrictions/Limitations = Use for Ref. Traj. planning for period of file
+Reference/Source of new values = 060301_022T12
+
+
+
+Parameter              Superceded Value       New Value
+
+
+BODY6_GM               37940584.97838498      37940584.95359504
+BODY699_GM             37931207.4218          37931207.4118
+BODY699_POLE_RA(1)     40.582375              40.582515
+BODY699_POLE_DEC(1)    83.537622              83.537604
+BODY699_JCOEF(2)       0.016290660391         0.016290685585
+BODY699_JCOEF(4)       -0.000935797472        -0.000935841110
+BODY601_GM             2.503255490608568      2.503209168287056
+BODY602_GM             7.208151961640861      7.208811870736135
+BODY603_GM             41.19986045608409      41.19992642786966
+BODY604_GM             73.11282801626780      73.11284728090631
+BODY605_GM             153.9400039367874      153.9399206434808
+BODY606_GM             8978.145353251261      8978.134804759919
+BODY606_JCOEF(2)       0.00002640             0.00003320
+BODY606_CCOEF(3)       0.0000079              0.0000111862
+BODY606_SCOEF(3)                              -0.0000003715220 *
+BODY607_GM             0.372587254705434      0.372786047857714
+BODY608_GM             120.5211143157129      120.5161788220962
+BODY609_GM             0.5533806776787945     0.5533583156478464
+
+
+* Note: Titan tesseral harmonic, BODY606_SCOEF(3), is included with this
+  delivery:
+  BODY606_SCOEF = ( 0.0,     0.0,     -0.0000003715220 )
+
+
+2006 Feb 14 ( published )
+A. Tinio
+
+Applicable current Ephemeris =  060213R_SCPSE_05348_06005.XSP
+Restrictions/Limitations =  Use for analysis for period of file.
+Reference/Source of new values = 060121_020T10
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.15649380      37940584.97838498
+BODY699_GM             37931207.5978          37931207.4218
+BODY699_POLE_RA(1)     40.582823              40.582375
+BODY699_POLE_DEC(1)    83.537575              83.537622
+BODY699_JCOEF(2)       0.016290651631         0.016290660391
+BODY699_JCOEF(4)       -0.000935923828        -0.000935797472
+BODY699_JCOEF(6)       0.000086273874         0.000086130696
+BODY601_GM             2.503473438509435      2.503255490608568
+BODY602_GM             7.208482454021635      7.208151961640861
+BODY603_GM             41.20142512691800      41.19986045608409
+BODY604_GM             73.11291388000183      73.11282801626780
+BODY605_GM             153.9397981709559      153.9400039367874
+BODY606_GM             8978.155502709762      8978.145353251261
+BODY607_GM             0.372499954808899      0.372587254705434
+BODY608_GM             120.5112356389298      120.5211143157129
+BODY609_GM             0.5533569886802691     0.5533806776787945
+
+Additionally, as provided in "Cassini Planetary Constants Usage Policy,
+Contents, and Update Process" (Rev. E, 16-Apr-2003) and OIA IO-043, the
+Cassini Navigation Team will be estimating some satellite values for
+J2 and C22.  The keywords for these coefficients will be of the forms:
+        BODY<nnn>_JCOEF       where <nnn> would be 601, 602, etc.
+        BODY<nnn>_CCOEF
+and the pck values would be:
+        ( 0.0, <J2> )    for J2 gravitational coefficients
+and     ( 0.0, 0.0, <C22> )  for C22 gravitational coefficients
+
+These current unnormalized values are available with this reconstruction:
+
+BODY602_JCOEF = ( 0.0, 0.00897 )
+BODY602_CCOEF = ( 0.0, 0.0, 0.00208 )
+
+BODY604_JCOEF = ( 0.0, 0.0012 )
+BODY604_CCOEF = ( 0.0, 0.0, 0.000361 )
+
+BODY605_JCOEF = ( 0.0, 0.000941 )
+BODY605_CCOEF = ( 0.0, 0.0, 0.000232 )
+
+BODY606_JCOEF = ( 0.0, 0.0000264 )
+BODY606_CCOEF = ( 0.0, 0.0, 0.0000079 )
+
+
+2006 Jan 12 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060111R_SCPSE_05320_05348.BSP
+Restrictions/Limitations =  Use for period of file.
+Reference/Source of new values = 051230_019T9
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.17590274      37940585.15649380
+BODY699_GM             37931207.6326          37931207.5978
+BODY699_POLE_RA(1)     40.583157              40.582823
+BODY699_POLE_DEC(1)    83.537570              83.537575
+BODY699_JCOEF(2)       0.016290685708         0.016290651631
+BODY699_JCOEF(4)       -0.000935953100        -0.000935923828
+BODY601_GM             2.503462470043706      2.503473438509435
+BODY602_GM             7.208374326151627      7.208482454021635
+BODY603_GM             41.20155898244365      41.20142512691800
+BODY604_GM             73.11290821305468      73.11291388000183
+BODY605_GM             153.9375651420232      153.9397981709559
+BODY606_GM             8978.161222465345      8978.155502709762
+BODY607_GM             0.372677926980588      0.372499954808899
+BODY608_GM             120.4921877511916      120.5112356389298
+BODY609_GM             0.5533233423151438     0.5533569886802691
+
+
+2005 Dec 13 ( published )
+A. Tinio
+
+Applicable current Ephemeris =   051213R_SCPSE_05293_05320.XSP
+Restrictions/Limitations =   Use for the period of this file
+Reference/Source of new values =   051128_018R1
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.24828158      37940585.17590274
+BODY699_GM             37931207.6394          37931207.6326
+BODY699_POLE_RA(1)     40.583441              40.583157
+BODY699_POLE_DEC(1)    83.537544              83.537570
+BODY699_JCOEF(2)       0.016290736784         0.016290685708
+BODY699_JCOEF(4)       -0.000935509628        -0.000935953100
+BODY601_GM             2.503432899195495      2.503462470043706
+BODY602_GM             7.208135453630815      7.208374326151627
+BODY603_GM             41.20196588064624      41.20155898244365
+BODY604_GM             73.11281403854379      73.11290821305468
+BODY605_GM             153.9961391059971      153.9375651420232
+BODY606_GM             8978.161488269006      8978.161222465345
+BODY607_GM             0.372813948978216      0.372677926980588
+BODY608_GM             120.4987924024436      120.4921877511916
+BODY609_GM             0.5533036326727672     0.5533233423151438
+
+
+2005 Nov 15 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 051114R_SCPSE_05275_05293.XSP
+Restrictions/Limitations = Use for tour analysis for period of file.
+Reference/Source of new values = 051031_017T8
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.30229028      37940585.24828158
+BODY699_GM             37931207.6574          37931207.6394
+BODY699_POLE_RA(1)     40.581524              40.583441
+BODY699_POLE_DEC(1)    83.537351              83.537544
+BODY699_JCOEF(2)       0.016290658643         0.016290736784
+BODY699_JCOEF(4)       -0.000935977180        -0.000935509628
+BODY699_JCOEF(6)       0.000085916004         0.000086273874
+BODY601_GM             2.521377772727696      2.503432899195495
+BODY602_GM             7.203310617192614      7.208135453630815
+BODY603_GM             41.20404503620523      41.20196588064624
+BODY604_GM             73.11270278320977      73.11281403854379
+BODY605_GM             154.0177629113878      153.9961391059971
+BODY606_GM             8978.157972403947      8978.161488269006
+BODY607_GM             0.371499507966020      0.372813948978216
+BODY608_GM             120.5028956594414      120.4987924024436
+BODY609_GM             0.5532983200668332     0.5533036326727672
+
+2005 Oct 21 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 051021R_SCPSE_05257_05275.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 051012_016D1
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.34349760      37940585.30229028
+BODY699_GM             37931207.6943          37931207.6574
+BODY699_POLE_RA(1)     40.582979              40.581524
+BODY699_POLE_DEC(1)    83.537892              83.537351
+BODY699_JCOEF(2)       0.016290717890         0.016290658643
+BODY699_JCOEF(4)       -0.000935625703        -0.000935977180
+BODY699_JCOEF(6)       0.000086359935         0.000085916004
+BODY601_GM             2.526812031114878      2.521377772727696
+BODY602_GM             7.209128567822218      7.203310617192614
+BODY603_GM             41.20938175350662      41.20404503620523
+BODY604_GM             73.11311455024394      73.11270278320977
+BODY605_GM             153.9760788846642      154.0177629113878
+BODY606_GM             8978.189785708180      8978.157972403947
+BODY607_GM             0.371309980105878      0.371499507966020
+BODY608_GM             120.5004502021633      120.5028956594414
+BODY609_GM             0.5531785509595187     0.5532983200668332
+
+2005 Oct 11 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 051011R_SCPSE_05245_05257.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 050927_015H1
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.31875592      37940585.34349760
+BODY699_GM             37931207.6724          37931207.6943
+BODY699_POLE_RA(1)     40.582875              40.582979
+BODY699_POLE_DEC(1)    83.537914              83.537892
+BODY699_JCOEF(2)       0.016290698730         0.016290717890
+BODY699_JCOEF(4)       -0.000935658433        -0.000935625703
+BODY601_GM             2.527676231780819      2.526812031114878
+BODY602_GM             7.208873373966934      7.209128567822218
+BODY603_GM             41.20956001485827      41.20938175350662
+BODY604_GM             73.11311058244327      73.11311455024394
+BODY605_GM             153.9761508783966      153.9760788846642
+BODY606_GM             8978.186036934201      8978.189785708180
+BODY607_GM             0.372357313080731      0.371309980105878
+BODY608_GM             120.4994492669644      120.5004502021633
+BODY609_GM             0.5531399174985459     0.5531785509595187
+
+
+2005 Sep 23 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 050922R_SCPSE_05225_05245.XSP
+Restrictions/Limitations =  Use for analysis for period of file.
+Reference/Source of new values = 050911_014T7
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.41646386      37940585.31875592
+BODY699_GM             37931207.7502          37931207.6724
+BODY699_POLE_RA(1)     40.583323              40.582875
+BODY699_POLE_DEC(1)    83.537945              83.537914
+BODY699_JCOEF(2)       0.016290703868         0.016290698730
+BODY699_JCOEF(4)       -0.000935636535        -0.000935658433
+BODY601_GM             2.527433358438375      2.527676231780819
+BODY602_GM             7.209550965627096      7.208873373966934
+BODY603_GM             41.20955753634430      41.20956001485827
+BODY604_GM             73.11310547668840      73.11311058244327
+BODY605_GM             153.9913950111069      153.9761508783966
+BODY606_GM             8978.185336761786      8978.186036934201
+BODY607_GM             0.375014936981534      0.372357313080731
+BODY608_GM             120.5017530353315      120.4994492669644
+BODY609_GM             0.5530820911204722     0.5531399174985459
+
+
+
+2005 Sep 08 ( published )
+A. Tinio
+
+Applicable current Ephemeris =   050907R_SCPSE_05205_05225.XSP
+Restrictions/Limitations =   Use for period of this file.
+Reference/Source of new values =   050824_013T6
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.61194924      37940585.41646386
+BODY699_GM             37931207.9363          37931207.7502
+BODY699_POLE_RA(1)     40.583019              40.583323
+BODY699_POLE_DEC(1)    83.537961              83.537945
+BODY699_JCOEF(2)       0.016290685394         0.016290703868
+BODY699_JCOEF(4)       -0.000935967005        -0.000935636535
+BODY601_GM             2.529211216189956      2.527433358438375
+BODY602_GM             7.212376404520326      7.209550965627096
+BODY603_GM             41.20963906707048      41.20955753634430
+BODY604_GM             73.11308526750042      73.11310547668840
+BODY605_GM             153.9923043182035      153.9913950111069
+BODY606_GM             8978.187230684733      8978.185336761786
+BODY607_GM             0.374716668929412      0.375014936981534
+BODY608_GM             120.5039579116963      120.5017530353315
+BODY609_GM             0.5530851646858529     0.5530820911204722
+
+
+
+2005 Aug 26 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 050825R_SCPSE_05186_05205.XSP
+Restrictions/Limitations = Use for data analysis for period of file.
+Reference/Source of new values = 050802_012Sa
+
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940585.41331755      37940585.61194924
+BODY699_GM             37931207.8002          37931207.9363
+BODY699_POLE_RA(1)     40.584385              40.583019
+BODY699_POLE_DEC(1)    83.537627              83.537961
+BODY699_JCOEF(2)       0.016290804116         0.016290685394
+BODY699_JCOEF(4)       -0.000933504702        -0.000935967005
+BODY699_JCOEF(6)       0.000092477088         0.000086359935
+BODY601_GM             2.526772990931723      2.529211216189956
+BODY602_GM             7.208888578402212      7.212376404520326
+BODY603_GM             41.20493245127680      41.20963906707048
+BODY604_GM             73.11277252343461      73.11308526750042
+BODY605_GM             153.9672076132773      153.9923043182035
+BODY606_GM             8978.166527318963      8978.187230684733
+BODY607_GM             0.378337733413031      0.374716668929412
+BODY608_GM             120.4944120884058      120.5039579116963
+BODY609_GM             0.5532264432054191     0.5530851646858529
+
+
+2005 Aug 02 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 050802R_SCPSE_05169_05186.XSP
+Restrictions/Limitations = Use for period of file.
+Reference/Source of new values = 050718_011E2
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940584.32393724      37940585.41331755
+BODY699_GM             37931206.6260          37931207.8002
+BODY699_POLE_RA(1)     40.582524              40.584385
+BODY699_POLE_DEC(1)    83.537645              83.537627
+BODY699_JCOEF(2)       0.016290795528         0.016290804116
+BODY699_JCOEF(4)       -0.000932738706        -0.000933504702
+BODY601_GM             2.530120927277264      2.526772990931723
+BODY602_GM             7.210665451438561      7.208888578402212
+BODY603_GM             41.20659404333172      41.20493245127680
+BODY604_GM             73.11260446242133      73.11277252343461
+BODY605_GM             154.0186476847478      153.9672076132773
+BODY606_GM             8978.179855914042      8978.166527318963
+BODY607_GM             0.378215663233720      0.378337733413031
+BODY608_GM             120.5079215829297      120.4944120884058
+BODY609_GM             0.5532635543008535     0.5532264432054191
+
+
+2005 Jul 11 ( published )
+A. Tinio
+
+Applicable current Ephemeris =  050708R_SCPSE_05150_05169.XSP
+Restrictions/Limitations =  Use for period of file.
+Reference/Source of new values = 050707_010Sa
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940571.43290575      37940584.32393724
+BODY699_GM             37931193.7263          37931206.6260
+BODY699_POLE_RA(1)     40.58051               40.582524
+BODY699_POLE_DEC(1)    83.537912              83.537645
+BODY699_JCOEF(2)       0.016290989185         0.016290795528
+BODY699_JCOEF(4)       -0.000931564786        -0.000932738706
+BODY601_GM             2.538987472063466      2.530120927277264
+BODY602_GM             7.209467692177664      7.210665451438561
+BODY603_GM             41.20833951087783      41.20659404333172
+BODY604_GM             73.11259945289306      73.11260446242133
+BODY605_GM             154.0294413273712      154.0186476847478
+BODY606_GM             8978.160024110673      8978.179855914042
+BODY607_GM             0.379051300989386      0.378215663233720
+BODY608_GM             120.5154106017876      120.5079215829297
+BODY609_GM             0.5532537713007321     0.5532635543008535
+
+2005 Jul 05 ( published )
+A. Tinio
+
+Applicable current Ephemeris =  050623R_SCPSE_05132_05150
+
+Restrictions/Limitations =  Use for tour analysis for period of file.
+
+Reference/Source of new values = 050613_009Sa
+
+Parameter              Superceded Value       New Value
+
+
+BODY6_GM               37940570.36454137      37940571.43290575
+BODY699_GM             37931192.6617          37931193.7263
+BODY699_POLE_RA(1)     40.581077              40.580518
+BODY699_POLE_DEC(1)    83.538043              83.537912
+BODY699_JCOEF(2)       0.016290903873         0.016290989185
+BODY699_JCOEF(4)       -0.000933053169        -0.000931564786
+BODY601_GM             2.539649757406880      2.538987472063466
+BODY602_GM             7.207150581927309      7.209467692177664
+BODY603_GM             41.20796800520257      41.20833951087783
+BODY604_GM             73.11254942698964      73.11259945289306
+BODY605_GM             154.0258089104270      154.0294413273712
+BODY606_GM             8978.156565061139      8978.160024110673
+BODY607_GM             0.379403816124753      0.379051300989386
+BODY608_GM             120.5204864031117      120.5154106017876
+BODY609_GM             0.5532476180130315     0.5532537713007321
+
+2005 Jun 09 ( published )
+D. Conner
+
+Applicable Ephemeris SPK File:
+     050606R_SCPSE_05114_05132 
+Restrictions/Limitations = Use for timespan of file.
+
+Reference/Source of new values = 050606_008Sa
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940560.63663255      37940570.36454137
+BODY699_GM             37931182.9332          37931192.6617
+BODY699_POLE_RA(1)     40.580644              40.581077
+BODY699_POLE_DEC(1)    83.538056              83.538043
+BODY699_JCOEF(2)       0.016291055854         0.016290903873
+BODY699_JCOEF(4)       -0.000931733527        -0.000933053169
+BODY601_GM             2.540653252053214      2.539649757406880
+BODY602_GM             7.205425461485284      7.207150581927309
+BODY603_GM             41.20782889316963      41.20796800520257
+BODY604_GM             73.11252681773537      73.11254942698964
+BODY605_GM             154.0324679857708      154.0258089104270
+BODY606_GM             8978.152308074805      8978.156565061139
+BODY607_GM             0.379158979334525      0.379403816124753
+BODY608_GM             120.5197925170135      120.5204864031117
+BODY609_GM             0.5532510109715066     0.5532476180130315
+
+
+2005 May 19 ( published )
+A. Tinio
+
+Applicable Ephemeris SPK File:
+   050513R_SCPSE_05097_05114
+Restrictions/Limitations = Use for timespan of file.
+
+Reference/Source of new values = 050513_007Sa
+
+Parameter               Superceded Value     New Value
+
+BODY6_GM                37940486.41643649    37940560.63663255 
+BODY699_GM              37931108.7402        37931182.9332 
+BODY699_POLE_RA(1)      40.578897            40.580644 
+BODY699_POLE_DEC(1)     83.537936            83.538056 
+BODY699_JCOEF(2)        0.016291230650       0.016291055854 
+BODY699_JCOEF(4)        -0.000931186978      -0.000931733527 
+BODY699_JCOEF(6)        0.000091862764       0.000092477088 
+BODY601_GM              2.541872652365942    2.540653252053214 
+BODY602_GM              7.203042868002126    7.205425461485284 
+BODY603_GM              41.20826146236565    41.20782889316963 
+BODY604_GM              73.11229775557260    73.11252681773537 
+BODY605_GM              154.0200209194596    154.0324679857708 
+BODY606_GM              8978.142297854909    8978.152308074805 
+BODY607_GM              0.374580947348313    0.379158979334525 
+BODY608_GM              120.5206235708291    120.5197925170135 
+BODY609_GM              0.5532316617014716   0.5532510109715066
+
+
+
+
+2005 May 05 ( published )
+D. Conner
+
+Applicable Ephemeris SPK File:
+   050506R_SCPSE_05081_05097
+Restrictions/Limitations =  Use for period of this file.
+
+Reference/Source of new values = 050502_006T5
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940491.60216828      37940486.41643649
+BODY699_GM             37931113.8322          37931108.7402
+BODY699_POLE_RA(1)     40.577216              40.578897
+BODY699_POLE_DEC(1)    83.537833              83.537936
+BODY699_JCOEF(2)       0.016291419485         0.016291230650
+BODY699_JCOEF(4)       -0.000930059692        -0.000931186978
+BODY699_JCOEF(6)       0.000092794848         0.000091862764
+BODY601_GM             2.541204859609778      2.541872652365942
+BODY602_GM             7.208563270001138      7.203042868002126
+BODY603_GM             41.20878136449268      41.20826146236565
+BODY604_GM             73.11206772081295      73.11229775557260
+BODY605_GM             154.1075398995426      154.0200209194596
+BODY606_GM             8978.138361913190      8978.142297854909
+BODY607_GM             0.372850585561523      0.374580947348313
+BODY608_GM             120.5278582301508      120.5206235708291
+BODY609_GM             0.5526937087918932     0.5532316617014716
+
+
+
+2005 Apr 29 ( published )
+D. Conner
+
+Applicable Ephemeris SPK File:
+   050426AP_SCPSE_05116_05216
+Restrictions/Limitations =  Use for period of this file.
+
+Reference/Source of new values = 050425_007Sa
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940502.18556380      37940491.60216828
+BODY699_GM             37931124.7142          37931113.8322
+BODY699_POLE_RA(1)     40.576012              40.577216
+BODY699_POLE_DEC(1)    83.537850              83.537833
+BODY699_JCOEF(2)       0.016291065583         0.016291419485
+BODY699_JCOEF(4)       -0.000932322006        -0.000930059692
+BODY699_JCOEF(6)       0.000091137816         0.000092794848
+BODY601_GM             2.540934363643657      2.541204859609778
+BODY602_GM             7.205763658107196      7.208563270001138
+BODY603_GM             41.20992788910005      41.20878136449268
+BODY604_GM             73.11190061154372      73.11206772081295
+BODY605_GM             153.8210020695582      154.1075398995426
+BODY606_GM             8978.126641404288      8978.138361913190
+BODY607_GM             0.379166152072442      0.372850585561523
+BODY608_GM             120.5233558989635      120.5278582301508
+BODY609_GM             0.5526908562645090     0.5526937087918932
+
+
+2005 Apr 21 ( published )
+D. Conner
+
+Applicable Ephemeris SPK File:
+   050414R_SCPSE_05034_05060  (s/c=-82, planets, satellites)
+
+Restrictions/Limitations =  Use for tour analysis for period of this file.
+
+Reference/Source of new values = 050312_004E1
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940496.33673127      37940502.18556380
+BODY699_GM             37931118.8405          37931124.7142
+BODY699_POLE_RA(1)     40.576463              40.576012
+BODY699_POLE_DEC(1)    83.537851              83.537850
+BODY699_JCOEF(2)       0.016290828142         0.016291065583
+BODY699_JCOEF(4)       -0.000933491306        -0.000932322006
+BODY699_JCOEF(6)       0.000090898497         0.000091137816
+BODY601_GM             2.541473321497260      2.540934363643657
+BODY602_GM             7.209619039344632      7.205763658107196
+BODY603_GM             41.21072942926893      41.20992788910005
+BODY604_GM             73.11206095252155      73.11190061154372
+BODY605_GM             153.8604802758120      153.8210020695582
+BODY606_GM             8978.112734019802      8978.126641404288
+BODY607_GM             0.379253012301593      0.379166152072442
+BODY608_GM             120.5170740119231      120.5233558989635
+BODY609_GM             0.5528058513249935     0.5526908562645090
+
+
+
+2005 Apr 12 ( published )  
+D. Conner
+
+Applicable Ephemeris SPK File:
+   050411R_SCPSE_05015_05034  (s/c=-82, planets, satellites)
+
+Restrictions/Limitations =  Use for Tour analysis for period of SPK file.
+
+Reference/Source of new values = 050218_003T3
+
+5rameter              Superceded Value       New Value
+
+BODY6_GM               37940515.88181417      37940496.33673127
+BODY699_GM             37931137.6508          37931118.8405
+BODY699_POLE_RA(1)     40.575513              40.576463
+BODY699_POLE_DEC(1)    83.537853              83.537851
+BODY699_JCOEF(2)       0.016290958191         0.016290828142
+BODY699_JCOEF(4)       -0.000932286762        -0.000933491306
+BODY601_GM             2.543473865943931      2.541473321497260
+BODY602_GM             7.689375056656368      7.209619039344632
+BODY603_GM             41.21109406519917      41.21072942926893
+BODY604_GM             73.11102520071464      73.11206095252155
+BODY605_GM             154.0395402008101      153.8604802758120
+BODY606_GM             8978.169116863904      8978.112734019802
+BODY607_GM             0.372672948245801      0.379253012301593
+BODY608_GM             120.5420141732170      120.5170740119231
+BODY609_GM             0.5526971060144958     0.5528058513249935
+
+
+
+2005 Mar 01 ( published )
+A. Tinio
+
+Applicable Ephemeris SPK File:
+   050214R_SCPSE_04336_05015  (s/c=-82, planets, satellites) 
+
+Restrictions/Limitations = Use only for timespan of current Ephemeris
+
+Reference/Source of new values = 050214_00cTc
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940575.96714743      37940515.88181417 
+BODY699_GM             37931197.4166          37931137.6508 
+BODY699_POLE_RA(1)     40.584988              40.575513 
+BODY699_POLE_DEC(1)    83.537357              83.537853 
+BODY699_JCOEF(2)       0.016291386368         0.016290958191 
+BODY699_JCOEF(4)       -0.000930863753        -0.000932286762 
+BODY699_JCOEF(6)       0.000089007261         0.000090898497 
+BODY601_GM             2.543221623761831      2.543473865943931 
+BODY602_GM             7.680749472948529      7.689375056656368 
+BODY603_GM             41.20953772443173      41.21109406519917 
+BODY604_GM             73.11013294006862      73.11102520071464 
+BODY605_GM             154.0976429614129      154.0395402008101 
+BODY606_GM             8978.252049389006      8978.169116863904 
+BODY607_GM             0.379196699024020      0.372672948245801 
+BODY608_GM             120.7250175986224      120.5420141732170 
+BODY609_GM             0.5529492368788559     0.5526971060144958 
+
+
+2005 Feb 28 ( published )
+A. Tinio
+
+Applicable Ephemeris SPK File:
+   050105R_SCPSE_04247_04336 (s/c=-82, planets, satellites)
+
+Restrictions/Limitations = Use for Tour Analysis for period of SPK file.
+
+Reference/Source of new values = 050105_00bTb
+
+Parameter              Superceded Value       New Value
+
+BODY2_GM               324858.598826460       324858.598826460
+BODY6_GM               37940594.58466490      37940575.96714743
+BODY699_GM             37931216.9052          37931197.4166
+BODY699_POLE_RA(1)     40.585770              40.584988
+BODY699_POLE_DEC(1)    83.537290              83.537357
+BODY699_JCOEF(2)       0.016290382080         0.016291386368
+BODY699_JCOEF(4)       -0.000934342762        -0.000930863753
+BODY601_GM             2.543886999046834      2.543221623761831
+BODY602_GM             7.896235619817622      7.680749472948529
+BODY603_GM             41.21020363352076      41.20953772443173
+BODY604_GM             73.10970856734933      73.11013294006862
+BODY605_GM             153.4403813617471      154.0976429614129
+BODY606_GM             8978.060680624023      8978.252049389006
+BODY607_GM             0.521670363874684      0.379196699024020
+BODY608_GM             120.3437832637150      120.7250175986224
+BODY609_GM*            120.7250175986224      0.5529492368788559
+
+*BODY609_GM value was inadvertently updated with the value for
+ BODY608_GM in the "2005 Jan 10" pck file.  This delivery
+ corrects this error. The new value for BODY609_GM is the previous
+ correct value which appears in the "2004 Dec 9" pck file. 
+ BODY608_GM is also correctly updated in this delivery. 
+
+2005 Jan 10 ( published )
+D. Conner
+
+Applicable Ephemeris SPK File:
+   050105R_SCPSE_04247_04336 (s/c=-82, planets, satellites)
+
+Restrictions/Limitations = Use for Tour Analysis for period of SPK file.
+
+Reference/Source of new values = 050105_00bTb
+
+Parameter              Superceded Value       New Value
+
+BODY2_GM               324858.598826460       324858.598826460
+BODY6_GM               37940594.58466490      37940575.96714743
+BODY699_GM             37931216.9052          37931197.4166
+BODY699_POLE_RA(1)     40.585770              40.584988
+BODY699_POLE_DEC(1)    83.537290              83.537357
+BODY699_JCOEF(2)       0.016290382080         0.016291386368
+BODY699_JCOEF(4)       -0.000934342762        -0.000930863753
+BODY601_GM             2.543886999046834      2.543221623761831
+BODY602_GM             7.896235619817622      7.680749472948529
+BODY603_GM             41.21020363352076      41.20953772443173
+BODY604_GM             73.10970856734933      73.11013294006862
+BODY605_GM             153.4403813617471      154.0976429614129
+BODY606_GM             8978.060680624023      8978.252049389006
+BODY607_GM             0.521670363874684      0.379196699024020
+BODY608_GM             120.3437832637150      120.7250175986224
+
+
+2004 Dec 9 ( published )
+D. Conner
+
+This file was created from cpck29Sep2004.tpc.
+Removed keywords controlled by PSG, including
+Jupiter satellites, to a separate file
+which is concatenated to this file.  Only NAVT affected keywords
+appear above.  
+
+Minor satellites and rocks keywords have been moved to the rocks
+PCK in a separate file cpck_rock.... 
+
+BODY799_GM keyword removed.  NAVT only provides a System GM.
+
+Applicable current Ephemeris = 041210AP_SCPSE_04329_08189
+Restrictions/Limitations = None
+Reference/Source of new values = 041207_00cTc (OD Solution)
+
+Parameter              Superceded Value       New Value
+
+BODY10_GM              132712440035.0199      132712440017.9870
+BODY2_GM               324858.592000000       324858.598826460
+BODY3_GM               403503.241738000       403503.233479087
+BODY399_GM             398600.4415000001      398600.4328969392
+BODY5_GM               126712765.4543717      126712767.8577960
+BODY599_GM             126686534.5576417      126686536.9610660
+BODY6_GM               37940630.56986377      37940594.58466490
+BODY699_GM             37931248.2650          37931216.9052
+BODY699_POLE_RA(1)     40.578921              40.585770
+BODY699_POLE_DEC(1)    83.537507              83.537290
+BODY699_JCOEF(2)       0.016292234642         0.016290382080
+BODY699_JCOEF(4)       -0.000927651602        -0.000934342762
+BODY699_JCOEF(6)       0.000096989418         0.000089007261
+BODY7_GM               5794549.007815570      5794549.007071874
+BODY301_GM             4902.800238000001      4902.800582147764
+BODY601_GM             2.520135918453203      2.543886999046834
+BODY602_GM             7.266915346837596      7.896235619817622
+BODY603_GM             41.21004576075436      41.21020363352076
+BODY604_GM             73.11466506841310      73.10970856734933
+BODY605_GM             155.8320579960241      153.4403813617471
+BODY606_GM             8977.930889955829      8978.060680624023
+BODY607_GM             0.720000000000000      0.521670363874684
+BODY608_GM             123.1583788283249      120.3437832637150
+BODY609_GM             0.5517732425959611     0.5529492368788559
+
+
+2004 Sep 29 (published)
+
+Applicable current Ephemeris:
+041001AP_SCPSE_04275_08222.XSP (s/c=-82, planets, satellites) 
+
+Restrictions/Limitations = None
+
+Reference/Source of new values = 040927_00aTa (OD solution)
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940690.7690100       37940630.56986377 
+BODY699_GM             37931300.4040          37931248.2650 
+BODY699_POLE_RA(1)     40.584666              40.578921 
+BODY699_POLE_DEC(1)    83.537319              83.537507 
+BODY699_JCOEF(2)       0.016293483929         0.016292234642 
+BODY699_JCOEF(4)       -0.000921635401        -0.000927651602 
+BODY699_JCOEF(6)       0.000088726120         0.000096989418 
+BODY601_GM             2.521560245529253      2.520135918453203 
+BODY602_GM             7.127481554948487      7.266915346837596 
+BODY603_GM             41.20541310412448      41.21004576075436 
+BODY604_GM             73.11977199413563      73.11466506841310 
+BODY605_GM             154.4787324900041      155.8320579960241 
+BODY606_GM             8977.981454369899      8977.930889955829 
+BODY608_GM             132.6589941798197      123.1583788283249 
+BODY609_GM             0.5515856703994798     0.5517732425959611
+
+2004 Jun 21 (published)
+
+Applicable current Ephemeris:
+040622AP_SCPSE_04002_09011.BSP (s/c=-82, planets, satellites)
+040622AP_SK_04122_08222.BSP (spacecraft ephemeris, scid=-82)
+040622AP_PE_04002_09011.BSP (planetary ephemeris)
+040622AP_SE_04002_09011.BSP (satellite ephemeris)
+
+Reference/Source of new values = 040615_00Sa  (OD solution)
+
+Parameter              Superceded Value       New Value
+
+BODY6_GM               37940679.45741954      37940690.76901004
+BODY699_GM             37931289.4836          37931300.4040
+BODY699_POLE_RA(1)     40.586420              40.584666
+BODY699_POLE_DEC(1)    83.537291              83.537319
+BODY699_JCOEF(2)       0.016292243237         0.016293483929
+BODY699_JCOEF(4)       -0.000928716077        -0.000921635401
+BODY699_JCOEF(6)       0.000088845313         0.000088726120
+BODY601_GM             2.539908238874431      2.521560245529253
+BODY602_GM             6.980134096218938      7.127481554948487
+BODY603_GM             41.21066708236702      41.20541310412448
+BODY604_GM             73.12382308588424      73.11977199413563
+BODY605_GM             154.6927779454911      154.4787324900041
+BODY606_GM             8978.009444641593      8977.981454369899
+BODY608_GM             132.2117925658847      132.6589941798197
+BODY609_GM             0.4852416379406062     0.5515856703994798    *
+
+* Reference for new Phoebe GM:  IOM 312.0-024-04 "Navigation Results 
+from the Phoebe flyby", J.B. Jones, 16 June 2004.
+
+
+2004 May 05 (published)
+
+BODY299_GM was set equal to the BODY2_GM.
+BODY799_GM was calculated based on the new BODY7_GM.
+
+Applicable Ephemeris Files:
+  040506AP_SCPSE_04122_08222.XSP (s/c=-82, planets, satellites)
+  040506AP_SK_04122_08222.XSP (spacecraft ephemeris, scid=-82)
+  040506AP_OPK_04122_08222.XSP (s/c & probe, scids=-82,-150)
+  040506AP_PE_94328_16357.XSP (planetary ephemeris)
+  040506AP_SE_04002_09011.XSP (satellite ephemeris)
+
+Reference/Source of new values is NAV OD Solution: 040409_00Sa
+
+Parameter              Superceded Value       New Value
+
+BODY10_GM              132712440017.9870      132712440035.0199
+BODY2_GM               324858.5988264598      324858.592000000
+BODY3_GM               403503.2334790870      403503.241738000
+BODY399_GM             398600.4328969392      398600.4415000001
+BODY5_GM               126712767.8577960      126712765.4543717
+BODY599_GM             126686536.9637693      126686534.5576417
+BODY6_GM               37940629.764           37940679.45741954
+BODY699_GM             37931267.73            37931289.4836
+BODY699_POLE_RA(1)     40.589                 40.586420
+BODY699_POLE_RA(2)     -0.036                 -0.042290
+BODY699_POLE_DEC(1)    83.537                 83.537291
+BODY699_POLE_DEC(2)    -0.004                 -0.004440
+BODY699_JCOEF(2)       0.016298               0.016292243237
+BODY699_JCOEF(4)       -0.000915              -0.000928716077
+BODY699_JCOEF(6)       0.000103               0.000088845313
+BODY699_CCOEF(3)       0.00000070             0.0000000000000
+BODY699_SCOEF(3)       -0.00000020            0.00000000
+BODY7_GM               5794549.007071874      5794549.007815570
+BODY301_GM             4902.800582147764      4902.800238000001
+BODY601_GM             2.5                    2.539908238874431
+BODY602_GM             4.9                    6.980134096218938
+BODY603_GM             41.808                 41.21066708236702
+BODY604_GM             73.156                 73.12382308588424
+BODY605_GM             154.000                154.6927779454911
+BODY606_GM             8978.2                 8978.009444641593
+BODY607_GM             0.99                   0.720000000000000
+BODY608_GM             106.0                  132.2117925658847
+BODY609_GM             0.48                   0.4852416379406062
+
+
+  
+--------                                                                                                                 REFERENCES
+
+   1.   Cassini NAV OD solution 040615_00Sa.
+   2.   Cassini NAV OD solution 040927_00aTa.
+   3.   Cassini NAV OD solution 041207_00cTc.
+   4.   Cassini NAV OD solution 050105_00bTb.
+   5.   Cassini Nav OD solution 050214_00cTc.
+   6.   Cassini Nav OD solution 050218_003T3.
+   7.   Cassini Nav OD solution 050312_004E1.
+   8.   Cassini Nav OD solution 050425_007Sa.
+   9.   Cassini Nav OD solution 050502_006T5.
+  10.   Cassini Nav OD solution 050513_007Sa.
+  11.   Cassini Nav OD solution 050606_008Sa.
+  12.   Cassini Nav OD solution 050613_009Sa.
+  13.   Cassini Nav OD solution 050707_010Sa.
+  14.   Cassini Nav OD solution 050718_011E2.
+  15.   Cassini Nav OD solution 050802_012Sa.
+  16.   Cassini Nav OD solution 050824_013T6.
+  17.   Cassini Nav OD solution 050911_014T7.
+  18.   Cassini Nav OD solution 050927_015H1.
+  19.   Cassini Nav OD solution 051012_016D1.
+  20.   Cassini Nav OD solution 051031_017T8.
+  21.   Cassini Nav OD solution 051128_018R1.
+  22.   Cassini Nav OD solution 051230_019T9.
+  23.   Cassini NAV OD solution 060121_020T10.
+  24.   Cassini NAV OD solution 060301_022T12.
+  25.   Cassini NAV OD solution 060301_021T11.
+  26.   Cassini NAV OD solution 060320_022T12.
+  27.   Cassini NAV OD solution 060503_023T13.
+  28.   Cassini NAV OD solution 060521_024T14.
+  29.   Cassini NAV OD solution 060705a_025T15.
+  30.   Cassini NAV OD solution 060723_026T16.
+  31.   Cassini NAV OD solution 060815_027Sa.
+  32.   Cassini NAV OD solution 060910_028T17.
+  33.   Cassini NAV OD solution 060926_029T18.
+  34.   Cassini NAV OD solution 061013_030T19.
+  35.   Cassini NAV OD solution 061029_031T20. 
+  36.   Cassini NAV OD solution 061114_032Sa.
+  37.   Cassini NAV OD solution 061127a_033Sa.
+  38.   Cassini NAV OD solution 061211_034Sa.
+  39.   Cassini NAV OD solution 061214_035T21.
+  40.   Cassini NAV OD solution 061231a_036T22.
+  41.   Cassini NAV OD solution 061122_034Sa.
+  42.   Cassini NAV OD solution 070131_038T24.
+  43.   Cassini NAV OD solution 070227_039T25.
+  44.   Cassini NAV OD solution 070311_040T26.
+  45.   Cassini NAV OD solution 070328_041T27.
+  46.   Cassini NAV OD solution 070412_042T28.
+  47.   Cassini NAV OD solution 070429_043T29.
+  48.   Cassini NAV OD solution 070516_044T30.
+  49.   Cassini NAV OD solution 070531_045T31.
+  50.   Cassini NAV OD solution 070616_046T32. 
+  51.   Cassini NAV OD solution  070703_047T33.
+  52.   Cassini NAV OD solution  070722_048T34.
+  53.   Cassini NAV OD solution 070902_049T35.
+
+  54.   Cassini NAV OD solution 071004_050T36.
+  55.   Cassini NAV OD solution 071121_051T37.
+  56.   Cassini NAV OD solution 071208_053T38.
+  57.   Cassini NAV OD solution 080108_055T40.
+  58.   Cassini NAV OD solution 080229_056T41.
+  59.   Cassini NAV OD solution 080313_060E3.
+  60.   Cassini NAV OD solution 080331_062T42.
+  61.   Cassini NAV OD solution 080516_063T43.
+  62.   Cassini NAV OD solution 080602_068T44.
+  63.   Cassini NAV OD solution 080803_070Sa.
+  64.   Cassini NAV OD solution 080816_079E4.
+  65.   Cassini NAV OD solution 081011_081E5.
+  66.   Cassini NAV OD solution 081106_089T46.
+  67.   Cassini NAV OD solution 081122_091T47.
+  68.   Cassini NAV OD solution 081208_094T48.
+  69.   Cassini NAV OD solution 081228_096T49.
+  70.   Cassini NAV OD solution 090209_098T50.
+  71.   Cassini NAV OD solution 090328_103T51.
+  72.   Cassini NAV OD solution 090407_107T52.
+  73.   Cassini NAV OD solution 090422_109T53.
+  74.   Cassini NAV OD solution 090507_110T54.
+  75.   Cassini NAV OD solution 090526_111T55.
+  76.   Cassini NAV OD solution 090609_112T56.
+  77.   Cassini NAV OD solution 090626_113T57.
+  78.   Cassini NAV OD solution 090710_114T58.
+  79.   Cassini NAV OD solution 090727_115T59.
+  80.   Cassini NAV OD solution 090810_116T60.
+  81.   Cassini NAV OD solution 090828_117T61.
+  82.   Cassini NAV OD solution 090903_118T62.
+  83.   Cassini NAV OD solution 091016_118T62.
+  84.   Cassini NAV OD solution 091105_120E7.
+  85.   Cassini NAV OD solution 091122_121E8.
+  86.   Cassini NAV OD solution 091214_122T63.
+  87.   Cassini NAV OD solution 100103_123T64.
+  88.   Cassini NAV OD solution 100131_125T66.
+  89.   Cassini NAV OD solution 100306_126R2.
+  90.   Cassini NAV OD solution 100409_128T67.
+  91.   Cassini NAV OD solution 100523_131T68.
+  92.   Cassini NAV OD solution 100608_132T69.
+  93.   Cassini NAV OD solution 100623_133T70.
+  94.   Cassini NAV OD solution 100709_134T71.
+  95.   Cassini NAV OD solution 100816_135E11.
+  96.   Cassini NAV OD solution 100927_137T72.
+  97.   Cassini NAV OD solution 101201_141E12.
+  98.   Cassini NAV OD solution 101223_142E13.
+  99.   Cassini NAV OD solution 110113_143R3.
+  100.   Cassini NAV OD solution 110511_148T76.
+  101.   Cassini NAV OD solution 110623_149T77.
+  102.   Cassini NAV OD solution 110915_150T78.
+  103.   Cassini NAV OD solution 111003_154E14.
+  104.   Cassini NAV OD solution 111216_157T79.
+  105.   Cassini NAV OD solution 120105_159T80.
+  106.   Cassini NAV OD solution 120203_160T81.
+  107.   Cassini NAV OD solution 120329_162E17.
+  108.   Cassini NAV OD solution 120416_164E18.
+  109.   Cassini NAV OD solution 120502_1_165E19.
+  110.   Cassini NAV OD solution 120523_166T83.
+  111.   Cassini NAV OD solution 120723_168T85.
+  112.   Cassini NAV OD solution 120926_170T86.
+  113.   Cassini NAV OD solution 121112_173T87.
+  114.   Cassini NAV OD solution 121201_175T88.
+  115.   Cassini NAV OD solution 121201_1_175T88.
+  116.   Cassini NAV OD solution 130216_176T89.
+  117.   Cassini NAV OD solution 130313_182R4.
+  118.   Cassini NAV OD solution 130408_184T90.
+  119.   Cassini NAV OD solution 130523_186T91.
+  120.   Cassini NAV OD solution 130713_191T92.
+  121.   Cassini NAV OD solution 130728_195T93.
+  122.   Cassini NAV OD solution 130911_1_196T94.
+  123.   Cassini NAV OD solution 131015_198T95.
+  124.   Cassini NAV OD solution 131203_199T96.
+  125.   Cassini NAV OD solution 140406_1_203T100.
+  126.   Cassini NAV OD solution 140520_204T101.
+  127.   Cassini NAV OD solution 140621_205T102.
+  128.   Cassini NAV OD solution 140820_207T104.
+  129.   Cassini NAV OD solution 140923_1_208T105.
+  130.   Cassini NAV OD solution 141023_1_209T106.
+  131.   Cassini NAV OD solution 141210_210T107.
+  132.   Cassini NAV OD solution 150214_212T109.
+  133.   Cassini NAV OD solution 150318_213T110.
+  134.   Cassini NAV OD solution 150507_214T111.
+  135.   Cassini NAV OD solution 150618_216D4.
+  136.   Cassini NAV OD solution 150709_218T112.
+  137.   Cassini NAV OD solution 150819_219D5.
+  138.   Cassini NAV OD solution 151001_221T113.
+  139.   Cassini NAV OD solution 151018_223E20.
+  140.   Cassini NAV OD solution 151030_224E21.
+  141.   Cassini NAV OD solution 151115_225T114.
+  142.   Cassini NAV OD solution 151222_226E22.
+  143.   Cassini NAV OD solution 160118_229T115.
+  144.   Cassini NAV OD solution 160203_231T116.
+  145.   Cassini NAV OD solution 160218_232T117.
+  146.   Cassini NAV OD solution 160405_233T118.
+  147.   Cassini NAV OD solution 160504_235T119.
+  148.   Cassini NAV OD solution 160606_236T120.
+  149.   Cassini NAV OD solution 160724_237T121.
+  150.   Cassini NAV OD solution 160810_1_239T122.
+  151.   Cassini NAV OD solution 160926_240T123.
+  152.   Cassini NAV OD solution 161019_244T124.
+  153.   Cassini NAV OD solution 161116_246T124.
+  154.   Cassini NAV OD solution 161202_1_249T125.
+  155.   Cassini NAV OD solution 170105_251T126.
+  156.   Cassini NAV OD solution 170423_254T126.
+  157.   Cassini NAV OD solution 170421_264T126.
+  158.   Cassini NAV OD solution 170507_269GF.
+  159.   Cassini NAV OD solution 170608_271GF.
+  160.   Cassini NAV OD solution 170714_276GF.
+  161.   Cassini NAV OD solution 170813_281GF.
+  162.   Cassini NAV OD solution 170915_1_288GF.
+ 
+KPL/PCK
+
+\begindata
+   CASSINI_PCK_VERSION     = ( '2010-SEP-02' )
+\begintext
+
+
+P_constants (PcK) SPICE kernel file
+
+Refer to the notes at the bottom of the file for help, contacts, 
+version history, references, and Cassini-specific parameter descriptions. 
+All radii and orientation values are from reference [1] unless 
+otherwise noted.
+
+This file was created by separating science controlled values from NAVT
+controlled values for ease of file maintenance.  References to GMs provided
+by the NAVT, Saturn Pole RA and DEC, and JCOEFF and SCOEFF have been removed.
+
+-------- SUN
+
+         Value for the Sun radii is from [2], page K7. 
+
+         \begindata 
+         BODY10_RADII           = (   696000.     696000.      696000.     )
+         BODY10_POLE_RA         = (  286.13       0.          0. )
+         BODY10_POLE_DEC        = (   63.87       0.          0. )
+         BODY10_PM              = (   84.10     +14.18440     0. )
+         BODY10_LONG_AXIS       = (    0.                        )
+         \begintext
+
+
+-------- VENUS
+
+         \begindata
+
+         BODY299_RADII            = (  6051.8       6051.8      6051.8 ) 
+         BODY299_POLE_RA          = (  272.76       0.          0. )
+         BODY299_POLE_DEC         = (  +67.16       0.          0. )
+         BODY299_PM               = (  160.20      -1.4813688   0. )
+         BODY299_LONG_AXIS        = (    0.                        )
+         \begintext
+
+
+-------- EARTH
+
+
+         Northern hemisphere projection of the Earth's magnetic dipole: 
+           coordinates are planetocentric, values are from [3].
+         
+         \begindata
+         BODY399_RADII     = (     6378.140    6378.140     6356.75   )
+         BODY399_POLE_RA        = (    0.      -0.641         0. )
+         BODY399_POLE_DEC       = (  +90.      -0.557         0. )
+         BODY399_PM             = (  190.147  +360.9856235     0. )
+         BODY399_LONG_AXIS      = (    0.                        )
+         BODY3_NUT_PREC_ANGLES  = ( 125.045         -1935.5364525000
+                                    250.089         -3871.0729050000
+                                    260.008        475263.3328725000
+                                    176.625        487269.6299850000
+                                    357.529         35999.0509575000
+                                    311.589        964468.4993100001
+                                    134.963        477198.8693250000
+                                    276.617         12006.3007650000
+                                     34.226         63863.5132425000
+                                     15.134         -5806.6093575000
+                                    119.743           131.8406400000
+                                    239.961          6003.1503825000
+                                     25.053        473327.7964200000 )
+         BODY399_MAG_NORTH_POLE_LON  =  ( -69.761 )
+         BODY399_MAG_NORTH_POLE_LAT  =  (  78.565 )
+         \begintext
+
+
+-------- JUPITER
+
+            
+         \begindata
+         BODY599_RADII     = (    71492.      71492.       66854.     )
+         BODY599_POLE_RA        = (   268.05    -0.009      0.  )
+         BODY599_POLE_DEC       = (   +64.49    +0.003      0.  )
+         BODY599_PM             = (   284.95  +870.5366420  0.  )
+         BODY599_LONG_AXIS      = (     0.                      )
+         BODY5_NUT_PREC_ANGLES  = (   73.32   91472.9
+                                      24.62   45137.2
+                                     283.90    4850.7
+                                     355.80    1191.3
+                                     119.90     262.1
+                                     229.80      64.3
+                                     352.35    2382.6
+                                     113.35    6070.0   
+                                     146.64  182945.8
+                                      49.24   90274.4  )
+
+         \begintext
+
+
+-------- SATURN
+
+         The first seven angles given in NUT_PREC are the angles S1 
+         through S7 from the 2000 IAU report; the eighth and ninth 
+         angles are 2*S1 and 2*S2, respectively.
+         
+         Ring models are from [4], [19], [20].  They are also documented in
+         [11] and [12]. 
+         F Ring Data are from [8]. 
+         MIMI zone reflects the old flight rule 
+         for MIMI INCA, +/- 30000 km thickness inside of 8.74 Rs.
+
+         BODY699_RADII_OPTICAL is for PDT to determine at what altitude 
+         that Saturn first starts to cast a discernible shadow.
+
+         BODY699_RADII_RS  models Saturn as a sphere and corresponds to a 100 
+         mbar surface. BODY699_RADII and BODY699_RADII_1BAR  correspond to a 
+         1 bar surface.  BODY699_RADII contains IAU values. BODY699_RADII_1BAR
+         currently contains IAU values but will likely be updated during the
+         mission. It is generally agreed that 60330.0 is the Saturn reference radius.  
+         This value in stored later in the file under the keyword RS.
+
+         Eventually three different magnetospheric models will be provided. This 
+         section currently serves as a placeholder.
+
+         BODY699_MAG_NORTH_POLE_LON = (   0.0 )
+         BODY699_MAG_NORTH_POLE_LAT = ( +90.0 )
+         BODY699_M1COEF          = ( 0.0   0.0   0.0  0.0)
+         BODY699_G1COEF          = ( 0.0   0.0   0.0  0.0)
+         BODY699_H1COEF          = ( 0.0   0.0   0.0  0.0)
+         BODY699_M2COEF          = ( 0.0   0.0   0.0  0.0)
+         BODY699_G2COEF          = ( 0.0   0.0   0.0  0.0)
+         BODY699_H2COEF          = ( 0.0   0.0   0.0  0.0)
+         BODY699_M3COEF          = ( 0.0   0.0   0.0  0.0)
+         BODY699_G3COEF          = ( 0.0   0.0   0.0  0.0)
+         BODY699_H3COEF          = ( 0.0   0.0   0.0  0.0)
+
+
+         \begindata
+         BODY699_RADII     = (     60268.      60268.       54364.     )
+         BODY699_RADII_1BAR = (    60268.      60268.       54364.     )
+         BODY699_RADII_OPTICAL = ( 60430.      60430.       54508.     )
+         BODY699_RADII_RS = (      60330.      60330.       60330.     )
+         BODY699_PM             = (  38.90   +810.7939024  0.  )
+         BODY699_LONG_AXIS      = (     0.                       )
+         BODY6_NUT_PREC_ANGLES  = (  353.32   75706.7
+                                      28.72   75706.7
+                                     177.40  -36505.5
+                                     300.00   -7225.9
+                                     316.45     506.2
+                                     345.20   -1016.3
+                                      29.80     -52.1
+                                     706.64  151413.4
+                                      57.44  151413.4  )
+         BODY699_RING1_NAME     = 'A Ring'
+         BODY699_RING1          = (122170.0 136780.0 0.1 0.1 0.5)
+         BODY699_RING1_1_NAME   = 'Encke Gap'
+         BODY699_RING1_1        = (133405.0 133730.0 0.0 0.0 0.0)
+         BODY699_RING2_NAME     = 'Cassini Division'
+         BODY699_RING2          = (117580.0 122170.0 0.0 0.0 0.0)
+         BODY699_RING3_NAME     = 'B Ring'
+         BODY699_RING3          = (92000.0 117580.0 0.1 0.1 1.5)
+         BODY699_RING4_NAME     = 'C Ring'
+         BODY699_RING4          = (74510.0 92000.0 0.1 0.1 0.1)
+         BODY699_RING5_NAME     = 'D Ring'
+         BODY699_RING5          = (66970.0 74510.0 0.1 0.1 0.00001)
+         BODY699_RING6_NAME     = 'E ring'
+         BODY699_RING6_A        = (189870.0 256900.0 9000.0 9000.0 0.000003)
+         BODY699_RING6_B        = (256900.0 420000.0 9000.0 17000.0 0.000003)
+         BODY699_RING7_NAME     = 'F Ring'
+         BODY699_RING7          = (140180.0 140270.0 6.5 6.5 0.1)
+         BODY699_RING7_FCENTER  = (140223.7, 0.00254, 24.1, 2.7001, 0.0065, 16.1, -2.6876)
+         BODY699_RING8_NAME     = 'G Ring'
+         BODY699_RING8          = (165000.0 176000.0 280.0 280.0 0.000001)
+         BODY699_MIMI_DUST_ZONE = ( 0.0 527284.2 60000.0 60000.0 )
+         \begintext
+
+
+-------- URANUS
+
+
+         \begindata
+         BODY799_RADII     = (    25559.      25559.       24973.     )
+         BODY799_POLE_RA        = (  257.311     0.         0.  )
+         BODY799_POLE_DEC       = (  -15.175     0.         0.  )
+         BODY799_PM             = (  203.81   -501.1600928  0.  )
+         BODY799_LONG_AXIS      = (    0.                       )
+         \begintext
+
+
+-------- MOON
+
+
+         \begindata
+         BODY301_RADII     = (     1737.4      1737.4       1737.4    )
+         BODY301_POLE_RA      = (  269.9949    0.0031        0.        )
+         BODY301_POLE_DEC     = (   66.5392    0.0130        0.        )
+         BODY301_PM           = (   38.3213   13.17635815   -1.4D-12   )
+         BODY301_LONG_AXIS    = (    0.                                )
+         BODY301_NUT_PREC_RA  = (  -3.8787   -0.1204  +0.0700  -0.0172
+                                    0.       +0.0072   0.       0.
+                                    0.       -0.0052   0.       0.
+                                   +0.0043                             )
+         BODY301_NUT_PREC_DEC = (   1.5419   0.0239   -0.0278  +0.0068
+                                    0.      -0.0029   +0.0009   0.
+                                    0.      +0.0008    0.       0.
+                                   -0.0009                             )
+         BODY301_NUT_PREC_PM  = (  3.5610   +0.1208   -0.0642  +0.0158
+                                  +0.0252   -0.0066   -0.0047  -0.0046
+                                  +0.0028   +0.0052   +0.0040  +0.0019
+                                  -0.0044                              )
+         \begintext
+
+
+Satellites of Jupiter
+-------------------------------------------------------
+
+-------- IO
+
+
+         BODY501_GM value from [5].
+
+         \begindata
+         BODY501_GM          =  (              5959.916     )
+         BODY501_RADII     = (     1829.4      1819.3       1815.7    )
+         BODY501_POLE_RA       = (  268.05          -0.009      0.  )
+         BODY501_POLE_DEC      = (  +64.50          +0.003      0.  )
+         BODY501_PM            = (  200.39        +203.4889538  0.  )
+         BODY501_LONG_AXIS     = (    0.                            )
+         BODY501_NUT_PREC_RA   = (    0.   0.    +0.094   +0.024   )
+         BODY501_NUT_PREC_DEC  = (    0.   0.    +0.040   +0.011   )
+         BODY501_NUT_PREC_PM   = (    0.   0.    -0.085   -0.022   )
+         \begintext
+
+
+-------- EUROPA
+
+
+         BODY502_GM value from [5].
+         
+         \begindata
+         BODY502_GM          =  (              3202.739       )
+         BODY502_RADII     = (     1564.13     1561.23      1560.93   )
+         BODY502_POLE_RA       = (  268.08          -0.009      0.   )
+         BODY502_POLE_DEC      = (  +64.51          +0.003      0.   )
+         BODY502_PM            = (   36.022         +101.3747235  0. )
+         BODY502_LONG_AXIS     = (    0.                             )
+         BODY502_NUT_PREC_RA   = ( 0. 0. 0. +1.086  +0.060  +0.015  +0.009 )
+         BODY502_NUT_PREC_DEC  = ( 0. 0. 0. +0.468  +0.026  +0.007  +0.002 )
+         BODY502_NUT_PREC_PM   = ( 0. 0. 0. -0.980  -0.054  -0.014  -0.008 )
+         \begintext
+
+
+-------- GANYMEDE
+
+
+         BODY503_GM value from [5].
+
+
+         \begindata
+         BODY503_GM          =  (              9887.834     )
+         BODY503_RADII     = (     2632.4      2632.29      2632.35   ) 
+         BODY503_POLE_RA       = (  268.20          -0.009      0.   )
+         BODY503_POLE_DEC      = (  +64.57          +0.003      0.   )
+         BODY503_PM            = (   44.064         +50.3176081  0.   )
+         BODY503_LONG_AXIS     = (    0.                             )
+         BODY503_NUT_PREC_RA   = ( 0. 0. 0.  -0.037  +0.431  +0.091   )
+         BODY503_NUT_PREC_DEC  = ( 0. 0. 0.  -0.016  +0.186  +0.039   )
+         BODY503_NUT_PREC_PM   = ( 0. 0. 0.  +0.033  -0.389  -0.082   )
+         \begintext
+
+
+-------- CALLISTO
+
+
+         BODY504_GM value from [5].
+         
+         \begindata
+         BODY504_GM          =  (              7179.289     )
+         BODY504_RADII     = (     2409.4      2409.2       2409.3    )
+         BODY504_POLE_RA       = (   268.72   -0.009      0.  )
+         BODY504_POLE_DEC      = (   +64.83   +0.003      0.  )
+         BODY504_PM            = (   259.51  +21.5710715  0.  )
+         BODY504_LONG_AXIS     = (     0.                     )
+         BODY504_NUT_PREC_RA   = ( 0. 0. 0. 0. -0.068 +0.590  0. +0.010 )
+         BODY504_NUT_PREC_DEC  = ( 0. 0. 0. 0. -0.029 +0.254  0. -0.004 )
+         BODY504_NUT_PREC_PM   = ( 0. 0. 0. 0. +0.061 -0.533  0. -0.009 )
+         \begintext
+
+
+-------- HIMALIA
+
+
+         BODY506_GM values from [21].
+         
+         \begindata
+         BODY506_GM       = (          0.45         )
+         BODY506_RADII    = (  85      85      85   )
+         BODY506_POLE_RA       = (   268.72   -0.009      0.  )
+         BODY506_POLE_DEC      = (   +64.83   +0.003      0.  )
+         BODY506_PM            = (   259.51  +21.5710715  0.  )
+         BODY506_LONG_AXIS     = (     0.                     )
+         \begintext
+
+
+Satellites of Saturn
+-----------------------------------------------------------
+
+-------- MIMAS
+
+
+         BODY601_RADII values from [22].
+         BODY601_PM values from [24].        
+ 
+         \begindata
+         BODY601_RADII         = (    207.4     196.8    190.6    ) 
+         BODY601_POLE_RA       = (    40.66    -0.036      0.  )
+         BODY601_POLE_DEC      = (   +83.52    -0.004      0.  )
+         BODY601_PM            = (   333.46  +381.9945550  0.  )
+         BODY601_LONG_AXIS     = (     0.                      )
+         BODY601_NUT_PREC_RA   = ( 0. 0. +13.56  0.    0.   0. 0. 0. 0. )
+         BODY601_NUT_PREC_DEC  = ( 0. 0.  -1.53  0.    0.   0. 0. 0. 0. )
+         BODY601_NUT_PREC_PM   = ( 0. 0. -13.48  0. -44.85  0. 0. 0. 0. )
+         \begintext
+
+
+-------- ENCELADUS
+
+
+         BODY602_RADII values from [22].
+         BODY602_PM values from [24].        
+
+         \begindata
+         BODY602_RADII     = (      256.6       251.4        248.3    )
+         BODY602_POLE_RA       = (   40.66    -0.036      0.  )
+         BODY602_POLE_DEC      = (  +83.52    -0.004      0.  )
+         BODY602_PM            = (    6.32  +262.7318996  0.  )
+         BODY602_LONG_AXIS     = (    0.                      )
+         \begintext
+
+
+-------- TETHYS
+
+         BODY603_RADII values from [22].
+         BODY603_PM values from [24].        
+
+         \begindata
+         BODY603_RADII     = (      540.4       531.1        527.5    )
+         BODY603_POLE_RA       = (    40.66    -0.036      0.  )
+         BODY603_POLE_DEC      = (   +83.52    -0.004      0.  )
+         BODY603_PM            = (     8.95  +190.6979085  0.  )
+         BODY603_LONG_AXIS     = (     0.                      )
+         BODY603_NUT_PREC_RA   = ( 0. 0. 0.  +9.66   0.    0.  0.  0.  0. )
+         BODY603_NUT_PREC_DEC  = ( 0. 0. 0.  -1.09   0.    0.  0.  0.  0. )
+         BODY603_NUT_PREC_PM   = ( 0. 0. 0.  -9.60  +2.23  0.  0.  0.  0. )
+         \begintext
+
+
+-------- DIONE
+
+         BODY604_RADII values from [22].
+         BODY604_PM values from [24].        
+
+         \begindata
+         BODY604_RADII     = (      563.8        561.0         560.3     )
+         BODY604_POLE_RA       = (    40.66    -0.036      0.  )
+         BODY604_POLE_DEC      = (   +83.52    -0.004      0.  )
+         BODY604_PM            = (   357.60  +131.5349316  0.  )
+         BODY604_LONG_AXIS     = (     0.                      )
+         \begintext
+
+
+-------- RHEA
+
+         BODY605_RADII values from [22].
+         BODY605_PM values from [24].        
+
+         \begindata
+         BODY605_RADII     = (      767.2        762.5         763.1     )
+         BODY605_POLE_RA       = (   40.38    -0.036      0.   )
+         BODY605_POLE_DEC      = (  +83.55    -0.004      0.   )
+         BODY605_PM            = (  235.16   +79.6900478  0.   )
+         BODY605_LONG_AXIS     = (    0.                       )
+         BODY605_NUT_PREC_RA   = ( 0. 0. 0. 0. 0.  +3.10  0. 0. 0. )
+         BODY605_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0.  -0.35  0. 0. 0. )
+         BODY605_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  -3.08  0. 0. 0. )
+         \begintext
+
+
+-------- TITAN
+
+         Titan Pole Use restriction:
+
+         The proposed new PCK Titan pole model incorporates a new pole position
+         (RA, Dec) with Titan's synchronous spin rate.  This model reduces
+         mislocation errors for RADAR passes between TA and T30 from 30km to
+         about 2.5km.  The new model contains no rate or nutation terms. 
+         Nominal values of these terms would cause changes of less than about 2km
+         in the position of surface features over the period 2000-2020.  
+
+         BODY606_POLE_RA, BODY606_POLE_DEC, BODY606_PM, BODY606_NUT_PREC_RA
+         BODY606_NUT_PREC_DEC, BODY606_NUT_PREC_PM values from [23].
+
+         \begindata
+         BODY606_RADII     = (     2575.       2575.        2575.     )
+         BODY606_POLE_RA       = (   +39.4827    0.         0.   )
+         BODY606_POLE_DEC      = (   +83.4279    0.         0.   )
+         BODY606_PM            = (   186.5855   22.5769768  0.   )
+         BODY606_LONG_AXIS     = (     0.                      )
+         BODY606_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 0.  0.  0. 0. )
+         BODY606_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 0.  0.  0. 0. )
+         BODY606_NUT_PREC_PM   = ( 0. 0. 0. 0. 0. 0.  0.  0. 0. )
+         BODY606_ATMOSPHERE = ( 175.0 10.0 
+                                0.000006350 11400.0 76.0 
+                                0.000000513 8030.0 -429.0 
+                                0.000073500 15000.0 44.0 )
+         \begintext
+
+
+-------- HYPERION
+
+
+         While Hyperion's spin state is chaotic, Voyager and ground-based
+         observations suggest some states are common (Thomas et al 1995, 
+         Icarus 117, 128-148).  The  spin pole orientation is from the
+         Voyager observations; both the spin pole orientation and spin rate
+         will probably differ during Cassini's mission. Hyperion radii and 
+         orientation from Peter Thomas @ Cornell
+
+
+         \begindata
+         BODY607_RADII     = (      164.        130.         107.    )
+         BODY607_POLE_RA = ( 226. 0 0 )
+         BODY607_POLE_DEC = ( 35. 0 0 )
+         BODY607_PM = ( 20.02 72.0 0 )
+         BODY607_LONG_AXIS     = (     0.                    )
+         \begintext
+
+
+-------- IAPETUS
+
+         BODY608_RADII values from [22].
+         BODY608_PM values from [24].        
+
+         \begindata
+         BODY608_RADII     = (      747.4        747.4         712.4     )
+         BODY608_POLE_RA       = (   318.16  -3.949      0.  )
+         BODY608_POLE_DEC      = (   +75.03  -1.143      0.  )
+         BODY608_PM            = (   355.20  +4.5379572  0.  )
+         BODY608_LONG_AXIS     = (     0.                    )
+         \begintext
+
+
+-------- PHOEBE
+
+
+         BODY609_PM from [13].
+
+
+         \begindata
+         BODY609_RADII     = (      115.        110.         105.     )
+         BODY609_POLE_RA       = (  355.00      0.         0.  )
+         BODY609_POLE_DEC      = (  +68.70      0.         0.  )
+         BODY609_PM            = (  178.58   +931.639  0.  )
+         BODY609_LONG_AXIS     = (    0.                       )
+         \begintext
+
+-------- CONSTANTS AND NOTES FOR PDT USERS
+
+
+         The astronomical unit AU, given in kilometers.
+
+         \begindata
+         AU                  =  (      149597870.7           )
+         \begintext
+         
+         
+         Saturn reference radius (Rs) is the base for measuring body 
+         distances and ring radial distances in mulitples of saturn radius.
+
+         
+         \begindata
+         RS                  = (       60330.0       )
+         \begintext
+
+
+
+         Note that GM values >= 1.0 are packaged as is into 7CONIC_VEC 
+         commands for AACS to propagate the body's ephemeris. 
+         For GM values < 1.0, the value in the G_MASS parameter 
+         of the 7CONIC_VEC command is set to 1.0.  One is the minimum 
+         value for the G_MASS parameter. The resetting of the G_MASS 
+         parameter to the minimum acceptable where the actual 
+         GM is < 1.0 is acceptable since CAS will not pass close enough 
+         to any of the affected bodies for the gravitational mass 
+         to have an effect.
+         
+-------- OBLATE SPHEROIDS VERSUS TRIAXIAL ELLIPSOIDS
+
+
+         Some Cassini software cannot model triaxial ellipsoids, where the
+         RADII are all different. Instead, they model bodies as oblate
+         spheroids, where the equatorial RADII values (the first two) must
+         be identical. In cases here where the equatorial radii are not
+         identical, the average of the two should be used when constructing
+         an oblate spheroid. The polar radius (the third RADII) can be used
+         as given in both cases.
+
+
+-------- CONSTANTS AND NOTES FOR CASPER USERS
+
+
+         \begindata
+         BODY601_GM/PRIMARY  =  (              6.59087D-08             )
+         BODY602_GM/PRIMARY  =  (              1.29181D-07             )
+         BODY603_GM/PRIMARY  =  (              1.1022D-06              )
+         BODY604_GM/PRIMARY  =  (              1.92865D-06             )
+         BODY605_GM/PRIMARY  =  (              4.05998D-06             )
+         BODY606_GM/PRIMARY  =  (              2.36697D-04             )
+         BODY607_GM/PRIMARY  =  (              2.60998D-08             )
+         BODY608_GM/PRIMARY  =  (              2.79453D-06             )
+         BODY609_GM/PRIMARY  =  (              1.26545D-08             )
+         BODY610_GM/PRIMARY  =  (              3.38507D-09             )
+         BODY611_GM/PRIMARY  =  (              9.41176D-10             )
+         BODY612_GM/PRIMARY  =  (              4.48179D-11             )
+         BODY613_GM/PRIMARY  =  (              1.26545D-11            )
+         BODY614_GM/PRIMARY  =  (              6.32723D-12            )
+         BODY615_GM/PRIMARY  =  (              1.89817D-11             )
+         BODY616_GM/PRIMARY  =  (              5.79996D-10             )
+         BODY617_GM/PRIMARY  =  (              3.42725D-10             )
+         BODY618_GM/PRIMARY  =  (              4.74543D-12             )
+         \begintext
+         
+-------- URLS AND CONTACTS
+
+
+Description of PCK format and contents can be found in NAIF's PCK "required
+reading" document, at:
+
+ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/ascii/individual_docs/pck.req
+
+
+NAIF tutorial on PCK formatting and use at:
+
+ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/Tutorials/office/individual_docs/16_pck.ppt
+ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/Tutorials/office/packages/
+SPICE_Tutorials_Office.zip
+
+
+The Cassini PCK & ephemeris files can be found on the DOM, and at:
+
+ftp://naif.jpl.nasa.gov/pub/naif/CASSINI/kernels/
+
+
+Questions regarding this file can be directed to:
+
+Diane Conner (818)354-8586 Diane.Conner@jpl.nasa.gov
+Adrian Tinio (818)354-7511 Adrian.Tinio@jpl.nasa.gov
+David Seal   (818)354-2707 David.Seal@jpl.nasa.gov
+
+
+-------- VERSION HISTORY
+
+The noted versions were officially published; the others were
+created and circulated for internal review only.
+
+2010 Sep 02 (published)
+A. Tinio
+
+ECR-110654 Implementation
+
+Update the rotation parameter W0 to IAU 2009 values
+
+NEW VALUES:
+   BODY601_PM = (   333.46  +381.9945550  0.  ) 
+   BODY602_PM = (    6.32  +262.7318996  0.  ) 
+   BODY603_PM = (     8.95  +190.6979085  0.  ) 
+   BODY604_PM = (   357.60  +131.5349316  0.  ) 
+   BODY605_PM = (  235.16   +79.6900478  0.   ) 
+   BODY608_PM = (   355.20  +4.5379572  0.  ) 
+
+OLD VALUES:
+   BODY601_PM = (   337.46  +381.9945550  0.  ) 
+   BODY602_PM = (    2.82  +262.7318996  0.  )
+   BODY603_PM = (    10.45  +190.6979085  0.  )
+   BODY604_PM = (   357.00  +131.5349316  0.  )
+   BODY605_PM = (  235.16   +79.6900478  0.   )
+   BODY608_PM = (   350.20  +4.5379572  0.  )
+ 
+2008 Apr 16 (published)
+A. Tinio
+
+ECR-107847 Implementation
+
+1. Update radii values for Mimas, Enceladus, Tethys, Dione, Rhea, and Iapetus. 
+
+NEW VALUES: 
+  BODY601_RADII = ( 207.4 196.8 190.6 ) MIMAS 
+  BODY602_RADII = ( 256.6 251.4 248.3 ) ENCELADUS 
+  BODY603_RADII = ( 540.4 531.1 527.5 ) TETHYS 
+  BODY604_RADII = ( 563.8 561.0 560.3 ) DIONE 
+  BODY605_RADII = ( 767.2 762.5 763.1 ) RHEA 
+  BODY608_RADII = ( 747.4 747.4 712.4 ) IAPETUS 
+
+SUPERCEDED VALUES: 
+  BODY601_RADII = ( 209.1 196.2 191.4 ) MIMAS 
+  BODY602_RADII = ( 256.3 247.3 244.6 ) ENCELADUS 
+  BODY603_RADII = ( 535.6 528.2 525.8 ) TETHYS 
+  BODY604_RADII = ( 560. 560. 560. ) DIONE 
+  BODY605_RADII = ( 764. 764. 764. ) RHEA 
+  BODY608_RADII = ( 718. 718. 718. ) IAPETUS 
+
+Radii values are from: 
+
+Porco, C.C., Thomas, P.C., Weiss, J.W., Richardson, D.C. 2007. Saturns Small Inner Satellites: Clues to Their Origins. Science 318, 1602. 
+
+Thomas, P.C., and 12 colleagues 2007. Shapes of the saturnian icy satellites and their significance. Icarus 190, 573-584. 
+
+
+2. Update Titan pole position  -  
+
+NEW VALUES: 
+ BODY606_POLE_RA = ( +39.4827 0. 0. )
+ BODY606_POLE_DEC = ( +83.4279 0. 0. )
+ BODY606_PM = ( 186.5855 22.5769768 0. )
+ BODY606_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 0.0 0. 0. )
+ BODY606_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0.0 0. 0. )
+ BODY606_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. 0.0 0. 0. )
+
+SUPERCEDED VALUES: 
+ BODY606_POLE_RA = ( 36.41 -0.036 0. )
+ BODY606_POLE_DEC = ( +83.94 -0.004 0. )
+ BODY606_PM = ( 189.64 +22.5769768 0. )
+ BODY606_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. +2.66 0. 0. )
+ BODY606_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. -0.30 0. 0. )
+ BODY606_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. -2.64 0. 0. ) 
+
+Titan PCK values from: Bryan Stiles
+
+
+2004 Dec 09 (published)
+D. Conner
+
+This file was created from file cpck14Oct2004.tpc.
+It contains keywords that will be maintained by the PSG.  NAVT maintained
+keywords have been moved in a separate file.
+
+Minor satellites and rocks keywords have been moved to the rocks
+PCK.
+ 
+
+2004 Oct 14 (published)
+
+Documentation was added to clarify the different radii defined for Saturn.
+Additional references that are publicly available were added for Saturn's 
+rings model. Jupiter's nutation precession angles, and
+Ganymede's W0 value were corrected to agree with the IAU 2000 report. 
+
+2004 Jun 21 (published)
+
+* Reference for new Phoebe GM:  IOM 312.0-024-04 "Navigation Results 
+from the Phoebe flyby", J.B. Jones, 16 June 2004.
+
+
+2004 Mar 05 (published)  
+
+  Updated descriptive text preceeding RS keyword.
+  Updated contact information and verified URLs.
+
+  Updates per ECR 103313:
+      Change 1:  Update the values for Phoebe Prime Meridian
+                 TO:
+                 BODY609_PM            = (  178.58   +931.639  0.  )
+
+                 Reference: Bauer, Simonelli, Buratti, IAU Circular 8279, 
+                            1/30/2004; re-reduced by Owen 2/5/2004
+
+      Change 2:  Saturn Reference Radius
+           ADD:
+           BODY699_RADII_RS = (    60330.      60330.       60330.     )
+           This radius models saturn as a sphere at 100 mbar. 
+                 
+                 Date: Tue, 25 Nov 2003 16:22:41 -0700
+                 From: Carolyn Porco <carolyn@ciclops.org>
+
+2002 Oct 01 (published)
+  Changed BODY699_RADII_OPTICAL to be consistent with recommendation of Phil
+  Nicholson dated 24 Sep. Added notes in the version history as to which
+  versions were published to the DOM, as opposed to the versions that were
+  intermediate for review.
+  
+
+
+  
+-------- FORMATTING FOR SPECIAL PARAMETERS
+
+
+BODYNNN_GM
+   GM in km^3/s^2
+   
+BODYNNN_RADII_OPTICAL
+BOYDNNN_RADII_RS
+BOYDNNN_RADII
+BODYNNN_RADII_1BAR
+
+    BODY699_RADII_OPTICAL is for PDT to determine at what altitude 
+    that Saturn first starts to cast a discernible shadow.
+
+    BODY699_RADII_RS models Saturn as a sphere and corresponds to a 100
+    mbar surface. 
+
+    BODY699_RADII and BODY699_RADII_1BAR correspond to a
+    1 bar surface.  BODY699_RADII contains IAU values. BODY699_RADII_1BAR
+    currently contains IAU values but will likely be updated during the
+    mission. 
+
+
+BODYNNN_ATMOSPHERE
+   Exponential atmospheric model in the form of one set of 
+        two values To, f, followed by any number of sets of 
+        three numbers Do, K, Zo. The atmospheric density in g/cm3 
+        can be calculated as follows: 
+        Z = height above surface (km) 
+        R = radius of body (km) 
+        T = thermospheric temperature (K) = To + f * sigma, where 
+        sigma is the number of standard deviations (conservatism) 
+        desired. If f > 0, positive sigma will result in a hotter 
+        thermosphere and higher density. 
+        H = scale height of atmosphere (km) = T * ( R + Z ) / K 
+        (K is a curve-fit parameter with units of degrees K) 
+        D = density (g/cm3) = Do * exp( - ( Z - Zo ) / H ) 
+        If there are more than one set of Do, K, Zo, sum each 
+        value to get the total atmospheric density.
+
+
+BODYNNN_RING*
+   The ring identification scheme is numeric with keyword-associated names.
+   The defnition of a ring is in a set of keywords. The BODYNNN_RING...
+   keyword set includes 
+
+
+   1) a required NAME keyword (BODYNNN_RING<n>_NAME), 
+   2) either a complete ring keyword (BODYNNN_RING<n>) or a set of segmented
+      ring keywords (BODYNNN_RING<n>_<X>), and 
+   3) optional embedded ringlet/gap keywords (BODYNNN_RING<n>_<n>) with
+      required names (BODYNNN_RING<n>_<n>_NAME). 
+
+
+   The total number of rings (BODYNNN_RING<n>) that can be defined is from
+   01 to 99. A complete ring can be segmented (BODYNNN_RING<n>_<X>) in upto
+   26 (A-Z) sub-segments. Embedded ringlets/gaps (BODYNNN_RING<n>_<n>) can
+   be defined from 1 to 99. Ring geometry is defined in the form of one set
+   of R1, R2, Z1, Z2, OD where R1 and R2 are inner and outer radii
+   respectively of the ring (in kilometers), Z1 and Z2 are the vertical
+   heights of the ring at R1 and R2 respectively (also in km, equal to 
+   one-half of the total thickness of the ring), and OD is the average optical
+   depth of the ring sub-segment/gap across R1 to R2. A complex ring
+   thickness model is pieced together by sub-segmenting Rs, Zs, & ODs; each
+   sub-segment is uniquely numbered.
+
+
+
+
+BODY699_RING7_FCENTER  
+   Elliptical orbital characteristics for the F Ring: The array items (and
+   units) are (in order):
+
+
+   SEMIMAJOR_AXIS (km)
+   ECCENTRICITY (degrees)
+   LONGITUDE_PERICENTER_EPOCH (degrees)
+   PERICENTER_PRECESSION_RATE (degrees)
+   INCLINATION (degrees)
+   LONGITUDE_ASCENDING_NODE_EPOCH (degrees)
+   NODAL_REGRESSION_RATE (degrees).
+
+
+   The epoch for the elements is J2000 (noon UTC on 1/1/2000) at the ring
+   (i.e., with no light-time correction). Longitudes are measured in the
+   prograde direction from the ascending node of Saturn's equatorial plane
+   on Earth's J2000 equator.
+
+
+-------- REFERENCES
+
+    1.   Seidelmann, P.K., Abalakin, V.K., Bursa, M., Davies, M.E.,
+         Bergh, C. de, Lieske, J.H., Oberst, J., Simon, J.L.,
+         Standish, E.M., Stooke, P., and Thomas, P.C. (2002).
+         "Report of the IAU/IAG Working Group on Cartographic
+         Coordinates and Rotational Elements of the Planets and
+         Satellites: 2000," Celestial Mechanics and Dynamical
+         Astronomy, v.82, Issue 1, pp. 83-111. 
+
+    2.   Nautical Almanac Office, United States Naval Observatory
+         and H.M. Nautical Almanac Office, Rutherford Appleton
+         Laboratory (2005).  "The Astronomical Almanac for
+         the Year 2002," U.S. Government Printing Office,
+         Washington, D.C.: and The Stationary Office, London.
+
+    3.   Russell, Christopher T., "Geophysical Coordinate Transformations," 
+         Cosmic Electrodynamics 2 (1971) 184-186.
+
+    4.   Showalter, Mark R. "Properties  of Saturn's E and G Rings from the
+         1995 Ring Plane Crossings", presented at Ames ring hazard
+         workshop, 25 January 1996.
+
+    5.   Jacobson, R. A. 2003b. private communication of constants 
+         used in the JUP230 ephemeris
+
+    6.   Jacobson, R.A., JPL IOM 312.F-99-084, 13 Oct 1999, "Sat105" 
+         ephemeris file
+
+    7.   Jacobson, R. A., 1996, "Orbits of the Saturnian Satellites 
+         from Earthbased and Voyager Observations", Blulletin of the 
+         American Astronmical Society 28(3), 1185.
+
+    8.   Bosh A.S., Olkin C.B., French R.G., Nicholson P.D. Icarus, 
+         May 2002, vol. 157, iss. 1, pp. 57-75(19)  
+
+    9.   Campbell, J.K., and J.D. Anderson, Gravity Field of the Saturnian 
+         System From Pioneer and Voyager Tracking Data, Astronomical 
+         Journal, 97, 1485-1495, 1989. 
+
+   10.   Cassini NAV OD solution SM828D.
+
+   11.   Cassini Mission Plan, JPL D-5564, Cassini document 699-100, 
+         revision N, May 2002.
+
+   12.   Cassini Dust Protection Plan, JPL D-24251, Cassini document 699-525,
+         revision A, October 2002. 
+
+   13.   Bauer, Simonelli, Buratti, IAU Circular 8279, 1/30/2004; 
+         re-reduced by Owen 2/5/2004
+
+   14.   Cassini NAV OD solution 040409_00Sa.   
+
+   15.   Cassini NAV OD solution 040615_00Sa.
+
+   16.   IOM 312.0-024-04 "Navigation Results from the Phoebe flyby", 
+         J.B. Jones, 16 June 2004.
+
+   17.   Cassini NAV OD solution 040909R. Reconstruction from Jupiter to SOI.
+
+   19.   Cuzzi, J. N., J. J. Lissauer, L. W. Esposito, J. B. Holberg, 
+         E. A. Marouf, G. L. Tyler, and A. Bouschot 1984. "Saturn's rings: 
+         Properties and processes." In Planetary Rings, (R. Greenberg and 
+         A. Brahic, Eds.), University of Arizona Press, Tucson, pp. 73-199. 
+
+   20.   HST High-Resolution Backscatter Image of Saturn's G Ring 
+         Jack J. Lissauer, Richard G. French Icarus, Vol. 146, No. 1, 
+         Jul 2000, pp. 12-18.
+
+   21.   NASA/JPL Web page: "Natural Satellite Physical Parameters", 
+         2004 September 22 <http://ssd.jpl.nasa.gov/sat_props.html>
+
+   22.   Porco, C.C., Thomas, P.C., Weiss, J.W., Richardson, D.C. 2007. 
+         Saturns Small Inner Satellites: Clues to Their Origins. Science 318, 1602.
+
+         Thomas, P.C., and 12 colleagues 2007. Shapes of the saturnian 
+         icy satellites and their significance. Icarus 190, 573-584. 
+
+   23.   Stiles, B. et als, "Determining Titan's Spin State from Cassini Radar
+         Images", Astronomical Journal, 135, 1669, May 2008. 
+
+   24.   Archinal, B.A., et als (2010).  
+         "Report of the IAU Working Group on Cartographic
+         Coordinates and Rotational Elements of the Planets and
+         Satellites: 2009"; Cassini ECR-100654 
+ 
+   Unless noted otherwise, values are from the IAU report. [1]
+
diff --git a/tests/pytests/data/N1702360370_1/naif0012.tls b/tests/pytests/data/N1702360370_1/naif0012.tls
new file mode 100644
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/N1702360370_1/naif0012.tls
@@ -0,0 +1,152 @@
+KPL/LSK
+
+
+LEAPSECONDS KERNEL FILE
+===========================================================================
+
+Modifications:
+--------------
+
+2016, Jul. 14   NJB  Modified file to account for the leapsecond that
+                     will occur on December 31, 2016.
+
+2015, Jan. 5    NJB  Modified file to account for the leapsecond that
+                     will occur on June 30, 2015.
+
+2012, Jan. 5    NJB  Modified file to account for the leapsecond that
+                     will occur on June 30, 2012.
+                     
+2008, Jul. 7    NJB  Modified file to account for the leapsecond that
+                     will occur on December 31, 2008.
+                     
+2005, Aug. 3    NJB  Modified file to account for the leapsecond that
+                     will occur on December 31, 2005.
+                     
+1998, Jul  17   WLT  Modified file to account for the leapsecond that
+                     will occur on December 31, 1998.
+                     
+1997, Feb  22   WLT  Modified file to account for the leapsecond that
+                     will occur on June 30, 1997.
+                     
+1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
+                     to 1-1-96.
+
+1995, Oct  25   WLT  Modified file to account for the leapsecond that
+                     will occur on Dec 31, 1995.
+
+1994, Jun  16   WLT  Modified file to account for the leapsecond on
+                     June 30, 1994.
+
+1993, Feb. 22  CHA   Modified file to account for the leapsecond on
+                     June 30, 1993.
+
+1992, Mar. 6   HAN   Modified file to account for the leapsecond on
+                     June 30, 1992.
+
+1990, Oct. 8   HAN   Modified file to account for the leapsecond on 
+                     Dec. 31, 1990.  
+
+
+Explanation:
+------------
+
+The contents of this file are used by the routine DELTET to compute the 
+time difference
+
+[1]       DELTA_ET  =  ET - UTC                                         
+          
+the increment to be applied to UTC to give ET. 
+
+The difference between UTC and TAI,
+
+[2]       DELTA_AT  =  TAI - UTC
+
+is always an integral number of seconds. The value of DELTA_AT was 10
+seconds in January 1972, and increases by one each time a leap second
+is declared. Combining [1] and [2] gives
+
+[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)
+
+                    =  (ET - TAI) + DELTA_AT
+
+The difference (ET - TAI) is periodic, and is given by
+
+[4]       ET - TAI  =  DELTA_T_A  + K sin E 
+
+where DELTA_T_A and K are constant, and E is the eccentric anomaly of the 
+heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores 
+small-period fluctuations, is accurate to about 0.000030 seconds.
+
+The eccentric anomaly E is given by 
+
+[5]       E = M + EB sin M
+
+where M is the mean anomaly, which in turn is given by 
+
+[6]       M = M  +  M t
+               0     1
+
+where t is the number of ephemeris seconds past J2000.
+
+Thus, in order to compute DELTA_ET, the following items are necessary.
+
+          DELTA_TA
+          K
+          EB
+          M0
+          M1
+          DELTA_AT      after each leap second.
+
+The numbers, and the formulation, are taken from the following sources.
+
+     1) Moyer, T.D., Transformation from Proper Time on Earth to 
+        Coordinate Time in Solar System Barycentric Space-Time Frame
+        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
+        33-56 and 57-68.
+
+     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
+        Reference System on Algorithms for Computing Time Differences
+        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.
+
+The variable names used above are consistent with those used in the 
+Astronomical Almanac.
+
+\begindata
+
+DELTET/DELTA_T_A       =   32.184
+DELTET/K               =    1.657D-3
+DELTET/EB              =    1.671D-2
+DELTET/M               = (  6.239996D0   1.99096871D-7 )
+
+DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
+                           11,   @1972-JUL-1     
+                           12,   @1973-JAN-1     
+                           13,   @1974-JAN-1     
+                           14,   @1975-JAN-1          
+                           15,   @1976-JAN-1          
+                           16,   @1977-JAN-1          
+                           17,   @1978-JAN-1          
+                           18,   @1979-JAN-1          
+                           19,   @1980-JAN-1          
+                           20,   @1981-JUL-1          
+                           21,   @1982-JUL-1          
+                           22,   @1983-JUL-1          
+                           23,   @1985-JUL-1          
+                           24,   @1988-JAN-1 
+                           25,   @1990-JAN-1
+                           26,   @1991-JAN-1 
+                           27,   @1992-JUL-1
+                           28,   @1993-JUL-1
+                           29,   @1994-JUL-1
+                           30,   @1996-JAN-1 
+                           31,   @1997-JUL-1
+                           32,   @1999-JAN-1
+                           33,   @2006-JAN-1
+                           34,   @2009-JAN-1
+                           35,   @2012-JUL-1
+                           36,   @2015-JUL-1 
+                           37,   @2017-JAN-1 )
+
+\begintext
+
+
diff --git a/tests/pytests/data/N1702360370_1/pck00010.tpc b/tests/pytests/data/N1702360370_1/pck00010.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..efa020922dc961191712ff8512cb4f95ea82036d
--- /dev/null
+++ b/tests/pytests/data/N1702360370_1/pck00010.tpc
@@ -0,0 +1,4061 @@
+KPL/PCK
+ 
+ 
+P_constants (PcK) SPICE kernel file
+===========================================================================
+
+        By: Nat Bachman (NAIF)    2011 October 21
+ 
+ 
+Purpose
+--------------------------------------------------------
+
+     This file makes available for use in SPICE-based application
+     software orientation and size/shape data for natural bodies. The
+     principal source of the data is a published report by the IAU
+     Working Group on Cartographic Coordinates and Rotational Elements
+     [1].
+
+     Orientation and size/shape data not provided by this file may be
+     available in mission-specific PCK files. Such PCKs may be the
+     preferred data source for mission-related applications.
+     Mission-specific PCKs can be found in PDS archives or on the NAIF
+     web site at URL:
+
+        http://naif.jpl.nasa.gov/naif/data
+
+
+File Organization
+--------------------------------------------------------
+ 
+     The contents of this file are as follows.
+ 
+     Introductory Information:
+
+         --   Purpose
+
+         --   File Organization
+ 
+         --   Version description
+ 
+         --   Disclaimer
+ 
+         --   Sources
+ 
+         --   Explanatory notes
+ 
+         --   Body numbers and names
+ 
+
+     PcK Data:
+ 
+
+        Orientation Data
+        ----------------
+
+         --   Orientation constants for the Sun, planets, and
+              Pluto. Additional items included in this section:
+
+                 - Earth north geomagnetic centered dipole value
+                   for the epochs 2012
+
+         --   Orientation constants for satellites
+ 
+         --   Orientation constants for asteroids 
+
+                 Davida
+                 Eros
+                 Gaspra
+                 Ida
+                 Itokawa
+                 Lutetia
+                 Pallas
+                 Steins
+                 Vesta
+ 
+         --   Orientation constants for comets 
+
+                 19P/Borrelly
+                 9P/Tempel 1
+
+
+         Orientation data provided in this file are used
+         by the SPICE Toolkit to evaluate the orientation
+         of body-fixed, body-centered reference frames
+         with respect to the ICRF frame ("J2000" in
+         SPICE documentation). These body-fixed frames
+         have names of the form
+
+            IAU_<body name>
+
+         for example
+
+            IAU_JUPITER
+
+         See the PCK Required Reading file pck.req for details.
+
+
+
+        Radii of Bodies
+        ---------------
+
+         --   Radii of Sun, planets, and Pluto
+         
+         --   Radii of satellites, where available
+         
+         --   Radii of asteroids 
+
+                 Ceres
+                 Davida
+                 Eros
+                 Gaspra
+                 Ida 
+                 Itokawa
+                 Lutetia
+                 Mathilde
+                 Steins
+                 Toutatis
+                 Vesta
+            
+         --   Radii of comets 
+
+                 19P/Borrelly
+                 81P/Wild 2
+                 9P/Tempel 1
+                 Halley
+
+
+
+Version Description
+--------------------------------------------------------
+ 
+     This file was created on October 21, 2011 at NASA's Navigation and
+     Ancillary Information Facility (NAIF), located at the Jet
+     Propulsion Laboratory, Pasadena, CA.
+
+     The previous version of the file was
+     
+        pck00009.tpc
+
+     That file was published March 3 2010.
+
+     This version incorporates data from reference [1]. This file
+     contains size, shape, and orientation data for all objects covered
+     by the previous version of the file.
+
+     New objects covered by this file but not the previous
+     version are:
+
+        Anthe
+        Daphnis
+        Davida
+        Lutetia
+        Methone
+        Pallas
+        Pallene
+        Polydeuces
+        Steins
+ 
+                         
+ 
+Disclaimer
+--------------------------------------------------------
+ 
+Applicability of Data
+
+     This P_constants file may not contain the parameter values that
+     you prefer. NAIF suggests that you inspect this file visually
+     before proceeding with any critical or extended data processing.
+
+File Modifications by Users
+
+     Note that this file may be readily modified by you to change
+     values or add/delete parameters. NAIF requests that you update the
+     "by line," date, version description section, and file name
+     if you modify this file.
+     
+     A user-modified file should be thoroughly tested before 
+     being published or otherwise distributed.
+
+     P_constants files must conform to the standards described
+     in the two SPICE technical reference documents:
+
+        PCK Required Reading
+        Kernel Required Reading
+
+
+Known Limitations and Caveats
+
+     Accuracy
+     --------
+
+     In general, the orientation models given here are claimed by the
+     IAU Working Group Report [1] to be accurate to 0.1 degree
+     ([1], p.158). However, NAIF notes that orientation models for
+     natural satellites and asteroids have in some cases changed
+     substantially with the availability of new observational data, so
+     users are urged to investigate the suitability for their
+     applications of the models presented here.
+
+     Earth orientation
+     -----------------
+
+     NAIF strongly cautions against using the earth rotation model
+     (from [1]), corresponding to the SPICE reference frame name
+     IAU_EARTH, for work demanding high accuracy. This model has been
+     determined by NAIF to have an error in the prime meridian location
+     of magnitude at least 150 arcseconds, with a local minimum
+     occurring during the year 1999. Regarding availability of better
+     earth orientation data for use with the SPICE system:
+
+        Earth orientation data are available from NAIF in the form of
+        binary earth PCK files. These files provide orientation data
+        for the ITRF93 (terrestrial) reference frame relative to the
+        ICRF.
+
+        NAIF employs an automated process to create these files; each
+        time JPL's Tracking Systems and Applications Section produces a
+        new earth orientation parameter (EOP) file, a new PCK is
+        produced. These PCKs cover a roughly 10 year time span starting
+        at Jan. 1, 2000. In these PCK files, the following effects are
+        accounted for in modeling the earth's rotation:
+
+           - Precession:                   1976 IAU model
+
+           - Nutation:                     1980 IAU model, plus interpolated
+                                           EOP nutation corrections
+
+           - Polar motion:                 interpolated from EOP file
+
+           - True sidereal time:
+
+                  UT1 - UT1R (if needed):  given by analytic formula
+                + TAI - UT1 (or UT1R):     interpolated from EOP file
+                + UT1 - GMST:              given by analytic formula
+                + equation of equinoxes:   given by analytic formula
+
+             where
+
+                TAI    =   International Atomic Time
+                UT1    =   Greenwich hour angle of computed mean sun - 12h
+                UT1R   =   Regularized UT1
+                GMST   =   Greenwich mean sidereal time                   
+
+        These kernels are available from the NAIF web site
+
+           http://naif.jpl.nasa.gov
+
+        (follow the links to Data, generic_kernels, and PCK data) or
+
+           ftp://naif.jpl.nasa.gov/pub/naif/generic_kernels/pck
+
+        or via anonymous ftp from the server
+ 
+           naif.jpl.nasa.gov
+
+        The kernels are in the path
+
+           pub/naif/generic_kernels/pck
+
+        At this time, these kernels have file names of the form
+
+           earth_000101_yymmdd_yymmdd.bpc
+
+        The first date in the file name, meaning 2000 January 1, is the
+        file's coverage begin time. The second and third dates are,
+        respectively, the file's coverage end time and the epoch of the
+        last datum.
+ 
+        These binary PCK files are very accurate (error < 0.1
+        microradian) for epochs preceding the epoch of the last datum.
+        For later epochs, the error rises to several microradians.
+
+        Binary PCK files giving accurate earth orientation from 1972 to
+        2007 and *low accuracy* predicted earth orientation from
+        2007 to 2037 are also available in the same location. See the
+        aareadme.txt file at the "pck" URL above for details.
+
+        Characteristics and names of the binary kernels described here
+        are subject to change. See the "pck" URL above for information
+        on current binary earth PCKs.
+
+
+     Lunar orientation
+     -----------------
+
+     The lunar orientation formula provided by this file is a
+     trigonometric polynomial approximation yielding the orientation of
+     the lunar "Mean Earth/Polar Axis" (ME) reference frame. The
+     SPICE reference frame name corresponding to this model is
+     IAU_MOON.
+
+     A more accurate approximation can be obtained by using both the
+     NAIF lunar frame kernel and the binary lunar orientation PCK file.
+     These files provide orientation data for the both the Mean
+     Earth/Polar Axis frame, which has the SPICE name MOON_ME, and the
+     Lunar Principal Axes frame, which has the SPICE name MOON_PA.
+
+     These files are available on the NAIF web site (see URLs above)
+     and in the NAIF server's ftp area. The lunar frame kernel is
+     located in the path
+ 
+        pub/naif/generic_kernels/fk/satellites
+
+     and has a name of the form
+
+        moon_yymmdd.tf
+
+     The binary lunar PCK is in the path
+
+        pub/naif/generic_kernels/pck
+
+     and has a name of the form
+
+        moon_pa_dennn_yyyy-yyyy.bpc
+
+     See the "aareadme.txt" files in the paths shown above for details
+     on file contents and versions. We also suggest you refer to the
+     SPICE tutorial named "lunar_earth_pck-fk," which is available from
+     the NAIF web site.
+
+
+     Earth geomagnetic dipole
+     ------------------------
+
+     The SPICE Toolkit doesn't currently contain software to model the
+     earth's north geomagnetic centered dipole as a function of time.
+     As a convenience for users, the north dipole location from the
+     epoch 2012.0 was selected as a representative datum, and the
+     planetocentric longitude and latitude of this location have been
+     associated with the keywords
+       
+        BODY399_N_GEOMAG_CTR_DIPOLE_LON
+        BODY399_N_GEOMAG_CTR_DIPOLE_LAT
+     
+     Values for the earth's north geomagnetic centered dipole are
+     presented in comments as a discrete time series for the time range
+     1945-2000. For details concerning the geomagnetic field model from
+     which these values were derived, including a discussion of the
+     model's accuracy, see [9] and [11].
+ 
+
+     Prime meridian offsets
+     ----------------------
+
+     Prime meridian offset kernel variables, which have names
+     of the form
+
+        BODYnnn_LONG_AXIS
+
+     are not used by SPICE geometry software. These variables should be
+     considered deprecated; however, they will be retained for
+     backwards compatibility.
+
+     Users wishing to specify an offset reflecting the orientation of a
+     reference ellipsoid relative to a body-fixed reference frame
+     specified here should do so by creating a constant-offset frame
+     (also called a "TK" frame) specification. See the Frames Required
+     Reading frames.req for details.
+ 
+     The Mars prime meridian offset given by [5] is provided for 
+     informational purposes only.
+
+
+     Software limitations
+     --------------------
+
+     SPICE Toolkits prior to version N0057 cannot make use of
+     trigonometric polynomial terms in the formulas for orientation of
+     the planets.
+ 
+     The second nutation precession angle (M2) for Mars is represented
+     by a quadratic polynomial in the 2006 IAU report. The SPICELIB
+     subroutine BODEUL can not handle this term (which is extremely
+     small), so we truncate the polynomial to a linear one. The 
+     resulting orientation error has a maximum magnitude of less
+     than 0.0032 degrees over the time span 1996-2015 and less than
+     0.0082 degrees over the time span 1986-2025.
+
+
+Sources and References
+--------------------------------------------------------
+ 
+     The sources for the constants listed in this file are:
+
+
+        [1]   Archinal, B.A., A'Hearn, M.F., Bowell, E., Conrad, A.,
+              Consolmagno, G.J., Courtin, R., Fukushima, T., 
+              Hestroffer, D., Hilton, J.L., Krasinsky, G.A.,
+              Neumann, G., Oberst, J., Seidelmann, P.K., Stooke, P.,
+              Tholen, D.J., Thomas, P.C., and Williams, I.P. 
+              "Report of the IAU Working Group on Cartographic Coordinates 
+              and Rotational Elements: 2009."
+
+        [2]   Archinal, B.A., A'Hearn, M.F., Conrad, A.,
+              Consolmagno, G.J., Courtin, R., Fukushima, T., 
+              Hestroffer, D., Hilton, J.L., Krasinsky, G.A.,
+              Neumann, G., Oberst, J., Seidelmann, P.K., Stooke, P.,
+              Tholen, D.J., Thomas, P.C., and Williams, I.P. 
+              "Erratum to: Reports of the IAU Working Group on
+              Cartographic Coordinates and Rotational Elements: 2006 &
+              2009."
+
+        [3]   Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F., 
+              Conrad, A., Consolmagno, G.J., Hestroffer, D.,
+              Hilton, J.L., Krasinsky, G.A., Neumann, G.,
+              Oberst, J., Stooke, P., Tedesco, E.F., Tholen, D.J., 
+              and Thomas, P.C. "Report of the IAU/IAG Working Group 
+              on cartographic coordinates and rotational elements: 2006."
+ 
+        [4]   Nautical Almanac Office, United States Naval Observatory
+              and H.M. Nautical Almanac Office, Rutherford Appleton
+              Laboratory (2010). "The Astronomical Almanac for
+              the Year 2010," U.S. Government Printing Office,
+              Washington, D.C.: and The Stationary Office, London.
+
+        [5]   Duxbury, Thomas C. (2001). "IAU/IAG 2000 Mars Cartographic
+              Conventions,"  presentation to the Mars Express Data
+              Archive Working Group, Dec. 14, 2001.
+
+        [6]   Russell, C.T. and Luhmann, J.G. (1990). "Earth: Magnetic 
+              Field and Magnetosphere." <http://www-ssc.igpp.ucla.
+              edu/personnel/russell/papers/earth_mag>. Originally
+              published in "Encyclopedia of Planetary Sciences," J.H.
+              Shirley and R.W. Fainbridge, eds. Chapman and Hall,
+              New York, pp 208-211.
+
+        [7]   Russell, C.T. (1971). "Geophysical Coordinate 
+              Transformations," Cosmic Electrodynamics 2  184-186.
+              NAIF document 181.0.
+     
+        [8]   ESA/ESTEC Space Environment Information System (SPENVIS)
+              (2003). Web page:  "Dipole approximations of the
+              geomagnetic field."  <http://www.spenvis.oma.be/spenvis/
+              help/background/magfield/cd.html>.
+ 
+        [9]   International Association of Geomagnetism and Aeronomy
+              and International Union of Geodesy and Geophysics (2004).
+              Web page:  "The 9th Generation International Geomagnetic
+              Reference Field." <http://www.ngdc.noaa.gov/
+              IAGA/vmod/igrf.html>.
+                             
+        [10]  Davies, M.E., Abalakin, V.K., Bursa, M., Hunt, G.E.,
+              and Lieske, J.H. (1989). "Report of the IAU/IAG/COSPAR
+              Working Group on Cartographic Coordinates and Rotational
+              Elements of the Planets and Satellites: 1988," Celestial
+              Mechanics and Dynamical Astronomy, v.46, no.2, pp.
+              187-204.
+
+        [11]  International Association of Geomagnetism and Aeronomy
+              Web page:  "International Geomagnetic Reference Field."  
+              Discussion URL:
+
+                 http://www.ngdc.noaa.gov/IAGA/vmod/igrf.html
+
+              Coefficients URL:
+
+                 http://www.ngdc.noaa.gov/IAGA/vmod/igrf11coeffs.txt
+
+         
+
+     Most values are from [1]. All exceptions are 
+     commented where they occur in this file. The exceptions are:
+ 
+                 
+         --   Radii for the Sun are from [4].
+
+         --   Prime meridian constant (W0) terms for Pluto, Charon,
+              and Ida are from [2].
+             
+         --   The second nutation precession angle (M2) for Mars is
+              represented by a quadratic polynomial in the 2000
+              IAU report. The SPICELIB subroutine BODEUL can not
+              handle this term (which is extremely small), so we
+              truncate the polynomial to a linear one.
+           
+          --  Earth north geomagnetic centered dipole values are from
+              [11]. The values were also computed from the 11th
+              generation IGRF by Nat Bachman.
+         
+
+     "Old values" listed are from the SPICE P_constants file
+     pck00009.tpc dated March 3, 2010. Most of these values came
+     from the 2006 IAU report [3].
+ 
+ 
+ 
+ 
+Explanatory Notes
+--------------------------------------------------------
+
+     This file, which is logically part of the SPICE P-kernel, contains
+     constants used to model the orientation, size and shape of the
+     Sun, planets, natural satellites, and selected comets and
+     asteroids. The orientation models express the direction of the
+     pole and location of the prime meridian of a body as a function of
+     time. The size/shape models ("shape models" for short) represent
+     all bodies as ellipsoids, using two equatorial radii and a polar
+     radius. Spheroids and spheres are obtained when two or all three
+     radii are equal.
+
+     The SPICE Toolkit routines that use this file are documented in
+     the SPICE "Required Reading" file pck.req. They are also 
+     documented in the "PCK" SPICE tutorial, which is available on
+     the NAIF web site.
+
+File Format
+        
+     A terse description of the PCK file format is given here. See the
+     SPICE "Required Reading" files pck.req and kernel.req for a
+     detailed explanation of the SPICE text kernel file format. The
+     files pck.req and kernel.req are included in the documentation
+     provided with the SPICE Toolkit.
+
+     The file starts out with the ``ID word'' string
+
+        KPL/PCK
+
+     This string identifies the file as a text kernel containing PCK 
+     data.
+
+     This file consists of a series of comment blocks and data blocks.
+     Comment blocks, which contain free-form descriptive or explanatory
+     text, are preceded by a \begintext token. Data blocks follow a
+     \begindata token. In order to be recognized, each of these tokens
+     must be placed on a line by itself.
+
+     The portion of the file preceding the first data block is treated
+     as a comment block; it doesn't require an initial \begintext
+     token.
+
+     This file identifies data using a series of
+
+        KEYWORD = VALUE
+
+     assignments. The left hand side of each assignment is a
+     "kernel variable" name; the right hand side is an associated value
+     or list of values. The SPICE subroutine API allows SPICE routines
+     and user applications to retrieve the set of values associated
+     with each kernel variable name.
+
+     Kernel variable names are case-sensitive and are limited to
+     32 characters in length. 
+
+     Numeric values may be integer or floating point. String values
+     are normally limited to 80 characters in length; however, SPICE
+     provides a mechanism for identifying longer, "continued" strings.
+     See the SPICE routine STPOOL for details.
+
+     String values are single quoted.
+
+     When the right hand side of an assignment is a list of values,
+     the list items may be separated by commas or simply by blanks.
+     The list must be bracketed by parentheses. Example:
+
+        BODY399_RADII     = ( 6378.1366   6378.1366   6356.7519 )
+ 
+     Any blanks preceding or following keyword names, values and equal
+     signs are ignored.
+  
+     Assignments may be spread over multiple lines, for example:
+
+        BODY399_RADII     = ( 6378.1366  
+                              6378.1366
+                              6356.7519 )
+
+     This file may contain blank lines anywhere. Non-printing
+     characters including TAB should not be present in the file: the
+     presence of such characters may cause formatting errors when the
+     file is viewed.
+
+Time systems and reference frames
+
+     The 2009 IAU Working Group Report [1] states the time scale used
+     as the independent variable for the rotation formulas is
+     Barycentric Dynamical Time (TDB) and that the epoch of variable
+     quantities is J2000 TDB (2000 Jan 1 12:00:00 TDB, Julian ephemeris
+     date 2451545.0 TDB). Throughout SPICE documentation and in this
+     file, we use the names "J2000 TDB" and "J2000" for this epoch. The
+     name "J2000.0" is equivalent.
+
+     SPICE documentation refers to the time system used in this file 
+     as either "ET" or "TDB." SPICE software makes no distinction 
+     between TDB and the time system associated with the independent
+     variable of the JPL planetary ephemerides T_eph.
+ 
+     The inertial reference frame used for the rotational elements in
+     this file is identified by [1] as the ICRF (International
+     Celestial Reference Frame). 
+
+     The SPICE PCK software that reads this file uses the label "J2000"
+     to refer to the ICRF; this is actually a mislabeling which has
+     been retained in the interest of backward compatibility. Using
+     data from this file, by means of calls to the SPICE frame
+     transformation routines, will actually compute orientation
+     relative to the ICRF.
+
+     The difference between the J2000 frame and the ICRF is
+     on the order of tens of milliarcseconds and is well below the
+     accuracy level of the formulas in this file.
+
+Orientation models
+ 
+     All of the orientation models use three Euler angles to describe
+     the orientation of the coordinate axes of the "Body Equator and
+     Prime Meridian" system with respect to an inertial system. By
+     default, the inertial system is the ICRF (labeled as "J2000"), but
+     other inertial frames can be specified in the file. See the PCK
+     Required Reading for details.
+ 
+     The first two angles, in order, are the ICRF right ascension and
+     declination (henceforth RA and DEC) of the north pole of a body as
+     a function of time. The third angle is the prime meridian location
+     (represented by "W"), which is expressed as a rotation about the
+     north pole, and is also a function of time.
+ 
+     For each body, the expressions for the north pole's right
+     ascension and declination, as well as prime meridian location, are
+     sums (as far as the models that appear in this file are concerned)
+     of quadratic polynomials and trigonometric polynomials, where the
+     independent variable is time.
+ 
+     In this file, the time arguments in expressions always refer to
+     Barycentric Dynamical Time (TDB), measured in centuries or days
+     past a reference epoch. By default, the reference epoch is the
+     J2000 epoch, which is Julian ephemeris date 2451545.0 (2000 Jan 1
+     12:00:00 TDB), but other epochs can be specified in the file. See
+     the PCK Required Reading for details.
+
+     Orientation models for satellites and some planets (including
+     Jupiter) involve both polynomial terms and trigonometric terms.
+     The arguments of the trigonometric terms are linear polynomials.
+     In this file, we call the arguments of these trigonometric terms
+     "nutation precession angles."
+
+     Example: 2009 IAU Model for orientation of Jupiter.  Note that 
+     these values are used as an example only; see the data area below 
+     for current values.
+
+        Right ascension
+        ---------------
+ 
+        alpha   =  268.056595 - 0.006499 T        +  0.000117 sin(Ja) 
+             0                + 0.000938 sin(Jb)  +  0.001432 sin(Jc)
+                              + 0.000030 sin(Jd)  +  0.002150 sin(Je)
+
+        Declination
+        -----------
+ 
+        delta   =   64.495303 + 0.002413 T        +  0.000050 cos(Ja)
+             0                + 0.000404 cos(Jb)  +  0.000617 cos(Jc)
+                              - 0.000013 cos(Jd)  +  0.000926 cos(Je)
+
+        Prime meridian
+        --------------
+
+        W       =  284.95  + 870.5366420 d
+ 
+
+     Here
+
+        T represents centuries past J2000 ( TDB ),
+ 
+        d represents days past J2000 ( TDB ).
+
+        Ja-Je are nutation precession angles.
+
+     In this file, the polynomials' coefficients above are assigned 
+     to kernel variable names (left-hand-side symbols) as follows
+
+        BODY599_POLE_RA        = (   268.056595     -0.006499       0. )
+        BODY599_POLE_DEC       = (    64.495303      0.002413       0. )
+        BODY599_PM             = (   284.95        870.5360000      0. )
+
+     and the trigonometric polynomials' coefficients are assigned 
+     as follows
+
+        BODY599_NUT_PREC_RA  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000117
+                                                                0.000938
+                                                                0.001432
+                                                                0.000030
+                                                                0.002150 )
+
+        BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000050
+                                                                0.000404
+                                                                0.000617
+                                                               -0.000013
+                                                                0.000926 )
+
+        BODY599_NUT_PREC_PM  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.0
+                                                                0.0
+                                                                0.0
+                                                                0.0
+                                                                0.0  ) 
+
+     Note the number "599"; this is the NAIF ID code for Jupiter.
+
+     In this file, the polynomial expressions for the nutation
+     precession angles are listed along with the planet's RA, DEC, and
+     prime meridian terms. Below are the 2006 IAU nutation precession
+     angles for the Jupiter system.
+
+        J1  =   73.32      +  91472.9 T
+        J2  =   24.62      +  45137.2 T
+        J3  =  283.90      +   4850.7 T
+        J4  =  355.80      +   1191.3 T
+        J5  =  119.90      +    262.1 T
+        J6  =  229.80      +     64.3 T
+        J7  =  352.25      +   2382.6 T
+        J8  =  113.35      +   6070.0 T
+
+        J9  =  146.64      + 182945.8 T
+        J10 =   49.24      +  90274.4 T 
+
+        Ja  =   99.360714  +   4850.4046 T
+        Jb  =  175.895369  +   1191.9605 T
+        Jc  =  300.323162  +    262.5475 T
+        Jd  =  114.012305  +   6070.2476 T
+        Je  =   49.511251  +     64.3000 T
+
+     Here
+
+        T represents centuries past J2000 ( TDB )
+
+        J1-J10 and Ja-Je are the nutation precession angles. The angles
+        J9 and J10 are equal to 2*J1 and 2*J2, respectively.
+ 
+        Angles J9 and J10 are not present in [1]; they have been added
+        to fit the terms 2*J1 and 2*J2, which appear in the orientation
+        models of several satellites, into a form that can be accepted
+        by the PCK system.
+
+     The assignment of the nutation precession angles for the
+     Jupiter system is as follows:
+ 
+        BODY5_NUT_PREC_ANGLES  = (    73.32      91472.9
+                                      24.62      45137.2
+                                     283.90       4850.7
+                                     355.80       1191.3
+                                     119.90        262.1
+                                     229.80         64.3
+                                     352.25       2382.6
+                                     113.35       6070.0   
+                                     146.64     182945.8
+                                      49.24      90274.4  
+                                      99.360714   4850.4046
+                                     175.895369   1191.9605
+                                     300.323162    262.5475
+                                     114.012305   6070.2476
+                                      49.511251     64.3000  )
+
+     You'll see an additional symbol grouped with the ones listed
+     above; it is
+ 
+        BODY599_LONG_AXIS
+ 
+     This is a deprecated feature; see the note on "Prime meridian
+     offsets" under "Known Limitations and Caveats" above.
+
+     The pattern of the formulas for satellite orientation is similar
+     to that for Jupiter. Example: 2006 IAU values for Io. Again, these
+     values are used as an example only; see the data area below for
+     current values.
+ 
+        Right ascension
+        ---------------
+
+        alpha  = 268.05  -  0.009 T  + 0.094 sin(J3)  +  0.024 sin(J4)
+             0  
+
+        Declination
+        -----------
+
+        delta  =  64.50  +  0.003 T  + 0.040 cos(J3)  +  0.011 cos(J4)
+             0           
+                          
+        Prime meridian
+        --------------
+
+        W      = 200.39  +  203.4889538 d  -  0.085 sin(J3)  -  0.022 sin(J4)
+
+ 
+        d represents days past J2000.
+ 
+        J3 and J4 are nutation precession angles.
+ 
+     The polynomial terms are assigned to symbols by the statements
+ 
+        BODY501_POLE_RA       = (  268.05          -0.009      0. )
+        BODY501_POLE_DEC      = (   64.50           0.003      0. )
+        BODY501_PM            = (  200.39         203.4889538  0. )
+ 
+     The coefficients of the trigonometric terms are assigned to symbols by
+     the statements
+
+        BODY501_NUT_PREC_RA   = (    0.   0.     0.094    0.024   )
+        BODY501_NUT_PREC_DEC  = (    0.   0.     0.040    0.011   )
+        BODY501_NUT_PREC_PM   = (    0.   0.    -0.085   -0.022   )
+
+     501 is the NAIF ID code for Io.
+ 
+     SPICE software expects the models for satellite orientation to
+     follow the form of the model shown here: the polynomial portions of the
+     RA, DEC, and W expressions are expected to be quadratic, the 
+     trigonometric terms for RA and W (satellite prime meridian) are expected 
+     to be linear combinations of sines of nutation precession angles, the 
+     trigonometric terms for DEC are expected to be linear combinations of 
+     cosines of nutation precession angles, and the polynomials for the 
+     nutation precession angles themselves are expected to be linear.
+ 
+     Eventually, the software will handle more complex expressions, we
+     expect.
+ 
+ 
+Shape models
+ 
+     There is only one kind of shape model supported by the SPICE
+     Toolkit software at present: the triaxial ellipsoid. The 2009 IAU
+     report [1] does not use any other models, except in the case of
+     Mars, where separate values are given for the north and south
+     polar radii. In this file, we provide as a datum the mean Mars
+     polar radius provided by [1]. The North and South values are
+     included as comments.
+
+     For each body, three radii are listed:  The first number is
+     the largest equatorial radius (the length of the semi-axis
+     containing the prime meridian), the second number is the smaller
+     equatorial radius, and the third is the polar radius.
+ 
+     Example: Radii of the Earth.
+ 
+        BODY399_RADII     = ( 6378.1366   6378.1366   6356.7519 )
+
+ 
+ 
+Body Numbers and Names
+--------------------------------------------------------
+ 
+ 
+     The following NAIF body ID codes and body names appear in this
+     file. See the NAIF IDs Required Reading file naif_ids.req for
+     a detailed discussion and a complete list of ID codes and names.
+
+
+        1  Mercury barycenter
+        2  Venus barycenter
+        3  Earth barycenter
+        4  Mars barycenter
+        5  Jupiter barycenter
+        6  Saturn barycenter
+        7  Uranus barycenter
+        8  Neptune barycenter
+        9  Pluto barycenter
+        10 Sun
+
+ 
+        199 Mercury
+ 
+ 
+        299 Venus
+ 
+ 
+        399 Earth
+ 
+        301 Moon
+ 
+ 
+        499 Mars
+ 
+        401 Phobos      402 Deimos
+ 
+ 
+        599 Jupiter
+ 
+        501 Io          502 Europa      503 Ganymede    504 Callisto
+        505 Amalthea    506 Himalia     507 Elara       508 Pasiphae
+        509 Sinope      510 Lysithea    511 Carme       512 Ananke
+        513 Leda        514 Thebe       515 Adrastea    516 Metis
+ 
+ 
+        699 Saturn
+ 
+        601 Mimas       602 Enceladus   603 Tethys      604 Dione
+        605 Rhea        606 Titan       607 Hyperion    608 Iapetus
+        609 Phoebe      610 Janus       611 Epimetheus  612 Helene
+        613 Telesto     614 Calypso     615 Atlas       616 Prometheus
+        617 Pandora     618 Pan         632 Methone     633 Pallene
+        634 Polydeuces  635 Daphnis     649 Anthe
+ 
+ 
+        799 Uranus
+ 
+        701 Ariel       702 Umbriel     703 Titania     704 Oberon
+        705 Miranda     706 Cordelia    707 Ophelia     708 Bianca
+        709 Cressida    710 Desdemona   711 Juliet      712 Portia
+        713 Rosalind    714 Belinda     715 Puck
+ 
+ 
+        899 Neptune
+ 
+        801 Triton      802 Nereid      803 Naiad       804 Thalassa
+        805 Despina     806 Galatea     807 Larissa     808 Proteus
+ 
+ 
+        999 Pluto
+ 
+        901 Charon
+ 
+ 
+        1000005 Comet 19P/Borrelly
+        1000036 Comet Halley
+        1000093 Comet 9P/Tempel 1
+        1000107 Comet 81P/Wild 2
+
+        2000001 Asteroid Ceres
+        2000002 Asteroid Pallas
+        2000004 Asteroid Vesta
+        2000021 Asteroid Lutetia
+        2000216 Asteroid Kleopatra
+        2000253 Asteroid Mathilde
+        2000433 Asteroid Eros
+        2000511 Asteroid Davida
+        2002867 Asteroid Steins
+        2004179 Asteroid Toutatis
+        2025143 Asteroid Itokawa
+        2431010 Asteroid Ida
+        9511010 Asteroid Gaspra
+        
+ 
+Orientation Constants for the Sun and Planets
+--------------------------------------------------------
+ 
+
+Sun
+ 
+     Old values:
+
+        Values are unchanged in the 2009 IAU report.
+
+     Current values:
+ 
+        \begindata
+ 
+        BODY10_POLE_RA         = (  286.13       0.          0. )
+        BODY10_POLE_DEC        = (   63.87       0.          0. )
+        BODY10_PM              = (   84.176     14.18440     0. )
+        BODY10_LONG_AXIS       = (    0.                        )
+
+        \begintext
+ 
+Mercury
+ 
+     Old values:
+ 
+        Values are from the 2006 IAU report.
+
+        body199_pole_ra          = (  281.01     -0.033      0. )
+        body199_pole_dec         = (   61.45     -0.005      0. )
+        body199_pm               = (  329.548     6.1385025  0. )
+
+
+     Current values:
+  
+        \begindata
+
+        BODY199_POLE_RA          = (  281.0097   -0.0328     0. )
+        BODY199_POLE_DEC         = (   61.4143   -0.0049     0. )
+        BODY199_PM               = (  329.5469    6.1385025  0. )
+ 
+        BODY199_LONG_AXIS        = (    0.                        )
+
+        BODY199_NUT_PREC_RA  = ( 0. 0. 0. 0. 0. )
+
+        BODY199_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. )
+
+        BODY199_NUT_PREC_PM  = (    0.00993822
+                                   -0.00104581
+                                   -0.00010280
+                                   -0.00002364
+                                   -0.00000532  )  
+        \begintext 
+
+           The linear coefficients have been scaled up from degrees/day
+           to degrees/century, because the SPICELIB PCK reader expects
+           these units.  The original constants were:
+                         
+                                    174.791086      4.092335
+                                    349.582171      8.184670
+                                    164.373257     12.277005
+                                    339.164343     16.369340
+                                    153.955429     20.461675
+
+
+        \begindata
+
+        BODY1_NUT_PREC_ANGLES  = ( 174.791086  0.14947253587500003E+06   
+                                   349.582171  0.29894507175000006E+06
+                                   164.373257  0.44841760762500006E+06  
+                                   339.164343  0.59789014350000012E+06    
+                                   153.955429  0.74736267937499995E+06 )
+        \begintext
+ 
+  
+Venus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY299_POLE_RA          = (  272.76       0.          0. )
+        BODY299_POLE_DEC         = (   67.16       0.          0. )
+        BODY299_PM               = (  160.20      -1.4813688   0. )
+ 
+        BODY299_LONG_AXIS        = (    0.                        )
+ 
+        \begintext
+
+
+Earth
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 report.
+ 
+     Current values:
+ 
+        \begindata 
+ 
+        BODY399_POLE_RA        = (    0.      -0.641         0. )
+        BODY399_POLE_DEC       = (   90.      -0.557         0. )
+        BODY399_PM             = (  190.147  360.9856235     0. )
+        BODY399_LONG_AXIS      = (    0.                        )
+
+        \begintext
+
+
+        Nutation precession angles for the Earth-Moon system:
+
+           The linear coefficients have been scaled up from degrees/day
+           to degrees/century, because the SPICELIB PCK reader expects
+           these units.  The original constants were:
+        
+                                    125.045D0   -0.0529921D0
+                                    250.089D0   -0.1059842D0
+                                    260.008D0   13.0120009D0
+                                    176.625D0   13.3407154D0
+                                    357.529D0    0.9856003D0
+                                    311.589D0   26.4057084D0
+                                    134.963D0   13.0649930D0
+                                    276.617D0    0.3287146D0
+                                     34.226D0    1.7484877D0
+                                     15.134D0   -0.1589763D0
+                                    119.743D0    0.0036096D0
+                                    239.961D0    0.1643573D0
+                                     25.053D0   12.9590088D0 
+
+
+        \begindata
+
+       
+        BODY3_NUT_PREC_ANGLES  = (  125.045         -1935.5364525000
+                                    250.089         -3871.0729050000
+                                    260.008        475263.3328725000  
+                                    176.625        487269.6299850000
+                                    357.529         35999.0509575000
+                                    311.589        964468.4993100000
+                                    134.963        477198.8693250000
+                                    276.617         12006.3007650000
+                                     34.226         63863.5132425000 
+                                     15.134         -5806.6093575000
+                                    119.743           131.8406400000
+                                    239.961          6003.1503825000 
+                                     25.053        473327.7964200000 )
+
+
+        \begintext
+ 
+
+     Earth north geomagnetic centered dipole:
+
+           The north dipole location is time-varying.  The values shown
+           below, taken from [8], represent a discrete sampling of the
+           north dipole location from 1945 to 2000. The terms DGRF and
+           IGRF refer to, respectively, "Definitive Geomagnetic
+           Reference Field" and "International Geomagnetic Reference
+           Field."  See references [6], [8], and [9] for details.
+
+           Coordinates are planetocentric. 
+
+             Data source    Lat      Lon
+             -----------   -----    ------
+              DGRF 1945    78.47    291.47
+              DGRF 1950    78.47    291.15
+              DGRF 1955    78.46    290.84
+              DGRF 1960    78.51    290.53
+              DGRF 1965    78.53    290.15
+              DGRF 1970    78.59    289.82
+              DGRF 1975    78.69    289.53
+              DGRF 1980    78.81    289.24 
+              DGRF 1985    78.97    289.10
+              DGRF 1990    79.13    288.89
+              IGRF 1995    79.30    288.59
+              IGRF 2000    79.54    288.43      
+
+        Original values:
+
+           Values are from [7].  Note the year of publication was 1971.
+
+           body399_mag_north_pole_lon  =  ( -69.761 )
+           body399_mag_north_pole_lat  =  (  78.565 )
+
+        Previous values:
+
+           body399_n_geomag_ctr_dipole_lon  =  ( 288.43 )
+           body399_n_geomag_ctr_dipole_lat  =  (  79.54 )
+
+
+        Current values:
+
+           Values are given for the epoch 2012.0 and were derived
+           by Nat Bachman from constants provided by [11].
+
+        \begindata
+       
+        BODY399_N_GEOMAG_CTR_DIPOLE_LON  =  ( 287.62 )
+        BODY399_N_GEOMAG_CTR_DIPOLE_LAT  =  (  80.13 )
+
+        \begintext
+
+
+
+ 
+Mars
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report.
+   
+     Current values:
+ 
+        \begindata
+ 
+        BODY499_POLE_RA          = (  317.68143   -0.1061      0.  )
+        BODY499_POLE_DEC         = (   52.88650   -0.0609      0.  )
+        BODY499_PM               = (  176.630    350.89198226  0.  )
+
+        \begintext
+ 
+        Source [5] specifies the following value for the lambda_a term
+        (BODY499_LONG_AXIS ) for Mars. This term is the POSITIVE EAST
+        LONGITUDE, measured from the prime meridian, of the meridian
+        containing the longest axis of the reference ellipsoid.
+        (CAUTION: previous values were POSITIVE WEST.)
+
+           body499_long_axis        = (  252.  )
+ 
+        We list this lambda_a value for completeness. The IAU report
+        [1] gives equal values for both equatorial radii, so the
+        lambda_a offset does not apply to the IAU model.
+ 
+        The 2003 IAU report defines M2, the second nutation precession angle,
+        by:
+ 
+                                                2
+           192.93  +  1128.4096700 d  +  8.864 T
+ 
+        We truncate the M2 series to a linear expression, because the PCK
+        software cannot handle the quadratic term.
+ 
+        Again, the linear terms are scaled by 36525.0:
+ 
+            -0.4357640000000000       -->     -15916.28010000000
+          1128.409670000000           -->   41215163.19675000
+            -1.8151000000000000E-02   -->       -662.9652750000000
+ 
+        We also introduce a fourth nutation precession angle, which
+        is the pi/2-complement of the third angle.  This angle is used
+        in computing the prime meridian location for Deimos.  See the
+        discussion of this angle below in the section containing orientation
+        constants for Deimos.
+ 
+        \begindata
+
+        BODY4_NUT_PREC_ANGLES  = (  169.51     -15916.2801
+                                    192.93   41215163.19675
+                                     53.47       -662.965275
+                                     36.53        662.965275  )
+ 
+        \begintext
+ 
+ 
+Jupiter
+ 
+     Old values:
+ 
+        The rotation rate is from the 2006 IAU report; all other
+        values are unchanged in the 2009 report.
+
+           body599_pm             = (   284.95        870.5366420      0. )
+
+                   
+     Current values:
+ 
+        The number of nutation precession angles is 15. The ninth and
+        tenth are twice the first and second, respectively. The
+        eleventh through fifteenth correspond to angles JA-JE in
+        the 2006 IAU report; angles JA-JE were not used prior to that
+        report.
+
+        \begindata
+ 
+ 
+        BODY599_POLE_RA        = (   268.056595     -0.006499       0. )
+        BODY599_POLE_DEC       = (    64.495303      0.002413       0. )
+        BODY599_PM             = (   284.95        870.5360000      0. )
+        BODY599_LONG_AXIS      = (     0.                        )
+ 
+        BODY599_NUT_PREC_RA  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000117
+                                                                0.000938
+                                                                0.001432
+                                                                0.000030
+                                                                0.002150 )
+
+        BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000050
+                                                                0.000404
+                                                                0.000617
+                                                               -0.000013
+                                                                0.000926 )
+
+        BODY599_NUT_PREC_PM  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.0
+                                                                0.0
+                                                                0.0
+                                                                0.0
+                                                                0.0  ) 
+
+
+        BODY5_NUT_PREC_ANGLES  = (    73.32      91472.9
+                                      24.62      45137.2
+                                     283.90       4850.7
+                                     355.80       1191.3
+                                     119.90        262.1
+                                     229.80         64.3
+                                     352.25       2382.6
+                                     113.35       6070.0   
+                                     146.64     182945.8
+                                      49.24      90274.4  
+                                      99.360714   4850.4046
+                                     175.895369   1191.9605
+                                     300.323162    262.5475
+                                     114.012305   6070.2476
+                                      49.511251     64.3000  )
+        \begintext
+ 
+ 
+Saturn
+ 
+     Old values:
+ 
+        Values are from the 2006 IAU report.
+
+
+        body699_pole_ra        = (    40.589    -0.036      0.  )
+        body699_pole_dec       = (    83.537    -0.004      0.  )
+        body699_pm             = (    38.90    810.7939024  0.  )
+        body699_long_axis      = (     0.                       )
+ 
+ 
+        The first seven angles given here are the angles S1 
+        through S7 from the 2000 report; the eighth and
+        ninth angles are 2*S1 and 2*S2, respectively.
+ 
+ 
+        body6_nut_prec_angles  = (  353.32   75706.7
+                                     28.72   75706.7  
+                                    177.40  -36505.5 
+                                    300.00   -7225.9 
+                                    316.45     506.2
+                                    345.20   -1016.3  
+                                     29.80     -52.1
+                                    706.64  151413.4
+                                     57.44  151413.4  )
+
+
+     Current values:
+ 
+
+        The change from the previous set of values is the
+        removal of S7. This causes BODY6_NUT_PREC_ANGLES 
+        elements that formerly corresponded to 2*S1 and 2*S1
+        to be shifted toward the start of the array.
+
+        \begindata
+
+        BODY699_POLE_RA        = (    40.589    -0.036      0.  )
+        BODY699_POLE_DEC       = (    83.537    -0.004      0.  )
+        BODY699_PM             = (    38.90    810.7939024  0.  )
+        BODY699_LONG_AXIS      = (     0.                       )
+ 
+        \begintext
+ 
+        The first six angles given here are the angles S1 
+        through S6 from the 2009 report; the seventh and
+        eigth angles are 2*S1 and 2*S2, respectively.
+ 
+ 
+        \begindata
+
+        BODY6_NUT_PREC_ANGLES  = (  353.32   75706.7
+                                     28.72   75706.7  
+                                    177.40  -36505.5 
+                                    300.00   -7225.9 
+                                    316.45     506.2
+                                    345.20   -1016.3  
+                                    706.64  151413.4
+                                     57.44  151413.4  )
+        \begintext
+ 
+ 
+Uranus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY799_POLE_RA        = (  257.311     0.         0.  )
+        BODY799_POLE_DEC       = (  -15.175     0.         0.  )
+        BODY799_PM             = (  203.81   -501.1600928  0.  )
+        BODY799_LONG_AXIS      = (    0.                       )
+ 
+        \begintext
+        
+        The first 16 angles given here are the angles U1 
+        through U16 from the 2000 report; the 17th and
+        18th angles are 2*U11 and 2*U12, respectively.
+        
+        \begindata
+         
+        BODY7_NUT_PREC_ANGLES  = (  115.75   54991.87
+                                    141.69   41887.66
+                                    135.03   29927.35
+                                     61.77   25733.59  
+                                    249.32   24471.46
+                                     43.86   22278.41 
+                                     77.66   20289.42  
+                                    157.36   16652.76  
+                                    101.81   12872.63   
+                                    138.64    8061.81
+                                    102.23   -2024.22 
+                                    316.41    2863.96  
+                                    304.01     -51.94  
+                                    308.71     -93.17 
+                                    340.82     -75.32 
+                                    259.14    -504.81 
+                                    204.46   -4048.44
+                                    632.82    5727.92     )
+                                    
+        \begintext
+ 
+ 
+ 
+Neptune
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+ 
+     Current values:
+
+        \begindata        
+ 
+           BODY899_POLE_RA        = (  299.36     0.         0. )
+           BODY899_POLE_DEC       = (   43.46     0.         0. )
+           BODY899_PM             = (  253.18   536.3128492  0. )
+           BODY899_LONG_AXIS      = (    0.                     )
+
+
+           BODY899_NUT_PREC_RA    = (  0.70 0. 0. 0. 0. 0. 0. 0. ) 
+           BODY899_NUT_PREC_DEC   = ( -0.51 0. 0. 0. 0. 0. 0. 0. )
+           BODY899_NUT_PREC_PM    = ( -0.48 0. 0. 0. 0. 0. 0. 0. )
+
+        \begintext
+ 
+           The 2000 report defines the nutation precession angles
+ 
+              N, N1, N2, ... , N7
+ 
+           and also uses the multiples of N1 and N7
+ 
+              2*N1
+ 
+           and
+ 
+              2*N7, 3*N7, ..., 9*N7
+ 
+           In this file, we treat the angles and their multiples as
+           separate angles.  In the kernel variable
+ 
+              BODY8_NUT_PREC_ANGLES
+ 
+           the order of the angles is
+ 
+              N, N1, N2, ... , N7, 2*N1, 2*N7, 3*N7, ..., 9*N7
+ 
+           Each angle is defined by a linear polynomial, so two
+           consecutive array elements are allocated for each
+           angle.  The first term of each pair is the constant term,
+           the second is the linear term.
+ 
+        \begindata 
+
+              BODY8_NUT_PREC_ANGLES = (   357.85         52.316
+                                          323.92      62606.6
+                                          220.51      55064.2 
+                                          354.27      46564.5
+                                           75.31      26109.4 
+                                           35.36      14325.4
+                                          142.61       2824.6  
+                                          177.85         52.316 
+                                          647.840    125213.200
+                                          355.700       104.632
+                                          533.550       156.948
+                                          711.400       209.264
+                                          889.250       261.580
+                                         1067.100       313.896
+                                         1244.950       366.212
+                                         1422.800       418.528
+                                         1600.650       470.844   )
+                                         
+        \begintext
+ 
+ 
+ 
+
+Orientation Constants for the Dwarf Planet Pluto
+--------------------------------------------------------
+ 
+Pluto
+ 
+     Old values:
+ 
+        Values are from the 2006 IAU report. 
+
+        body999_pole_ra        = (  312.993   0.          0. )
+        body999_pole_dec       = (    6.163   0.          0. )
+        body999_pm             = (  237.305  -56.3625225  0. )
+        body999_long_axis      = (    0.                     )
+
+
+     Current values:
+
+        Due to the new definition of planetocentric coordinates
+        for small bodies, and to the reclassification of Pluto
+        as a dwarf planet, Pluto's north pole direction has been
+        inverted. 
+
+        The PM constant W0 is from [2]. 
+
+        \begindata
+ 
+        BODY999_POLE_RA        = (  132.993   0.          0. )
+        BODY999_POLE_DEC       = (   -6.163   0.          0. )
+        BODY999_PM             = (  302.695   56.3625225  0. )
+        BODY999_LONG_AXIS      = (    0.                     )
+
+        \begintext
+ 
+ 
+ 
+ 
+Orientation constants for the satellites
+--------------------------------------------------------
+ 
+ 
+Satellites of Earth
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+ 
+     New values:
+ 
+        \begindata
+ 
+
+        BODY301_POLE_RA      = (  269.9949        0.0031        0.      )
+        BODY301_POLE_DEC     = (   66.5392        0.0130        0.      )
+        BODY301_PM           = (   38.3213       13.17635815   -1.4D-12 )
+        BODY301_LONG_AXIS    = (    0.                                  )
+   
+        BODY301_NUT_PREC_RA  = (   -3.8787   -0.1204   0.0700   -0.0172
+                                    0.0       0.0072   0.0       0.0
+                                    0.0      -0.0052   0.0       0.0
+                                    0.0043                              )
+        
+        BODY301_NUT_PREC_DEC = (   1.5419     0.0239  -0.0278    0.0068
+                                   0.0       -0.0029   0.0009    0.0
+                                   0.0        0.0008   0.0       0.0     
+                                  -0.0009                               )
+        
+        BODY301_NUT_PREC_PM  = (   3.5610     0.1208  -0.0642    0.0158
+                                   0.0252    -0.0066  -0.0047   -0.0046
+                                   0.0028     0.0052   0.0040    0.0019
+                                  -0.0044                               )
+        \begintext
+ 
+
+ 
+Satellites of Mars
+ 
+ 
+     Phobos
+ 
+          Old values:
+ 
+             Values are unchanged in the 2009 IAU report.
+ 
+
+          Current values:
+ 
+            The quadratic prime meridian term is scaled by 1/36525**2:
+ 
+               8.864000000000000   --->   6.6443009930565219E-09
+ 
+        \begindata
+ 
+          BODY401_POLE_RA  = ( 317.68    -0.108     0.                     )
+          BODY401_POLE_DEC = (  52.90    -0.061     0.                     )
+          BODY401_PM       = (  35.06  1128.8445850 6.6443009930565219E-09 )
+                                       
+          BODY401_LONG_AXIS     = (    0.   )
+ 
+          BODY401_NUT_PREC_RA   = (   1.79    0.    0.   0. )
+          BODY401_NUT_PREC_DEC  = (  -1.08    0.    0.   0. )
+          BODY401_NUT_PREC_PM   = (  -1.42   -0.78  0.   0. )
+
+
+        \begintext
+ 
+ 
+     Deimos
+ 
+        Old values:
+ 
+           Values are unchanged in the 2009 IAU report.
+  
+        New values:
+ 
+           The Deimos prime meridian expression is:
+ 
+ 
+                                                     2
+              W = 79.41  +  285.1618970 d  -  0.520 T  -  2.58 sin M
+                                                                    3
+ 
+                                                       +  0.19 cos M .
+                                                                    3
+ 
+ 
+           At the present time, the PCK kernel software (the routine
+           BODEUL in particular) cannot handle the cosine term directly,
+           but we can represent it as
+ 
+              0.19 sin M
+                        4
+ 
+           where
+ 
+              M   =  90.D0 - M
+               4              3
+ 
+           Therefore, the nutation precession angle assignments for Phobos
+           and Deimos contain four coefficients rather than three.
+ 
+           The quadratic prime meridian term is scaled by 1/36525**2:
+ 
+              -0.5200000000000000  --->   -3.8978300049519307E-10
+ 
+        \begindata
+ 
+           BODY402_POLE_RA       = (  316.65     -0.108       0.           )
+           BODY402_POLE_DEC      = (   53.52     -0.061       0.           )
+           BODY402_PM            = (   79.41    285.1618970  -3.897830D-10 )
+           BODY402_LONG_AXIS     = (    0.                                 )
+ 
+           BODY402_NUT_PREC_RA   = (    0.   0.   2.98    0.   )
+           BODY402_NUT_PREC_DEC  = (    0.   0.  -1.78    0.   )
+           BODY402_NUT_PREC_PM   = (    0.   0.  -2.58    0.19 )
+
+        \begintext
+ 
+ 
+ 
+ 
+Satellites of Jupiter
+ 
+ 
+     Io
+ 
+          Old values:
+ 
+             Values are unchanged in the 2009 IAU report.
+ 
+          Current values:
+         
+        \begindata
+ 
+        BODY501_POLE_RA       = (  268.05          -0.009      0. )
+        BODY501_POLE_DEC      = (   64.50           0.003      0. )
+        BODY501_PM            = (  200.39         203.4889538  0. )
+        BODY501_LONG_AXIS     = (    0.                           )
+ 
+        BODY501_NUT_PREC_RA   = (    0.   0.     0.094    0.024   )
+        BODY501_NUT_PREC_DEC  = (    0.   0.     0.040    0.011   )
+        BODY501_NUT_PREC_PM   = (    0.   0.    -0.085   -0.022   )
+
+        \begintext
+ 
+ 
+ 
+     Europa
+ 
+ 
+        Old values:
+
+           Values are unchanged in the 2009 IAU report.      
+
+
+        Current values:
+ 
+        \begindata 
+ 
+        BODY502_POLE_RA       = (  268.08          -0.009      0.   )
+        BODY502_POLE_DEC      = (   64.51           0.003      0.   )
+        BODY502_PM            = (   36.022        101.3747235  0.   )
+        BODY502_LONG_AXIS     = (    0.                             )
+ 
+        BODY502_NUT_PREC_RA   = ( 0. 0. 0.   1.086   0.060   0.015   0.009 )
+        BODY502_NUT_PREC_DEC  = ( 0. 0. 0.   0.468   0.026   0.007   0.002 )
+        BODY502_NUT_PREC_PM   = ( 0. 0. 0.  -0.980  -0.054  -0.014  -0.008 )
+ 
+        \begintext
+ 
+ 
+     Ganymede
+ 
+        Old values:
+ 
+             Values are unchanged in the 2009 IAU report.
+
+        Current values:
+        
+        \begindata
+    
+        BODY503_POLE_RA       = (  268.20         -0.009       0.  )
+        BODY503_POLE_DEC      = (   64.57          0.003       0.  )
+        BODY503_PM            = (   44.064        50.3176081   0.  )
+        BODY503_LONG_AXIS     = (    0.                            )
+
+        BODY503_NUT_PREC_RA   = ( 0. 0. 0.  -0.037   0.431   0.091   )
+        BODY503_NUT_PREC_DEC  = ( 0. 0. 0.  -0.016   0.186   0.039   )
+        BODY503_NUT_PREC_PM   = ( 0. 0. 0.   0.033  -0.389  -0.082   )
+ 
+        \begintext
+ 
+ 
+     Callisto
+ 
+        Old values:
+
+             Values are unchanged in the 2009 IAU report.
+                
+        Current values:
+        
+        
+        \begindata
+  
+        BODY504_POLE_RA       = (   268.72    -0.009       0.  )
+        BODY504_POLE_DEC      = (    64.83     0.003       0.  )
+        BODY504_PM            = (   259.51    21.5710715   0.  )
+        BODY504_LONG_AXIS     = (     0.                       )
+ 
+        BODY504_NUT_PREC_RA   = ( 0. 0. 0. 0.  -0.068   0.590  0.   0.010 )
+        BODY504_NUT_PREC_DEC  = ( 0. 0. 0. 0.  -0.029   0.254  0.  -0.004 )
+        BODY504_NUT_PREC_PM   = ( 0. 0. 0. 0.   0.061  -0.533  0.  -0.009 )
+ 
+        \begintext
+ 
+ 
+     Amalthea
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report.        
+        
+        Current values:
+         
+        \begindata
+ 
+        BODY505_POLE_RA       = (   268.05    -0.009      0.  )
+        BODY505_POLE_DEC      = (    64.49     0.003      0.  )
+        BODY505_PM            = (   231.67   722.6314560  0.  )
+        BODY505_LONG_AXIS     = (     0.                      )
+ 
+        BODY505_NUT_PREC_RA  = ( -0.84  0. 0. 0. 0. 0. 0. 0.   0.01  0. )
+        BODY505_NUT_PREC_DEC = ( -0.36  0. 0. 0. 0. 0. 0. 0.   0.    0. )
+        BODY505_NUT_PREC_PM  = (  0.76  0. 0. 0. 0. 0. 0. 0.  -0.01  0. )
+ 
+        \begintext
+ 
+ 
+     Thebe
+ 
+ 
+        Old values:
+                
+           Values are unchanged in the 2009 IAU report.                
+          
+        Current values:
+        
+        \begindata
+ 
+        BODY514_POLE_RA       = (  268.05     -0.009       0.  )
+        BODY514_POLE_DEC      = (   64.49      0.003       0.  )
+        BODY514_PM            = (    8.56    533.7004100   0.  )
+        BODY514_LONG_AXIS     = (    0.                        )
+ 
+        BODY514_NUT_PREC_RA  = ( 0.  -2.11  0. 0. 0. 0. 0. 0. 0.  0.04 )
+        BODY514_NUT_PREC_DEC = ( 0.  -0.91  0. 0. 0. 0. 0. 0. 0.  0.01 )
+        BODY514_NUT_PREC_PM  = ( 0.   1.91  0. 0. 0. 0. 0. 0. 0. -0.04 )
+ 
+        \begintext
+ 
+ 
+     Adrastea
+ 
+        Old values:
+                
+           Values are unchanged in the 2009 IAU report.                
+        
+        Current values:
+        
+        \begindata 
+ 
+        BODY515_POLE_RA       = (  268.05     -0.009       0.  )
+        BODY515_POLE_DEC      = (   64.49      0.003       0.  )
+        BODY515_PM            = (   33.29   1206.9986602   0.  )
+        BODY515_LONG_AXIS     = (    0.                        )
+
+        \begintext
+ 
+ 
+     Metis
+  
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report.  
+              
+        Current values:
+           
+        \begindata
+
+        BODY516_POLE_RA       = (  268.05     -0.009       0.  )
+        BODY516_POLE_DEC      = (   64.49      0.003       0.  )
+        BODY516_PM            = (  346.09   1221.2547301   0.  )
+        BODY516_LONG_AXIS     = (    0.                        )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Saturn
+      
+     
+     Mimas
+ 
+        Old values:
+        
+           Values are from the 2006 IAU report.
+               
+           body601_pole_ra       = (   40.66     -0.036      0.  )
+           body601_pole_dec      = (   83.52     -0.004      0.  )
+           body601_pm            = (  337.46    381.9945550  0.  )
+           body601_long_axis     = (     0.                      )
+ 
+           body601_nut_prec_ra   = ( 0. 0.   13.56  0.    0.    0. 0. 0. 0. )
+           body601_nut_prec_dec  = ( 0. 0.   -1.53  0.    0.    0. 0. 0. 0. )
+           body601_nut_prec_pm   = ( 0. 0.  -13.48  0.  -44.85  0. 0. 0. 0. )
+
+
+        Current values:
+
+        \begindata
+  
+           BODY601_POLE_RA       = (   40.66     -0.036      0.  )
+           BODY601_POLE_DEC      = (   83.52     -0.004      0.  )
+           BODY601_PM            = (  333.46    381.9945550  0.  )
+           BODY601_LONG_AXIS     = (     0.                      )
+ 
+           BODY601_NUT_PREC_RA   = ( 0. 0.   13.56  0.    0.    0. 0. 0.  )
+           BODY601_NUT_PREC_DEC  = ( 0. 0.   -1.53  0.    0.    0. 0. 0.  )
+           BODY601_NUT_PREC_PM   = ( 0. 0.  -13.48  0.  -44.85  0. 0. 0.  )
+
+        \begintext
+ 
+ 
+     Enceladus
+ 
+ 
+        Old values:
+        
+           Values are from the 2006 IAU report.  
+               
+           body602_pole_ra       = (   40.66    -0.036       0. )
+           body602_pole_dec      = (   83.52    -0.004       0. )
+           body602_pm            = (    2.82   262.7318996   0. )
+           body602_long_axis     = (    0.                      )
+
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY602_POLE_RA       = (   40.66    -0.036       0. )
+           BODY602_POLE_DEC      = (   83.52    -0.004       0. )
+           BODY602_PM            = (    6.32   262.7318996   0. )
+           BODY602_LONG_AXIS     = (    0.                      )
+
+        \begintext
+ 
+ 
+ 
+     Tethys
+ 
+ 
+        Old values:
+        
+           Values are from the 2006 IAU report. 
+ 
+           body603_pole_ra       = (   40.66    -0.036       0. )
+           body603_pole_dec      = (   83.52    -0.004       0. )
+           body603_pm            = (   10.45   190.6979085   0. )
+           body603_long_axis     = (    0.                      )
+ 
+           body603_nut_prec_ra   = ( 0. 0. 0.   9.66   0.    0.  0.  0.  0. )
+           body603_nut_prec_dec  = ( 0. 0. 0.  -1.09   0.    0.  0.  0.  0. )
+           body603_nut_prec_pm   = ( 0. 0. 0.  -9.60   2.23  0.  0.  0.  0. )
+
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY603_POLE_RA       = (   40.66    -0.036       0. )
+           BODY603_POLE_DEC      = (   83.52    -0.004       0. )
+           BODY603_PM            = (    8.95   190.6979085   0. )
+           BODY603_LONG_AXIS     = (    0.                      )
+ 
+           BODY603_NUT_PREC_RA   = ( 0. 0. 0.   9.66   0.    0.  0.  0. )
+           BODY603_NUT_PREC_DEC  = ( 0. 0. 0.  -1.09   0.    0.  0.  0. )
+           BODY603_NUT_PREC_PM   = ( 0. 0. 0.  -9.60   2.23  0.  0.  0. )
+
+        \begintext
+ 
+ 
+     Dione
+ 
+ 
+        Old values:
+        
+           Values are from the 2006 IAU report. 
+ 
+           body604_pole_ra       = (  40.66      -0.036      0.  )
+           body604_pole_dec      = (  83.52      -0.004      0.  )
+           body604_pm            = (  357.00    131.5349316  0.  )
+           body604_long_axis     = (    0.                       )
+
+
+        Current values:
+ 
+        \begindata
+   
+           BODY604_POLE_RA       = (  40.66      -0.036      0.  )
+           BODY604_POLE_DEC      = (  83.52      -0.004      0.  )
+           BODY604_PM            = (  357.6     131.5349316  0.  )
+           BODY604_LONG_AXIS     = (    0.                       )
+
+        \begintext
+ 
+ 
+ 
+     Rhea
+     
+ 
+        Old values:
+        
+           Values are from the 2009 IAU report.
+
+           body605_pole_ra       = (   40.38   -0.036       0. )
+           body605_pole_dec      = (   83.55   -0.004       0. )
+           body605_pm            = (  235.16   79.6900478   0. )
+           body605_long_axis     = (    0.                     )
+ 
+           body605_nut_prec_ra   = ( 0. 0. 0. 0. 0.   3.10   0. 0. 0. )
+           body605_nut_prec_dec  = ( 0. 0. 0. 0. 0.  -0.35   0. 0. 0. )
+           body605_nut_prec_pm   = ( 0. 0. 0. 0. 0.  -3.08   0. 0. 0. )
+
+ 
+        Current values:
+ 
+           Data values are unchanged in the 2009 IAU report. However
+           the kernel variable contents have changed due to removal of
+           the angle S7.
+
+        \begindata
+   
+           BODY605_POLE_RA       = (   40.38   -0.036       0. )
+           BODY605_POLE_DEC      = (   83.55   -0.004       0. )
+           BODY605_PM            = (  235.16   79.6900478   0. )
+           BODY605_LONG_AXIS     = (    0.                     )
+ 
+           BODY605_NUT_PREC_RA   = ( 0. 0. 0. 0. 0.   3.10   0. 0. )
+           BODY605_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0.  -0.35   0. 0. )
+           BODY605_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  -3.08   0. 0. )
+ 
+        \begintext
+ 
+ 
+ 
+     Titan
+ 
+ 
+        Old values:
+        
+           Values are from the 2006 IAU report. 
+
+           BODY606_POLE_RA       = (    36.41   -0.036      0. )
+           BODY606_POLE_DEC      = (    83.94   -0.004      0. )
+           BODY606_PM            = (   189.64   22.5769768  0. )
+           BODY606_LONG_AXIS     = (     0.                    )
+ 
+           BODY606_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 0.  2.66  0. 0 )
+           BODY606_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 0. -0.30  0. 0 )
+           BODY606_NUT_PREC_PM   = ( 0. 0. 0. 0. 0. 0. -2.64  0. 0 )
+
+
+        Current values:
+
+              Note removal of dependence on the nutation precession
+              angles.
+ 
+        \begindata
+ 
+           BODY606_POLE_RA       = (    39.4827    0.         0. )
+           BODY606_POLE_DEC      = (    83.4279    0.         0. )
+           BODY606_PM            = (   186.5855   22.5769768  0. )
+           BODY606_LONG_AXIS     = (     0.                      )
+ 
+           BODY606_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 0. 0. 0 )
+           BODY606_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 0. 0. 0 )
+           BODY606_NUT_PREC_PM   = ( 0. 0. 0. 0. 0. 0. 0. 0 )
+
+        \begintext
+ 
+ 
+ 
+     Hyperion
+ 
+         The IAU report does not give an orientation model for Hyperion.
+         Hyperion's rotation is in chaotic and is not predictable for
+         long periods.
+
+ 
+     Iapetus
+ 
+ 
+        Old values:
+        
+           Values are from the 2006 IAU report. 
+
+           body608_pole_ra       = (   318.16  -3.949      0.  )
+           body608_pole_dec      = (    75.03  -1.143      0.  )
+           body608_pm            = (   350.20   4.5379572  0.  )
+           body608_long_axis     = (     0.                    )
+
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY608_POLE_RA       = (   318.16  -3.949      0.  )
+           BODY608_POLE_DEC      = (    75.03  -1.143      0.  )
+           BODY608_PM            = (   355.2    4.5379572  0.  )
+           BODY608_LONG_AXIS     = (     0.                    )
+
+        \begintext
+ 
+ 
+ 
+     Phoebe
+ 
+
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+  
+        Current values:
+ 
+        \begindata 
+  
+           BODY609_POLE_RA       = ( 356.90       0.         0.  )
+           BODY609_POLE_DEC      = (  77.80       0.         0.  )
+           BODY609_PM            = ( 178.58     931.639      0.  )
+           BODY609_LONG_AXIS     = (    0.                       )
+
+        \begintext
+ 
+ 
+     Janus
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+
+        Current values:
+
+           Data values are unchanged in the 2009 IAU report. However
+           the kernel variable contents have changed due to removal of
+           the angle S7.
+ 
+        \begindata
+
+           BODY610_POLE_RA       = (  40.58    -0.036       0. )
+           BODY610_POLE_DEC      = (  83.52    -0.004       0. )
+           BODY610_PM            = (  58.83   518.2359876   0. )
+           BODY610_LONG_AXIS     = (   0.                      )
+ 
+           BODY610_NUT_PREC_RA   = ( 0. -1.623  0. 0. 0. 0. 0.  0.023 )
+           BODY610_NUT_PREC_DEC  = ( 0. -0.183  0. 0. 0. 0. 0.  0.001 )
+           BODY610_NUT_PREC_PM   = ( 0.  1.613  0. 0. 0. 0. 0. -0.023 )
+ 
+        \begintext
+ 
+ 
+ 
+     Epimetheus
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+         
+        Current values:
+ 
+           Data values are unchanged in the 2009 IAU report. However
+           the kernel variable contents have changed due to removal of
+           the angle S7.
+
+        \begindata 
+  
+           BODY611_POLE_RA       = (  40.58    -0.036        0. )
+           BODY611_POLE_DEC      = (  83.52    -0.004        0. )
+           BODY611_PM            = ( 293.87   518.4907239    0. )
+           BODY611_LONG_AXIS     = (   0.                       )
+ 
+           BODY611_NUT_PREC_RA   = ( -3.153   0. 0. 0. 0. 0.   0.086  0. )
+           BODY611_NUT_PREC_DEC  = ( -0.356   0. 0. 0. 0. 0.   0.005  0. )
+           BODY611_NUT_PREC_PM   = (  3.133   0. 0. 0. 0. 0.  -0.086  0. )
+
+        \begintext
+ 
+ 
+ 
+     Helene
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+ 
+           BODY612_POLE_RA       = (  40.85     -0.036        0. )
+           BODY612_POLE_DEC      = (  83.34     -0.004        0. )
+           BODY612_PM            = ( 245.12    131.6174056    0. )
+           BODY612_LONG_AXIS     = (   0.                        )
+
+        \begintext
+ 
+ 
+ 
+     Telesto
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+ 
+           BODY613_POLE_RA       = ( 50.51    -0.036      0.  )
+           BODY613_POLE_DEC      = ( 84.06    -0.004      0.  )
+           BODY613_PM            = ( 56.88   190.6979332  0.  )
+           BODY613_LONG_AXIS     = (  0.                      )
+
+        \begintext
+
+ 
+ 
+     Calypso
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY614_POLE_RA       = (   36.41    -0.036        0.  )
+           BODY614_POLE_DEC      = (   85.04    -0.004        0.  )
+           BODY614_PM            = (  153.51   190.6742373    0.  )
+           BODY614_LONG_AXIS     = (    0.                        )
+ 
+        \begintext
+ 
+ 
+ 
+     Atlas
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY615_POLE_RA       = (   40.58     -0.036      0. )
+           BODY615_POLE_DEC      = (   83.53     -0.004      0. )  
+           BODY615_PM            = (  137.88    598.3060000  0. )
+           BODY615_LONG_AXIS     = (    0.                      )
+
+        \begintext
+ 
+ 
+ 
+     Prometheus
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY616_POLE_RA       = (  40.58      -0.036    )
+           BODY616_POLE_DEC      = (  83.53      -0.004    )
+           BODY616_PM            = ( 296.14     587.289000 )
+           BODY616_LONG_AXIS     = (   0.                  )
+ 
+        \begintext
+ 
+ 
+ 
+     Pandora
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY617_POLE_RA       = (   40.58     -0.036      0.  )
+           BODY617_POLE_DEC      = (   83.53     -0.004      0.  )
+           BODY617_PM            = (  162.92    572.7891000  0.  )
+           BODY617_LONG_AXIS     = (     0.                      )
+ 
+        \begintext
+ 
+ 
+ 
+     Pan
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY618_POLE_RA       = (   40.6     -0.036       0. )
+           BODY618_POLE_DEC      = (   83.5     -0.004       0. )
+           BODY618_PM            = (   48.8    626.0440000   0. )
+           BODY618_LONG_AXIS     = (    0.                      )
+
+        \begintext
+ 
+ 
+ 
+ 
+ 
+Satellites of Uranus
+ 
+  
+ 
+     Ariel
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+ 
+        Current values:
+
+        \begindata 
+
+           BODY701_POLE_RA       = ( 257.43     0.          0. )
+           BODY701_POLE_DEC      = ( -15.10     0.          0. )
+           BODY701_PM            = ( 156.22  -142.8356681   0. )
+           BODY701_LONG_AXIS     = (   0.                      )
+ 
+           BODY701_NUT_PREC_RA   = (  0. 0. 0. 0. 0.
+                                      0. 0. 0. 0. 0.  0.    0.    0.29 )
+ 
+           BODY701_NUT_PREC_DEC  = (  0. 0. 0. 0. 0.
+                                      0. 0. 0. 0. 0.  0.    0.    0.28 )
+ 
+           BODY701_NUT_PREC_PM   = (  0. 0. 0. 0. 0.
+                                      0. 0. 0. 0. 0.  0.   0.05   0.08 )
+        \begintext
+ 
+ 
+ 
+     Umbriel
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+ 
+           BODY702_POLE_RA       = (  257.43     0.          0. )
+           BODY702_POLE_DEC      = (  -15.10     0.          0. )
+           BODY702_PM            = (  108.05   -86.8688923   0. )
+           BODY702_LONG_AXIS     = (    0.                      )
+ 
+           BODY702_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0.   0.    0.   0.21 )
+ 
+           BODY702_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0.   0.    0.   0.20 )
+ 
+           BODY702_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  
+                                     0. 0. 0. 0. 0.   0.  -0.09  0.   0.06 )
+
+        \begintext
+ 
+ 
+ 
+     Titania
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY703_POLE_RA       = (  257.43    0.          0. )
+           BODY703_POLE_DEC      = (  -15.10    0.          0. )
+           BODY703_PM            = (   77.74  -41.3514316   0. )
+           BODY703_LONG_AXIS     = (    0.                     )
+ 
+           BODY703_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0. 0. 0. 0.   0.29 )
+ 
+           BODY703_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0. 0. 0. 0.   0.28 )
+ 
+           BODY703_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  
+                                     0. 0. 0. 0. 0.   0. 0. 0. 0.   0.08 )
+        \begintext
+ 
+ 
+ 
+     Oberon
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY704_POLE_RA       = (  257.43    0.          0. )
+           BODY704_POLE_DEC      = (  -15.10    0.          0. )
+           BODY704_PM            = (    6.77  -26.7394932   0. )
+           BODY704_LONG_AXIS     = (    0.                     )
+ 
+ 
+           BODY704_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0.16 )
+ 
+           BODY704_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0.16 )
+ 
+           BODY704_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  
+                                     0. 0. 0. 0. 0.  
+                                     0. 0. 0. 0. 0.   0.04 )
+        \begintext
+ 
+ 
+ 
+     Miranda
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY705_POLE_RA      = (  257.43     0.         0. )
+           BODY705_POLE_DEC     = (  -15.08     0.         0. )
+           BODY705_PM           = (   30.70  -254.6906892  0. )
+           BODY705_LONG_AXIS    = (    0.                     )
+ 
+           BODY705_NUT_PREC_RA  = ( 0.     0.     0.    0.    0.  
+                                    0.     0.     0.    0.    0. 
+                                    4.41   0.     0.    0.    0. 
+                                    0.    -0.04   0.             )
+ 
+           BODY705_NUT_PREC_DEC = ( 0.     0.     0.    0.    0.  
+                                    0.     0.     0.    0.    0. 
+                                    4.25   0.     0.    0.    0. 
+                                    0.    -0.02   0.             )
+ 
+           BODY705_NUT_PREC_PM  = ( 0.     0.     0.    0.    0.  
+                                    0.     0.     0.    0.    0. 
+                                    1.15  -1.27   0.    0.    0.  
+                                    0.    -0.09   0.15           )
+        \begintext
+ 
+ 
+ 
+     Cordelia
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY706_POLE_RA      = (   257.31      0.         0.  )
+           BODY706_POLE_DEC     = (   -15.18      0.         0.  )
+           BODY706_PM           = (   127.69  -1074.5205730  0.  )
+           BODY706_LONG_AXIS    = (     0.                       )
+ 
+           BODY706_NUT_PREC_RA  = (   -0.15    0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )
+
+           BODY706_NUT_PREC_DEC = (    0.14    0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )  
+
+           BODY706_NUT_PREC_PM  = (   -0.04    0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             ) 
+ 
+        \begintext
+ 
+ 
+
+     Ophelia
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+   
+           BODY707_POLE_RA      = (  257.31     0.         0. )
+           BODY707_POLE_DEC     = (  -15.18     0.         0. )
+           BODY707_PM           = (  130.35  -956.4068150  0. )
+           BODY707_LONG_AXIS    = (    0.                     )
+ 
+           BODY707_NUT_PREC_RA  = (    0.     -0.09   0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )
+
+           BODY707_NUT_PREC_DEC = (    0.      0.09   0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )
+
+           BODY707_NUT_PREC_PM  = (    0.     -0.03   0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )
+ 
+        \begintext
+ 
+ 
+ 
+     Bianca
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY708_POLE_RA      = (  257.31     0.         0.  )
+           BODY708_POLE_DEC     = (  -15.18     0.         0.  )
+           BODY708_PM           = (  105.46  -828.3914760  0.  )
+           BODY708_LONG_AXIS    = (    0.                      )
+ 
+           BODY708_NUT_PREC_RA  = (    0.      0.    -0.16    0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.               )
+
+           BODY708_NUT_PREC_DEC = (    0.      0.     0.16    0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.               )
+
+           BODY708_NUT_PREC_PM  = (    0.      0.    -0.04    0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.               )
+
+        \begintext
+ 
+ 
+ 
+     Cressida
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+ 
+           BODY709_POLE_RA      = (  257.31      0.          0.  )
+           BODY709_POLE_DEC     = (  -15.18      0.          0.  )
+           BODY709_PM           = (   59.16   -776.5816320   0.  )
+           BODY709_LONG_AXIS    = (    0.                        )
+ 
+
+           BODY709_NUT_PREC_RA  = (    0.      0.     0.     -0.04   0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.                )
+
+
+           BODY709_NUT_PREC_DEC = (    0.      0.     0.      0.04   0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.                )
+
+
+           BODY709_NUT_PREC_PM  = (    0.      0.     0.     -0.01   0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.                )
+
+
+        \begintext
+ 
+ 
+ 
+     Desdemona
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+  
+           BODY710_POLE_RA      = ( 257.31      0.           0.  )
+           BODY710_POLE_DEC     = ( -15.18      0.           0.  )
+           BODY710_PM           = (  95.08   -760.0531690    0.  )
+           BODY710_LONG_AXIS    = (   0.                         )
+ 
+           BODY710_NUT_PREC_RA  = (   0.      0.     0.      0.    -0.17 
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+
+           BODY710_NUT_PREC_DEC = (   0.      0.     0.      0.     0.16 
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+
+           BODY710_NUT_PREC_PM  = (   0.      0.     0.      0.    -0.04  
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                 )
+
+        \begintext
+ 
+ 
+ 
+     Juliet
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY711_POLE_RA      = (  257.31     0.           0.   )
+           BODY711_POLE_DEC     = (  -15.18     0.           0.   )
+           BODY711_PM           = (  302.56  -730.1253660    0.   )
+           BODY711_LONG_AXIS    = (    0.                         )
+ 
+           BODY711_NUT_PREC_RA  = (   0.      0.     0.      0.     0.  
+                                     -0.06    0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                 )
+ 
+           BODY711_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.06    0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                 )
+  
+           BODY711_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                     -0.02    0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                 )
+ 
+        \begintext
+ 
+ 
+ 
+     Portia
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+    
+           BODY712_POLE_RA      = (  257.31      0.           0.   )
+           BODY712_POLE_DEC     = (  -15.18      0.           0.   )
+           BODY712_PM           = (   25.03   -701.4865870    0.   )
+           BODY712_LONG_AXIS    = (    0.                          )
+ 
+           BODY712_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
+                                      0.     -0.09   0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                )
+
+           BODY712_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.      0.09   0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.               )
+
+           BODY712_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                      0.     -0.02   0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.               )
+
+        \begintext
+ 
+ 
+ 
+     Rosalind
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+   
+           BODY713_POLE_RA      = ( 257.31      0.          0.  )
+           BODY713_POLE_DEC     = ( -15.18      0.          0.  )
+           BODY713_PM           = ( 314.90   -644.6311260   0.  )
+           BODY713_LONG_AXIS    = (   0.                        )
+ 
+           BODY713_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
+                                      0.      0.    -0.29    0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.               )
+
+           BODY713_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.28    0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.              )
+
+           BODY713_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                      0.      0.    -0.08    0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.              )
+ 
+        \begintext
+ 
+ 
+ 
+     Belinda
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+ 
+           BODY714_POLE_RA      = (   257.31      0.         0. )
+           BODY714_POLE_DEC     = (   -15.18      0.         0. )
+           BODY714_PM           = (   297.46   -577.3628170  0. )
+           BODY714_LONG_AXIS    = (     0.                      )
+ 
+           BODY714_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.     -0.03   0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                )
+
+           BODY714_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.      0.03   0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                )
+
+           BODY714_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.     -0.01   0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                )
+        \begintext
+ 
+ 
+ 
+     Puck
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY715_POLE_RA      = (  257.31      0.         0.  )
+           BODY715_POLE_DEC     = (  -15.18      0.         0.  )
+           BODY715_PM           = (   91.24   -472.5450690  0.  )
+           BODY715_LONG_AXIS    = (    0.                       )
+ 
+           BODY715_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.      0.    -0.33 
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+
+           BODY715_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.      0.     0.31
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+
+           BODY715_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.      0.    -0.09
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+  
+        \begintext
+ 
+ 
+ 
+ 
+Satellites of Neptune
+ 
+ 
+     Triton
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+ 
+        Current values:
+ 
+        \begindata
+
+           BODY801_POLE_RA       = ( 299.36     0.         0.  )
+           BODY801_POLE_DEC      = (  41.17     0.         0.  )
+           BODY801_PM            = ( 296.53   -61.2572637  0.  )
+           BODY801_LONG_AXIS     = (   0.                      )
+ 
+ 
+           BODY801_NUT_PREC_RA   = (  0.      0.      0.      0.  
+                                      0.      0.      0.    -32.35    
+                                      0.     -6.28   -2.08   -0.74       
+                                     -0.28   -0.11   -0.07   -0.02    
+                                     -0.01                         )
+ 
+ 
+           BODY801_NUT_PREC_DEC  = (  0.      0.      0.      0.  
+                                      0.      0.      0.     22.55    
+                                      0.      2.10    0.55    0.16   
+                                      0.05    0.02    0.01    0.
+                                      0.                           )
+ 
+ 
+           BODY801_NUT_PREC_PM   = (  0.      0.      0.      0.  
+                                      0.      0.      0.     22.25   
+                                      0.      6.73    2.05    0.74   
+                                      0.28    0.11    0.05    0.02
+                                      0.01                         )
+  
+        \begintext
+ 
+ 
+ 
+ 
+     Nereid
+ 
+        Old values:
+ 
+           Values are from the 1988 IAU report [10].  Note that this 
+           rotation model pre-dated the 1989 Voyager 2 Neptune
+           encounter.
+
+ 
+           body802_pole_ra       = (    273.48    0.        0.  )
+           body802_pole_dec      = (     67.22    0.        0.  )
+           body802_pm            = (    237.22    0.9996465 0.  )
+           body802_long_axis     = (      0.                    )
+ 
+ 
+           The report seems to have a typo:  in the nut_prec_ra expression,
+           where the report gives  -0.51 sin 3N3, we use -0.51 3N2.
+ 
+           body802_nut_prec_ra   = (  0.    -17.81
+                                      0.      0.     0.      0.
+                                      0.      0.     0.
+                                      2.56   -0.51   0.11   -0.03  )
+ 
+           body802_nut_prec_dec  = (  0.     -6.67
+                                      0.      0.     0.      0.
+                                      0.      0.     0.
+                                      0.47   -0.07   0.01          )
+ 
+           body802_nut_prec_pm   = (  0.     16.48
+                                      0.      0.     0.      0.
+                                      0.      0.     0.
+                                     -2.57    0.51 -0.11    0.02  )
+ 
+ 
+ 
+        Current values:
+ 
+           The 2009 report [1] states that values for Nereid are not
+           given because Nereid is not in synchronous rotation with Neptune
+           (notes following table 2).
+ 
+ 
+ 
+     Naiad
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+ 
+        \begindata
+  
+           BODY803_POLE_RA       = (  299.36      0.          0.  )
+           BODY803_POLE_DEC      = (   43.36      0.          0.  )
+           BODY803_PM            = (  254.06  +1222.8441209   0.  )
+           BODY803_LONG_AXIS     = (    0.                        )
+ 
+ 
+           BODY803_NUT_PREC_RA   = (    0.70     -6.49     0.      0.
+                                        0.        0.       0.      0.
+                                        0.25      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+ 
+           BODY803_NUT_PREC_DEC  = (   -0.51     -4.75     0.      0.
+                                        0.        0.       0.      0.
+                                        0.09      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+ 
+           BODY803_NUT_PREC_PM   = (   -0.48      4.40     0.      0.
+                                        0.        0.       0.      0.
+                                       -0.27      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+    
+        \begintext
+ 
+ 
+ 
+ 
+     Thalassa
+ 
+
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY804_POLE_RA       = (  299.36      0.          0. )
+           BODY804_POLE_DEC      = (   43.45      0.          0. )
+           BODY804_PM            = (  102.06   1155.7555612   0. )  
+           BODY804_LONG_AXIS     = (    0.                       )
+ 
+ 
+           BODY804_NUT_PREC_RA   = (    0.70      0.      -0.28    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+   
+  
+           BODY804_NUT_PREC_DEC  = (   -0.51      0.      -0.21    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0. 
+                                        0.                             )
+ 
+           BODY804_NUT_PREC_PM   = (   -0.48      0.       0.19    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0. 
+                                        0.                             )
+                                                                 
+        \begintext
+ 
+ 
+ 
+     Despina
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+ 
+        \begindata
+  
+           BODY805_POLE_RA       = (  299.36      0.          0. )
+           BODY805_POLE_DEC      = (   43.45      0.          0. )
+           BODY805_PM            = (  306.51  +1075.7341562   0. )
+           BODY805_LONG_AXIS     = (    0.                       )
+ 
+ 
+           BODY805_NUT_PREC_RA   = (    0.70      0.       0.     -0.09
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                              )
+ 
+           BODY805_NUT_PREC_DEC  = (   -0.51      0.       0.     -0.07
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                              )
+ 
+           BODY805_NUT_PREC_PM   = (   -0.49      0.       0.      0.06
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                              )
+        \begintext
+ 
+ 
+ 
+     Galatea
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+ 
+        \begindata
+  
+           BODY806_POLE_RA       = (   299.36      0.          0. )
+           BODY806_POLE_DEC      = (    43.43      0.          0. )
+           BODY806_PM            = (   258.09    839.6597686   0. )
+           BODY806_LONG_AXIS     = (     0.                       )
+ 
+ 
+           BODY806_NUT_PREC_RA   = (    0.70      0.       0.      0.
+                                       -0.07      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+ 
+           BODY806_NUT_PREC_DEC  = (   -0.51      0.       0.      0.
+                                       -0.05      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+ 
+           BODY806_NUT_PREC_PM   = (   -0.48      0.       0.      0.
+                                        0.05      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             ) 
+        \begintext
+
+ 
+     Larissa
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+  
+        \begindata
+
+           BODY807_POLE_RA       = (   299.36     0.           0. )
+           BODY807_POLE_DEC      = (    43.41     0.           0. )
+           BODY807_PM            = (   179.41  +649.0534470    0. )
+           BODY807_LONG_AXIS     = (     0.                       )
+ 
+ 
+           BODY807_NUT_PREC_RA   = (    0.70      0.       0.      0.
+                                        0.       -0.27     0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+ 
+           BODY807_NUT_PREC_DEC  = (   -0.51      0.       0.      0.
+                                        0.       -0.20     0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+ 
+           BODY807_NUT_PREC_PM   = (   -0.48      0.       0.      0.
+                                        0.        0.19     0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+        \begintext
+ 
+ 
+ 
+     Proteus
+ 
+
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY808_POLE_RA       = (  299.27      0.          0.  )
+           BODY808_POLE_DEC      = (   42.91      0.          0.  )
+           BODY808_PM            = (   93.38   +320.7654228   0.  )
+           BODY808_LONG_AXIS     = (    0.                        )
+ 
+ 
+           BODY808_NUT_PREC_RA   = (    0.70      0.       0.      0.
+                                        0.        0.      -0.05    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+ 
+           BODY808_NUT_PREC_DEC  = (   -0.51      0.       0.      0.
+                                        0.        0.      -0.04    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+ 
+           BODY808_NUT_PREC_PM   = (   -0.48      0.       0.      0.
+                                        0.        0.       0.04    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+   
+        \begintext
+  
+ 
+ 
+ 
+ 
+Satellites of Pluto
+ 
+     Charon
+ 
+        Old values:
+        
+           Values are from the 2006 IAU report. 
+ 
+           body901_pole_ra       = (   312.993    0.         0. )
+           body901_pole_dec      = (     6.163    0.         0. )
+           body901_pm            = (    57.305  -56.3625225  0. )
+           body901_long_axis     = (     0.                     )
+
+               
+        Current values:
+ 
+        Due to the new definition of planetocentric coordinates
+        for small bodies, and to the reclassification of Pluto
+        as a dwarf planet, Charon's north pole direction has been
+        inverted. 
+
+        The PM constant W0 is from [2]. 
+
+        \begindata
+ 
+           BODY901_POLE_RA       = (   132.993    0.         0. )
+           BODY901_POLE_DEC      = (    -6.163    0.         0. )
+           BODY901_PM            = (   122.695   56.3625225  0. )
+           BODY901_LONG_AXIS     = (     0.                     )
+
+        \begintext
+ 
+ 
+ 
+Orientation constants for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+Ceres
+
+        Current values:
+ 
+        \begindata
+
+           BODY2000001_POLE_RA       = (   291.       0.         0.  )
+           BODY2000001_POLE_DEC      = (    59.       0.         0.  )
+           BODY2000001_PM            = (   170.90   952.1532     0.  )
+           BODY2000001_LONG_AXIS     = (     0.                      )
+ 
+        \begintext
+
+
+
+Pallas
+
+        Current values:
+ 
+        \begindata
+
+           BODY2000002_POLE_RA       = (    33.       0.         0.  )
+           BODY2000002_POLE_DEC      = (    -3.       0.         0.  )
+           BODY2000002_PM            = (    38.    1105.8036     0.  )
+           BODY2000002_LONG_AXIS     = (     0.                      )
+ 
+        \begintext
+
+
+
+Vesta
+
+        Old values:
+        
+           Values are from the 2009 IAU report. 
+
+           body2000004_pole_ra       = (   301.      0.         0.  )
+           body2000004_pole_dec      = (    41.      0.         0.  )
+           body2000004_pm            = (   292.   1617.332776   0.  )
+           body2000004_long_axis     = (     0.                     )
+
+        Current values:
+ 
+        \begindata
+
+           BODY2000004_POLE_RA       = (   305.8     0.         0.  )
+           BODY2000004_POLE_DEC      = (    41.4     0.         0.  )
+           BODY2000004_PM            = (   292.   1617.332776   0.  )
+           BODY2000004_LONG_AXIS     = (     0.                     )
+ 
+        \begintext
+
+
+
+Lutetia
+
+        Current values:
+ 
+        \begindata
+
+           BODY2000021_POLE_RA       = (    52.       0.         0.  )
+           BODY2000021_POLE_DEC      = (    12.       0.         0.  )
+           BODY2000021_PM            = (    94.    1057.7515     0.  )
+           BODY2000021_LONG_AXIS     = (     0.                      )
+ 
+        \begintext
+
+
+
+Ida
+
+        Old values:
+        
+           BODY2431010_POLE_RA       = (  168.76      0.         0. )
+           BODY2431010_POLE_DEC      = (   -2.88      0.         0. )
+           BODY2431010_PM            = (  265.95  +1864.6280070  0. )
+           BODY2431010_LONG_AXIS     = (    0.                      )
+
+        Current values:
+ 
+        The PM constant W0 is from [2]. 
+
+        \begindata
+ 
+           BODY2431010_POLE_RA       = (  168.76      0.         0. )
+           BODY2431010_POLE_DEC      = (   -2.88      0.         0. )
+           BODY2431010_PM            = (  274.05  +1864.6280070  0. )
+           BODY2431010_LONG_AXIS     = (    0.                      )
+ 
+        \begintext
+
+
+
+Eros
+
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY2000433_POLE_RA       = (   11.35       0.           0. )
+           BODY2000433_POLE_DEC      = (   17.22       0.           0. )
+           BODY2000433_PM            = (  326.07    1639.38864745   0. )
+           BODY2000433_LONG_AXIS     = (    0.                         )
+ 
+        \begintext
+
+
+
+Davida
+
+        Current values:
+ 
+        \begindata
+
+           BODY2000511_POLE_RA       = (  297.        0.           0. )
+           BODY2000511_POLE_DEC      = (    5.        0.           0. )
+           BODY2000511_PM            = (  268.1    1684.4193549    0. )
+           BODY2000511_LONG_AXIS     = (    0.                        )
+ 
+        \begintext
+
+
+
+Gaspra
+
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+               
+        Current values:
+ 
+        \begindata 
+ 
+           BODY9511010_POLE_RA       = (   9.47     0.         0. )
+           BODY9511010_POLE_DEC      = (  26.70     0.         0. )
+           BODY9511010_PM            = (  83.67  1226.9114850  0. )
+           BODY9511010_LONG_AXIS     = (   0.                     )
+
+        \begintext
+
+
+
+Steins
+
+        Current values:
+ 
+        \begindata 
+ 
+           BODY2002867_POLE_RA       = (  90.        0.        0. )
+           BODY2002867_POLE_DEC      = ( -62.        0.        0. )
+           BODY2002867_PM            = (  93.94   1428.852332  0. )
+           BODY2002867_LONG_AXIS     = (   0.                     )
+
+        \begintext
+
+
+
+Itokawa
+
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY2025143_POLE_RA       = (   90.53       0.           0. )
+           BODY2025143_POLE_DEC      = (  -66.30       0.           0. )
+           BODY2025143_PM            = (  000.0      712.143        0. )
+           BODY2025143_LONG_AXIS     = (    0.                         )
+ 
+        \begintext
+
+
+
+9P/Tempel 1
+
+
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY1000093_POLE_RA       = (   294.       0.         0.  )
+           BODY1000093_POLE_DEC      = (    73.       0.         0.  )
+           BODY1000093_PM            = (   252.63   212.064      0.  )
+           BODY1000093_LONG_AXIS     = (     0.                      )
+ 
+        \begintext
+
+
+
+19P/Borrelly
+
+        Old values:
+        
+           Values are unchanged in the 2009 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY1000005_POLE_RA       = (   218.5      0.         0.  )
+           BODY1000005_POLE_DEC      = (   -12.5      0.         0.  )
+           BODY1000005_PM            = (   000.     390.0        0.  )
+           BODY1000005_LONG_AXIS     = (     0.                      )
+ 
+        \begintext
+
+
+
+
+
+
+ 
+Radii of Sun and Planets
+--------------------------------------------------------
+ 
+ 
+Sun
+ 
+        \begindata
+ 
+        BODY10_RADII      = (  696000.  696000.  696000.  )
+ 
+        \begintext
+ 
+ 
+Mercury
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY199_RADII     = ( 2439.7   2439.7   2439.7 )
+ 
+        \begintext
+ 
+ 
+Venus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY299_RADII     = ( 6051.8   6051.8   6051.8 )
+ 
+        \begintext
+ 
+ 
+Earth
+ 
+     Old values:
+ 
+        Values are from the 2006 IAU report.
+ 
+        body399_radii     = ( 6378.14   6378.14   6356.75 )
+
+
+     Current values:
+ 
+
+        \begindata
+ 
+        BODY399_RADII     = ( 6378.1366   6378.1366   6356.7519 )
+ 
+        \begintext
+ 
+ 
+Mars
+ 
+ 
+     Old values:
+
+        Values are from the 2006 IAU report.
+
+        body499_radii       = (  3397.  3397.  3375.  )
+
+ 
+     Current values:
+
+        The 2009 IAU report gives separate values for the north and
+        south polar radii:
+
+           north:  3373.19
+           south:  3379.21 
+
+        The report provides the average of these values as well,
+        which we use as the polar radius for the triaxial model.
+ 
+        \begindata
+ 
+        BODY499_RADII       = ( 3396.19   3396.19   3376.20 )
+ 
+        \begintext
+ 
+ 
+ 
+Jupiter
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY599_RADII     = ( 71492   71492   66854 )
+ 
+        \begintext
+ 
+ 
+ 
+Saturn
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY699_RADII     = ( 60268   60268   54364 )
+ 
+        \begintext
+ 
+ 
+ 
+Uranus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY799_RADII     = ( 25559   25559   24973 )
+ 
+        \begintext
+ 
+ 
+ 
+Neptune
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report.
+  
+     Current values:
+ 
+        (Values are for the 1 bar pressure level.)
+ 
+        \begindata
+ 
+        BODY899_RADII     = ( 24764   24764  24341 )
+ 
+        \begintext
+ 
+ 
+
+Radii of the Dwarf Planet Pluto
+--------------------------------------------------------
+
+ 
+Pluto
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY999_RADII     = ( 1195   1195   1195 )
+ 
+        \begintext
+ 
+
+
+
+Radii of Satellites
+--------------------------------------------------------
+ 
+ 
+Moon
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY301_RADII     = ( 1737.4   1737.4   1737.4 )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Mars
+ 
+     Old values:
+ 
+        Values are from the 2006 IAU report. 
+ 
+        body401_radii     = ( 13.4    11.2    9.2 )
+        body402_radii     = (  7.5     6.1    5.2 )
+
+     Current values:
+ 
+        \begindata
+ 
+        BODY401_RADII     = ( 13.0    11.4    9.1 )
+        BODY402_RADII     = (  7.8     6.0    5.1 )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Jupiter
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report,
+        except for those of Europa, Ganymede, Callisto, 
+        and Metis. For Metis, now all three radii are
+        provided.
+ 
+           body502_radii     = ( 1564.13  1561.23  1560.93 )
+           body503_radii     = ( 2632.4   2632.29  2632.35 )
+           body504_radii     = ( 2409.4   2409.2   2409.3  )
+
+           The value for the second radius for body 516 is not given in 
+           2003 IAU report.   The values given are:
+
+              body516_radii    = (  30   ---   20   )
+
+           For use within the SPICE system, we use only the mean radius.
+
+           body516_radii    = (  21.5   21.5  21.5  )
+
+
+
+
+     Current values:
+         
+        Note that for Ganymede and Callisto only mean radii
+        are provided.
+
+        \begindata
+ 
+        BODY501_RADII     = ( 1829.4   1819.4   1815.7  )
+        BODY502_RADII     = ( 1562.6  1560.3    1559.5  )
+        BODY503_RADII     = ( 2631.2  2631.2    2631.2  )
+        BODY504_RADII     = ( 2410.3  2410.3    2410.3  )
+        BODY505_RADII     = (  125       73       64    )
+ 
+        \begintext
+ 
+        Only mean radii are available in the 2003 IAU report for bodies
+        506-513.
+ 
+        \begindata
+ 
+        BODY506_RADII    = (    85       85       85   )
+        BODY507_RADII    = (    40       40       40   )
+        BODY508_RADII    = (    18       18       18   )
+        BODY509_RADII    = (    14       14       14   )
+        BODY510_RADII    = (    12       12       12   )
+        BODY511_RADII    = (    15       15       15   )
+        BODY512_RADII    = (    10       10       10   )
+        BODY513_RADII    = (     5        5        5   )
+        BODY514_RADII    = (    58       49       42   )
+        BODY515_RADII    = (    10        8        7   )
+        BODY516_RADII    = (    30       20       17   )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Saturn
+ 
+ 
+     Old values:
+ 
+        Values are from the 2006 IAU report.
+    
+        body601_radii     = (  207.4     196.8     190.6  )
+        body602_radii     = (  256.6     251.4     248.3  )
+        body603_radii     = (  540.4     531.1     527.5  )
+        body604_radii     = (  563.8     561.0     560.3  )
+        body605_radii     = (  767.2     762.5     763.1  )
+        body606_radii     = ( 2575      2575      2575    )
+        body607_radii     = (  164       130       107    )
+        body608_radii     = (  747.4     747.4     712.4  )
+        body609_radii     = (  108.6     107.7     101.5  )
+        body610_radii     = (   97.0      95.0      77.0  )
+        body611_radii     = (   69.0      55.0      55.0  )
+ 
+ 
+        Only the first equatorial radius for Helene (body 612) is given in the
+        2006 IAU report:
+ 
+            body612_radii     = (       17.5        ---          ---     )
+ 
+        The mean radius is 16km; we use this radius for all three axes, as
+        we do for the satellites for which only the mean radius is available.
+  
+        body612_radii     = (  17.5      17.5      17.5  )
+        body613_radii     = (  15        12.5       7.5  )
+        body614_radii     = (  15.0       8.0       8.0  )
+        body615_radii     = (  18.5      17.2      13.5  )
+        body616_radii     = (  74.0      50.0      34.0  )
+        body617_radii     = (  55.0      44.0      31.0  )
+ 
+         For Pan, only a mean radius is given in the 2006 report.
+ 
+        body618_radii     = (   10       10     10   )
+ 
+  
+       
+     Current values:
+ 
+        \begindata
+ 
+        BODY601_RADII     = (  207.8     196.7     190.6   )
+        BODY602_RADII     = (  256.6     251.4     248.3   )
+        BODY603_RADII     = (  538.4     528.3     526.3   )
+        BODY604_RADII     = (  563.4     561.3     559.6   )
+        BODY605_RADII     = (  765.0     763.1     762.4   )
+        BODY606_RADII     = ( 2575.15    2574.78   2574.47 )
+        BODY607_RADII     = (  180.1      133.0    102.7   )
+        BODY608_RADII     = (  745.7     745.7     712.1   )
+        BODY609_RADII     = (  109.4     108.5     101.8   )
+        BODY610_RADII     = (  101.5      92.5      76.3   )
+        BODY611_RADII     = (   64.9      57.0      53.1   ) 
+        BODY612_RADII     = (   21.7      19.1      13.0   )
+        BODY613_RADII     = (   16.3      11.8      10.0   )
+        BODY614_RADII     = (   15.1      11.5       7.0   )
+        BODY615_RADII     = (   20.4      17.7       9.4   )
+        BODY616_RADII     = (   67.8      39.7      29.7   )
+        BODY617_RADII     = (   52.0      40.5      32.0   ) 
+        BODY618_RADII     = (   17.2      15.7      10.4   )
+
+        BODY632_RADII     = (    1.6       1.6       1.6   )
+        BODY633_RADII     = (    2.9       2.8       2.0   )
+        BODY634_RADII     = (    1.5       1.2       1.0   )
+        BODY635_RADII     = (    4.3       4.1       3.2   )
+        BODY649_RADII     = (    1         1         1     )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Uranus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY701_RADII     = (  581.1   577.9   577.7 )
+        BODY702_RADII     = (  584.7   584.7   584.7 )
+        BODY703_RADII     = (  788.9   788.9   788.9 )
+        BODY704_RADII     = (  761.4   761.4   761.4 )
+        BODY705_RADII     = (  240.4   234.2   232.9 )
+ 
+        \begintext
+ 
+        The 2000 report gives only mean radii for satellites 706--715.
+ 
+        \begindata
+ 
+        BODY706_RADII     = (   13      13      13 )
+        BODY707_RADII     = (   15      15      15 )
+        BODY708_RADII     = (   21      21      21 )
+        BODY709_RADII     = (   31      31      31 )
+        BODY710_RADII     = (   27      27      27 )
+        BODY711_RADII     = (   42      42      42 )
+        BODY712_RADII     = (   54      54      54 )
+        BODY713_RADII     = (   27      27      27 )
+        BODY714_RADII     = (   33      33      33 )
+        BODY715_RADII     = (   77      77      77 )
+ 
+        \begintext
+ 
+ 
+ 
+ 
+Satellites of Neptune
+ 
+ 
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+ 
+     Current values:
+ 
+        The 2009 report gives mean radii only for bodies 801-806.
+ 
+        \begindata
+ 
+        BODY801_RADII     = ( 1352.6  1352.6  1352.6 )
+        BODY802_RADII     = (  170     170     170   )
+        BODY803_RADII     = (   29      29     29    )
+        BODY804_RADII     = (   40      40     40    )
+        BODY805_RADII     = (   74      74     74    )
+        BODY806_RADII     = (   79      79     79    )
+ 
+        \begintext 
+ 
+        The second equatorial radius for Larissa is not given in the 2009
+        report.  The available values are:
+ 
+            BODY807_RADII     = (   104     ---     89   )
+ 
+        For use within the SPICE system, we use only the mean radius.
+
+        \begindata
+ 
+        BODY807_RADII     = (   96      96     96   )
+        BODY808_RADII     = (  218     208    201   )
+ 
+        \begintext
+ 
+ 
+ 
+ 
+Satellites of Pluto
+ 
+     
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+             
+     Current values:
+ 
+        \begindata
+ 
+        BODY901_RADII     = (  605     605    605   )
+ 
+        \begintext
+ 
+
+
+Radii for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+
+
+Ceres
+
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2000001_RADII     = ( 487.3  487.3  454.7 )
+ 
+        \begintext
+
+
+
+Vesta
+
+
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2000004_RADII     = ( 289.  280.  229.  )
+ 
+        \begintext
+
+
+
+Lutetia
+
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2000021_RADII     = (  62.0   50.5   46.5  )
+ 
+        \begintext
+
+
+           
+Ida
+
+     
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+
+     Current values:
+ 
+ 
+        \begindata
+ 
+        BODY2431010_RADII     = (   26.8   12.0    7.6 )
+ 
+        \begintext
+
+
+
+Mathilde
+
+
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2000253_RADII     = (  33.   24.   23.  )
+ 
+        \begintext
+
+
+      
+Eros
+ 
+
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+
+     Current values:
+ 
+ 
+        \begindata
+ 
+        BODY2000433_RADII     = (  17.0   5.5   5.5  )
+ 
+        \begintext
+
+
+
+Davida
+ 
+
+     Current values:
+ 
+ 
+        \begindata
+ 
+        BODY2000511_RADII     = (  180.   147.   127.  )
+ 
+        \begintext
+
+
+
+Gaspra
+
+     
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+
+     Current values:
+ 
+ 
+        \begindata
+ 
+        BODY9511010_RADII     = (    9.1    5.2    4.4 )
+ 
+        \begintext
+
+
+ 
+Steins
+ 
+
+     Current values:
+ 
+ 
+        \begindata
+ 
+        BODY2002867_RADII     = (  3.24     2.73     2.04  )
+ 
+        \begintext
+
+
+
+Toutatis
+
+
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2004179_RADII     = (  2.13  1.015  0.85  )
+ 
+        \begintext
+
+
+ 
+Itokawa
+
+
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2025143_RADII     = (  0.535   0.294   0.209  )
+ 
+        \begintext
+
+
+Kleopatra
+
+
+     Old values:
+
+        Values are from the 2003 report.
+
+ 
+        body2000216_radii     = (   108.5      47    40.5  )
+ 
+
+     Current values:
+ 
+ 
+        No values are provided in the 2009 report.
+
+        
+   
+
+
+Halley
+
+
+     Old values:
+ 
+        Values are unchanged in the 2009 IAU report. 
+
+     Current values:
+
+        \begindata
+ 
+        BODY1000036_RADII     = (  8.0   4.0   4.0  )
+ 
+        \begintext
+
+
+
+9P/Tempel 1
+
+
+     Old values:
+ 
+        The effective radius is unchanged in the 2009 IAU report. 
+
+     Current values:
+
+
+        The value in the data assignment below is the 
+        "effective radius."
+            
+        According to [1]:
+
+           The maximum and minimum radii are not properly 
+           the values of the principal semi-axes, they
+           are half the maximum and minimum values of the
+           diameter. Due to the large deviations from a
+           simple ellipsoid, they may not correspond with
+           measurements along the principal axes, or be
+           orthogonal to each other.
+
+        \begindata
+ 
+        BODY1000093_RADII     = (  3.0   3.0   3.0  )
+ 
+        \begintext
+
+
+19P/Borrelly
+
+
+     Old values:
+
+        Values are unchanged in the 2009 report.
+
+     Current values:
+
+
+        The value in the data assignment below is the 
+        "effective radius."
+
+        The first principal axis length is 
+
+           3.5 km
+
+        The lengths of the other semi-axes are not provided
+        by [1].
+
+        \begindata
+ 
+        BODY1000005_RADII     = (  4.22   4.22   4.22  )
+
+        \begintext
+
+
+
+81P/Wild 2
+
+
+     Old values:
+
+        Values are unchanged in the 2009 report.
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY1000107_RADII     = (  2.7   1.9   1.5 )
+ 
+        \begintext
+
+        
+
+===========================================================================
+End of file pck00010.tpc
+===========================================================================
+
+
+
diff --git a/tests/pytests/test_cassini_drivers.py b/tests/pytests/test_cassini_drivers.py
index bddfe992c3e4c43befc37e917847313ef62ca090..978871ba98a63343cb959e2225ced5d628766044 100644
--- a/tests/pytests/test_cassini_drivers.py
+++ b/tests/pytests/test_cassini_drivers.py
@@ -1,62 +1,127 @@
 import pytest
-
 import ale
-from ale.drivers import co_drivers
-from unittest.mock import PropertyMock, patch
+import os
 
-# 'Mock' the spice module where it is imported
-from conftest import SimpleSpice, get_mockkernels
+import numpy as np
+from ale.drivers import co_drivers
+import unittest 
+from unittest.mock import patch
 
-simplespice = SimpleSpice()
-co_drivers.spice = simplespice
+from conftest import get_image_label, get_image_kernels, convert_kernels, compare_dicts
 
 from ale.drivers.co_drivers import CassiniIssPds3LabelNaifSpiceDriver
+from conftest import get_image_kernels, convert_kernels, get_image_label
+
+@pytest.fixture()
+def usgscsm_compare_dict():
+    return {'radii': 
+             {'semimajor': 256.6, 
+               'semiminor': 248.3, 
+               'unit': 'km'}, 
+            'sensor_position': 
+              {'positions': [np.array([ -2256954.95303959, -24306346.83742413,   -639245.80662036])], 
+               'velocities': [np.array([-6890.54418209, -2939.21925245,    21.83699238])], 
+               'unit': 'm'}, 
+            'sun_position': 
+              {'positions': [np.array([-2.30750862e+11, -1.39662303e+12, 3.09841240e+11])], 
+               'velocities': [np.array([-7.41107317e+07, 1.22577658e+07, 3.91731010e+03])], 
+               'unit': 'm'}, 
+            'sensor_orientation': 
+              {'quaternions': [[-0.21183452, -0.66567547, -0.69966839,  0.14988809]]}, 
+            'detector_sample_summing': 1, 
+            'detector_line_summing': 1, 
+            'focal_length_model': {'focal_length': 2003.09}, 
+            'detector_center': {'line': 511.5, 'sample': 511.5}, 
+            'starting_detector_line': 0, 
+            'starting_detector_sample': 0, 
+            'focal2pixel_lines': [0.0, 0.0, 83.33333333333333], 
+            'focal2pixel_samples': [0.0, 83.33333333333333, 0.0], 
+            'optical_distortion': 
+              {'radial': 
+                {'coefficients': [-8e-06, 0, 0]}}, 
+            'image_lines': 1024, 
+            'image_samples': 1024, 
+            'name_platform': 'CASSINI ORBITER', 
+            'name_sensor': 'IMAGING SCIENCE SUBSYSTEM - NARROW ANGLE', 
+            'reference_height': 
+              {'maxheight': 1000, 
+               'minheight': -1000, 
+               'unit': 'm'}, 
+            'name_model': 'USGS_ASTRO_FRAME_SENSOR_MODEL', 
+            'center_ephemeris_time': 376938208.24072826}
+
+@pytest.fixture()
+def test_kernels(scope="module", autouse=True):
+    kernels = get_image_kernels("N1702360370_1")
+    updated_kernels, binary_kernels = convert_kernels(kernels)
+    yield updated_kernels
+    for kern in binary_kernels:
+        os.remove(kern)
+
+def test_cassini_load(test_kernels, usgscsm_compare_dict):
+    label_file = get_image_label("N1702360370_1")
+    usgscsm_isd = ale.load(label_file, props={'kernels': test_kernels}, formatter='usgscsm')
+    assert compare_dicts(usgscsm_isd, usgscsm_compare_dict) == []
+
+# ========= Test cassini pds3label and naifspice driver =========
+class test_cassini_pds3_naif(unittest.TestCase):
+    
+    def setUp(self):
+        label = get_image_label("N1702360370_1", "pds3")
+        self.driver = CassiniIssPds3LabelNaifSpiceDriver(label)
+    
+    def test_short_mission_name(self):
+        assert self.driver.short_mission_name == "co"
+    
+    def test_spacecraft_name(self):
+        assert self.driver.spacecraft_name == "CASSINI"
+    
+    def test_focal2pixel_samples(self):
+        with patch('ale.drivers.co_drivers.spice.gdpool', return_value=[12.0]) as gdpool, \
+             patch('ale.base.data_naif.spice.bods2c', return_value=-12345) as bods2c:
+             assert self.driver.focal2pixel_samples == [0.0, 83.33333333333333, 0.0]
+             gdpool.assert_called_with('INS-12345_PIXEL_SIZE', 0, 1)
+             
+    def test_focal2pixel_lines(self):
+        with patch('ale.drivers.co_drivers.spice.gdpool', return_value=[12.0]) as gdpool, \
+             patch('ale.base.data_naif.spice.bods2c', return_value=-12345) as bods2c:
+             assert self.driver.focal2pixel_lines == [0.0, 0.0, 83.33333333333333]
+             gdpool.assert_called_with('INS-12345_PIXEL_SIZE', 0, 1)
+    
+    def test_odtk(self):
+        assert self.driver.odtk == [-8e-06, 0, 0]
+    
+    def test_instrument_id(self):
+        assert self.driver.instrument_id == "CASSINI_ISS_NAC"
+    
+    def test_focal_epsilon(self):
+        with patch('ale.drivers.co_drivers.spice.gdpool', return_value=[0.03]) as gdpool, \
+             patch('ale.base.data_naif.spice.bods2c', return_value=-12345) as bods2c:
+             assert self.driver.focal_epsilon == 0.03
+             gdpool.assert_called_with('INS-12345_FL_UNCERTAINTY', 0, 1)
+    
+    def test_focal_length(self):
+        # This value isn't used for anything in the test, as it's only used for the
+        # default focal length calculation if the filter can't be found.
+        with patch('ale.drivers.co_drivers.spice.gdpool', return_value=[10.0]) as gdpool, \
+             patch('ale.base.data_naif.spice.bods2c', return_value=-12345) as bods2c:
+             assert self.driver.focal_length == 2003.09
+    
+    def test_detector_center_sample(self):
+        with patch('ale.drivers.co_drivers.spice.gdpool', return_value=[511.5, 511.5]) as gdpool, \
+             patch('ale.base.data_naif.spice.bods2c', return_value=-12345) as bods2c:
+             assert self.driver.detector_center_sample == 511.5
+             gdpool.assert_called_with('INS-12345_FOV_CENTER_PIXEL', 0, 2)
+    
+    def test_detector_center_line(self):
+        with patch('ale.drivers.co_drivers.spice.gdpool', return_value=[511.5, 511.5]) as gdpool, \
+             patch('ale.base.data_naif.spice.bods2c', return_value=-12345) as bods2c:
+             assert self.driver.detector_center_sample == 511.5
+             gdpool.assert_called_with('INS-12345_FOV_CENTER_PIXEL', 0, 2)
+    
+    def test_sensor_model_version(self):
+        assert self.driver.sensor_model_version == 1
+    
+    def test_sensor_frame_id(self):
+        assert self.driver.sensor_frame_id == 14082360
 
-CassiniIssPds3LabelNaifSpiceDriver.metakernel = get_mockkernels
-
-@pytest.fixture
-def driver():
-    return CassiniIssPds3LabelNaifSpiceDriver("")
-
-def test_short_mission_name(driver):
-    assert driver.short_mission_name=='co'
-
-def test_instrument_id(driver):
-    with patch('ale.base.label_pds3.Pds3Label.instrument_id', new_callable=PropertyMock) as mock_instrument_id:
-        mock_instrument_id.return_value = 'ISSNA'
-        assert driver.instrument_id == 'CASSINI_ISS_NAC'
-        mock_instrument_id.return_value = 'ISSWA'
-        assert driver.instrument_id == 'CASSINI_ISS_WAC'
-
-@patch('ale.base.data_naif.NaifSpice.ikid', 123)
-def test_focal_epsilon(driver):
-    assert driver.focal_epsilon == 1
-
-def test_spacecraft_name(driver):
-    assert driver.spacecraft_name == 'CASSINI'
-
-@patch('ale.base.data_naif.NaifSpice.ikid', 123)
-def test_focal2pixel_samples(driver):
-    assert driver.focal2pixel_samples == [0,1000,0]
-
-@patch('ale.base.data_naif.NaifSpice.ikid', 123)
-def test_focal2pixel_lines(driver):
-    assert driver.focal2pixel_lines == [0,0,1000]
-
-def testodtk(driver):
-    with patch('ale.base.label_pds3.Pds3Label.instrument_id', new_callable=PropertyMock) as mock_instrument_id:
-        mock_instrument_id.return_value = 'ISSNA'
-        assert driver.odtk == [float('-8e-6'), 0, 0]
-        mock_instrument_id.return_value = 'ISSWA'
-        assert driver.odtk == [float('-6.2e-5'), 0, 0]
-
-@patch('ale.base.data_naif.NaifSpice.ikid', 123)
-def test_detector_center_line(driver):
-    assert driver.detector_center_line == 1
-
-@patch('ale.base.data_naif.NaifSpice.ikid', 123)
-def test_detector_center_sample(driver):
-        assert driver.detector_center_sample == 1
-
-def test_sensor_model_version(driver):
-    assert driver.sensor_model_version == 1