diff --git a/ale/drivers/viking_drivers.py b/ale/drivers/viking_drivers.py
new file mode 100644
index 0000000000000000000000000000000000000000..74c2eb4926c8ec07f7b81e8a8c9b29d7b4e84162
--- /dev/null
+++ b/ale/drivers/viking_drivers.py
@@ -0,0 +1,82 @@
+import spiceypy as spice
+
+import ale
+from ale.base.data_naif import NaifSpice
+from ale.base.label_isis import IsisLabel
+from ale.base.type_sensor import Framer
+from ale.base.base import Driver
+
+class VikingIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, Driver):
+
+ @property
+ def spacecraft_name(self):
+ """
+ Overridden to work with spice calls.
+
+ Returns
+ -------
+ : str
+ Name of the spacecraft.
+ """
+ name_lookup = {
+ 'VIKING_ORBITER_1': 'VIKING ORBITER 1',
+ 'VIKING_ORBITER_2': 'VIKING ORBITER 2'
+ }
+
+ return name_lookup[super().spacecraft_name]
+
+ @property
+ def alt_ikid(self):
+ """
+ Viking Orbiter 1 & 2 each have an alternate naif id code as defined in the
+ SCLK kernels.
+ Expects spacecraft name to be defined.
+ Returns -27999 for vo1 and -30999 for vo2
+
+ Returns
+ -------
+ : integer
+ Alternate Naif Integer ID code for the instrument
+ """
+
+ alt_id_lookup = {
+ 'VIKING ORBITER 1': -27999,
+ 'VIKING ORBITER 2':-30999
+ }
+
+ return alt_id_lookup[self.spacecraft_name]
+
+ @property
+ def ikid(self):
+ """
+ Overridden to grab the ikid from the Isis Cube since there is no way to
+ obtain this value with a spice bods2c call.
+
+ Returns
+ -------
+ : integer
+ Naif Integer ID code for the instrument
+ """
+ return self.label['IsisCube']['Kernels']['NaifFrameCode']
+
+ @property
+ def ephemeris_start_time(self):
+ """
+ Overridden to use the alternate instrument ID. Also computes an offset to match
+ what is being done in ISIS code.
+ Expects spacecraft_clock_start_count to be defined.
+
+ Returns
+ -------
+ : float
+ ephemeris start time of the image
+ """
+ ephemeris_start_time = spice.scs2e(self.alt_ikid, str(self.spacecraft_clock_start_count))
+
+ if self.exposure_duration <= .420:
+ offset1 = 7.0 / 8.0 * 4.48
+ else:
+ offset1 = 3.0 / 8.0 * 4.48
+ offset2 = 1.0 / 64.0 * 4.48
+
+ return ephemeris_start_time + offset1 + offset2
diff --git a/tests/pytests/data/f004a47/f004a47_0.xsp b/tests/pytests/data/f004a47/f004a47_0.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..882f7c9465824320c9ad97aef2301797400c4a38
--- /dev/null
+++ b/tests/pytests/data/f004a47/f004a47_0.xsp
@@ -0,0 +1,634 @@
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+'-1DEAAE3E44EFF6^5'
+'20409F1BCF505A^4'
+'2CCDB8F97EBC0C^2'
+'-2D9AEE0704A8D4^0'
+'23E006DB88DB62^-2'
+'-17C41DAAD996A2^-2'
+'-2A910332B3C0FC^-4'
+'-12A1A650F76381^-5'
+'-B378E4E5B5C22^-7'
+'-2C5FA4C^8'
+'2A3^6'
+'23^2'
+'1^1'
+END_ARRAY 3 39
+BEGIN_ARRAY 4 54
+'MAR097 '
+'-2C3F00B654EA7E^8'
+'-2C3EF5A98E0114^8'
+'1F3'
+'4'
+'1'
+'3'
+54
+'-2C3ED97^8'
+'2A3^4'
+'8923746F47BA6^-4'
+'8730C71F3AA63^-3'
+'58FADEC94F2968^-3'
+'-2C7C672962C18^-3'
+'-D6FB1B8F1858C^-4'
+'3F5513081AC1A6^-4'
+'8ACD8407C1043^-5'
+'-2AA9A81AFCBF2^-5'
+'-2ABF1BC56E776C^-3'
+'-446395088ADF5C^-3'
+'74090AE0A3875C^-3'
+'1EBF63251E68C4^-3'
+'-11DB19E75CE682^-3'
+'-23123CDB81C202^-4'
+'F47CE931A524B8^-5'
+'13C59BAC1CC28^-6'
+'-197D32A40E685C^-3'
+'-6EFF23753160B^-3'
+'BD71AE06B3FEC8^-4'
+'29744C77D64AFA^-3'
+'-1FFF45EF4A0951^-4'
+'-36658289E7B914^-4'
+'34D15D935EA536^-5'
+'18A900D4EA963^-5'
+'7B883FA42AF96^-7'
+'60AFCF493791D^-6'
+'-571A5E2879FB9C^-6'
+'-264C9483AC3B3A^-6'
+'E20936B2CB705^-7'
+'277B4FA72EF02^-7'
+'-E285F3AA384D48^-8'
+'0^0'
+'4E72B8D9639FC^-7'
+'7E334823A4778^-6'
+'3DAE2A60FD54^-6'
+'-31D45E2B743A88^-6'
+'-8499D0FEBB5B3^-7'
+'458B1168017688^-7'
+'68FB43AA201968^-9'
+'0^0'
+'-11F3AB7EC77A6^-7'
+'CD55EC95D13A4^-7'
+'51F2F334E5BD68^-6'
+'-520EDA2FB4A4D4^-7'
+'-C61ECDCEFB0E88^-7'
+'F0613CA585C81^-8'
+'82EFB587B5BF^-8'
+'0^0'
+'-2C3F03A^8'
+'546^4'
+'32^2'
+'1^1'
+END_ARRAY 4 54
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /home/pgiroux/Desktop/f004a47/f004a47_0.bsp LOG FILE
+
+; Created 2019-09-30/09:31:27.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /home/pgiroux/Desktop/f004a47/f004a47_0.bsp
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/viking1/kernels/spk/viking1a.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -27
+ BEGIN_TIME = 1976 JUN 23 18:11:38.484
+ END_TIME = 1976 JUN 23 18:58:47.261
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/spk/mar097.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 4, 10, 499
+ BEGIN_TIME = 1976 JUN 23 18:11:38.484
+ END_TIME = 1976 JUN 23 18:58:47.261
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/f004a47/f004a47_isis3.lbl b/tests/pytests/data/f004a47/f004a47_isis3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..91a9a8a571aa2c36c5875478b6beb28f3a415a96
--- /dev/null
+++ b/tests/pytests/data/f004a47/f004a47_isis3.lbl
@@ -0,0 +1,105 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 1204
+ TileLines = 1056
+
+ Group = Dimensions
+ Samples = 1204
+ Lines = 1056
+ Bands = 1
+ End_Group
+
+ Group = Pixels
+ Type = UnsignedByte
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftName = VIKING_ORBITER_1
+ InstrumentId = VISUAL_IMAGING_SUBSYSTEM_CAMERA_A
+ TargetName = MARS
+ StartTime = 1976-06-23T18:42:11
+ ExposureDuration = 0.012730 <seconds>
+ SpacecraftClockCount = 25973540
+ FloodModeId = ON
+ GainModeId = HIGH
+ OffsetModeId = OFF
+ End_Group
+
+ Group = Archive
+ DataSetId = VO1/VO2-M-VIS-2-EDR-V2.0
+ ProductId = 004A47
+ MissonPhaseName = PRIMARY_MISSION
+ ImageNumber = 25973540
+ OrbitNumber = 4
+ End_Group
+
+ Group = BandBin
+ FilterName = CLEAR
+ FilterId = 4
+ Center = 0.52 <micrometers>
+ Width = 0.35 <micrometers>
+ End_Group
+
+ Group = Kernels
+ NaifFrameCode = -27001
+ CameraVersion = 1
+ End_Group
+
+
+ Group = Reseaus
+ Line = (4, 8, 11, 13, 15, 17, 18, 20, 21, 22, 23, 132, 134, 137, 139,
+ 141, 143, 145, 147, 148, 150, 151, 152, 260, 264, 266, 268,
+ 270, 272, 274, 276, 277, 279, 281, 389, 391, 394, 396, 398,
+ 400, 401, 403, 405, 407, 408, 409, 518, 521, 523, 526, 528,
+ 529, 531, 532, 534, 536, 538, 647, 648, 651, 653, 655, 657,
+ 658, 660, 662, 663, 665, 666, 776, 779, 781, 783, 785, 786,
+ 788, 789, 790, 792, 794, 906, 907, 909, 911, 913, 914, 915,
+ 917, 918, 920, 922, 923, 1035, 1037, 1039, 1040, 1042, 1043,
+ 1044, 1046, 1047, 1048, 1051)
+ Sample = (18, 137, 255, 372, 489, 605, 721, 837, 954, 1070, 1187, 20,
+ 79, 197, 314, 431, 547, 663, 779, 895, 1011, 1127, 1186, 20,
+ 139, 256, 373, 490, 605, 721, 837, 953, 1069, 1185, 21, 81,
+ 199, 316, 432, 548, 663, 779, 895, 1010, 1126, 1184, 22, 141,
+ 257, 374, 489, 605, 721, 836, 952, 1068, 1184, 22, 82, 199,
+ 316, 431, 547, 663, 778, 893, 1009, 1125, 1183, 22, 141, 257,
+ 373, 489, 604, 719, 835, 950, 1066, 1182, 22, 81, 198, 314,
+ 430, 545, 660, 776, 891, 1007, 1123, 1181, 20, 138, 255, 371,
+ 486, 602, 717, 832, 948, 1064, 1180)
+ Type = (1, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6)
+ Valid = (0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0)
+ Template = $viking1/reseaus/vo1.visa.template.cub
+ Status = Nominal
+ End_Group
+End_Object
+
+Object = Label
+ Bytes = 65536
+End_Object
+
+Object = History
+ Name = IsisCube
+ StartByte = 1336961
+ Bytes = 428
+End_Object
+
+Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 1337389
+ Bytes = 2052
+End_Object
+
+End
diff --git a/tests/pytests/data/f004a47/f004a47_pds3.lbl b/tests/pytests/data/f004a47/f004a47_pds3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..923e8986efe52239d0f71872aa5e8a3e9e1ed15f
--- /dev/null
+++ b/tests/pytests/data/f004a47/f004a47_pds3.lbl
@@ -0,0 +1,1633 @@
+CCSD3ZF0000100000001NJPL3IF0PDS200000001 = SFDU_LABEL
+/* FILE FORMAT AND LENGTH */
+RECORD_TYPE = VARIABLE_LENGTH
+RECORD_BYTES = 1204
+FILE_RECORDS = 2177
+LABEL_RECORDS = 61
+/* POINTERS TO START RECORDS OF MAJOR OBJECTS IN FILE */
+^IMAGE_HISTOGRAM = 62
+^ENCODING_HISTOGRAM = 63
+^ENGINEERING_TABLE = 65
+^LINE_HEADER_TABLE = 66
+^IMAGE = 1122
+/* IMAGE DESCRIPTION */
+DATA_SET_ID = 'VO1/VO2-M-VIS-2-EDR-V2.0'
+SPACECRAFT_NAME = VIKING_ORBITER_1
+MISSION_PHASE_NAME = PRIMARY_MISSION
+TARGET_NAME = MARS
+IMAGE_ID = '004A47'
+IMAGE_NUMBER = 25973540
+IMAGE_TIME = 1976-06-23T18:42:11Z
+EARTH_RECEIVED_TIME = 1976-06-24T07:34:44Z
+ORBIT_NUMBER = 4
+INSTRUMENT_NAME = VISUAL_IMAGING_SUBSYSTEM_CAMERA_A
+GAIN_MODE_ID = HIGH
+FLOOD_MODE_ID = ON
+OFFSET_MODE_ID = OFF
+FILTER_NAME = CLEAR
+EXPOSURE_DURATION = 0.012730 <SECONDS>
+NOTE = "HIGH RESOLUTION STEREO SEQUENCE OF
+ THE A1 LANDING SITE"
+/* DESCRIPTION OF THE OBJECTS CONTAINED IN FILE */
+OBJECT = IMAGE_HISTOGRAM
+ ITEMS = 256
+ ITEM_TYPE = VAX_INTEGER
+ ITEM_BITS = 32
+END_OBJECT
+OBJECT = ENCODING_HISTOGRAM
+ ITEMS = 511
+ ITEM_TYPE = VAX_INTEGER
+ ITEM_BITS = 32
+END_OBJECT
+OBJECT = ENGINEERING_TABLE
+ ROWS = 1
+ ROW_BYTES = 152
+CCSD3ZF0000100000001NJPL3IF0PDS200000001 = SFDU_LABEL
+
+OBJECT = ENGINEERING_TABLE_STRUCTURE
+ INTERCHANGE_FORMAT = BINARY
+ BYTES = 152
+ NOTE = "This structure describes the format of
+ the engineering record that is included in each image file.
+ This record contains the first 152 bytes of data extracted from
+ the Mission and Test Imaging System (MTIS) header record on each
+ file of an imaging EDR tape."
+
+ OBJECT = COLUMN
+ NAME = MTIS_RECORD_ID
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 1
+ BYTES = 2
+ DESCRIPTION = "Mission and Test Imaging System record
+ ID."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PHYSICAL_SEQUENCE_NUMBER
+ DATA_TYPE = VAX_UNSIGNED_INTEGER
+ START_BYTE = 3
+ BYTES = 2
+ DESCRIPTION = "Physical sequence number on Experiment
+ Data Record tape. Not used."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LOGICAL_SEQUENCE_NUMBER
+ DATA_TYPE = VAX_UNSIGNED_INTEGER
+ START_BYTE = 5
+ BYTES = 2
+ DESCRIPTION = "Logical sequence number on Experiment
+ Data Record tape. Not used."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_ERT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 7
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time year and day
+ value. Time of first line segment in the file containing valid
+ data. This field is NOT stored in VAX least significant byte
+ first format."
+
+ OBJECT = BIT_COLUMN
+ NAME = FIRST_ERT_YEAR
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 1
+ BITS = 7
+ DESCRIPTION = "Earth Received Time year of century
+ (1900). Time of first line record in the file containing valid
+ data. This field is often incorrect."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FIRST_ERT_DAY
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 7
+ BITS = 9
+ DESCRIPTION = "Earth Received Time day of year."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_ERT_MINUTE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 9
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time minute of day."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_ERT_MILLISECOND
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 11
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time millisecond of
+ minute."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_ERT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 13
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time year and day
+ value. Time of last line segment of the file containing valid
+ data."
+
+ OBJECT = BIT_COLUMN
+ NAME = LAST_ERT_YEAR
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 1
+ BITS = 7
+ DESCRIPTION = "Earth Received Time year of century
+ (1900). This field is often incorrect."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = LAST_ERT_DAY
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 8
+ BITS = 9
+ DESCRIPTION = "Earth Received Time day of year."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_ERT_MINUTE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 15
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time minute of day."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_ERT_MILLISECOND
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 17
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time millisecond of
+ minute."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_FDS_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 19
+ BYTES = 4
+ DESCRIPTION = "Flight Data Subsystem count for the
+ first line segment of the file containing valid data. Note that
+ this may not correspond to the FDS count for line 1, segment 1."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_FDS_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 23
+ BYTES = 4
+ DESCRIPTION = "Flight Data Subsystem count for the
+ last line segment of the file containing valid data. Note that
+ this may not correspond to the FDS count for segment 7 of line
+ 1056."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = EDR_ID
+ DATA_TYPE = CHARACTER
+ START_BYTE = 27
+ BYTES = 6
+ DESCRIPTION = "Tape reel identifier of the original
+ EDR tape for this image."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = EDR_FILE_NUMBER
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 33
+ BYTES = 2
+ DESCRIPTION = "File number of image on original EDR
+ tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FILL_IN
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 34
+ BYTES = 1
+ DESCRIPTION = "Value used to fill in missing samples
+ (always zero)."
+ END_OBJECT = COLUMN
+ OBJECT = COLUMN
+ NAME = TRACK_PRESENCE_MASK
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 36
+ BYTES = 1
+ DESCRIPTION = "Mask indicating which tracks are
+ present in the image. The nominal value is HEX 7F, indicating
+ that all seven tracks are present."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = AVERAGE_PIXEL
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 37
+ BYTES = 2
+ DESCRIPTION = "Average pixel value for image."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_1
+ DATA_TYPE = CHARACTER
+ START_BYTE = 39
+ BYTES = 4
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MINIMUM_SNR
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 43
+ BYTES = 2
+ FACTOR = 0.03125
+ DESCRIPTION = "Minimum signal to noise ratio. The
+ minimum noise level found for the scan lines. Divide by 32 to
+ get the actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MAXIMUM_SNR
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 45
+ BYTES = 2
+ FACTOR = 0.03125
+ DESCRIPTION = "Maximum signal to noise ratio. The
+ maximum noise level found for the scan lines. Divide by 32 to
+ get the actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_2
+ DATA_TYPE = CHARACTER
+ START_BYTE = 47
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MINIMUM_AGC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 49
+ BYTES = 2
+ FACTOR = 0.0625
+ DESCRIPTION = "Automatic gain control minimum.
+ Divide by 16 to get actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MAXIMUM_AGC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 51
+ BYTES = 2
+ FACTOR = 0.0625
+ DESCRIPTION = "Automatic gain control maximum.
+ Divide by 16 to get actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_3
+ DATA_TYPE = CHARACTER
+ START_BYTE = 53
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 55
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that contain some valid data (maximum is 7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FULLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 57
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that were fully synchronized (maximum is 7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PARTLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 59
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that were partly synchronized (maximum is 7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI0_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 61
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 0 (maximum is 7 x 1056).
+ DQI0 indicates bad data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI1_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 63
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 1 (maximum is 7 x 1056).
+ DQI1 means SNR low, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI2_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 65
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 2 (maximum is 7 x 1056).
+ DQI2 means SNR good, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI3_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 67
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 3 (maximum is 7 x 1056).
+ DQI3 means SNR low, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI4_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 69
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 4 (maximum is 7 x 1056).
+ DQI4 means SNR good, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FDS_CORRECTIONS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 71
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with corrected FDS counts."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PNERROR_CORRECTIONS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 73
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with corrected pseudonoise codes."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = ADJUSTED_PNERROR_CORRECTIONS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 75
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with corrected pseudonoise codes adjusted based on the
+ number of line segments processed versus the total in a full
+ image (7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNREADABLE_RECORDS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 77
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that could not be read from the Master Data Record tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LOGICAL_SEQUENCE_BREAKS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 79
+ BYTES = 2
+ DESCRIPTION = "Total number of breaks in logical
+ sequence number in reading the System/Master Data Record tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DATA_BREAKS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 81
+ BYTES = 2
+ DESCRIPTION = "Total number of breaks in data
+ sequence in reading the System/Master Data Record tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_4
+ DATA_TYPE = CHARACTER
+ START_BYTE = 83
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINES
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 85
+ BYTES = 2
+ DESCRIPTION = "Total number of lines in the file that
+ contain some valid data (nominal is 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FULL_LINES
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 87
+ BYTES = 2
+ DESCRIPTION = "Number of lines in the file that are
+ composed of seven line segments."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PARTIAL_LINES
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 89
+ BYTES = 2
+ DESCRIPTION = "Total number of line records in the
+ file that contain some valid data but are not composed of seven
+ line segments."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_LINE_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 91
+ BYTES = 2
+ DESCRIPTION = "First line in image containing valid
+ data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_LINE_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 93
+ BYTES = 2
+ DESCRIPTION = "Last line in image containing valid
+ data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_5
+ DATA_TYPE = CHARACTER
+ START_BYTE = 95
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = IMAGE_ID
+ DATA_TYPE = CHARACTER
+ START_BYTE = 97
+ BYTES = 6
+ DESCRIPTION = "Image identifier (PICNO) for this
+ image, formatted OOOSNN, where OOO is orbit number, S is
+ spacecraft identifier (A for Viking Orbiter 1 prime and extended
+ missions; B for Viking Orbiter 2; and S for Viking Orbiter 1
+ Survey mission)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VRP_RUN_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 103
+ BYTES = 2
+ DESCRIPTION = "Viking Reconstruction Processing run
+ number."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DISK_ID
+ DATA_TYPE = CHARACTER
+ START_BYTE = 105
+ BYTES = 6
+ DESCRIPTION = "MTIS disk identifier of the original
+ EDR file for this image."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_6
+ DATA_TYPE = CHARACTER
+ START_BYTE = 111
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = TRANSMITTED_CODE_WORD1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 113
+ BYTES = 2
+ DESCRIPTION = "Transmitted command code word for the
+ image."
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ START_BIT = 1
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Set to 1 if data not present for the
+ following measurements."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ START_BIT = 3
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Data quality indicator associated with
+ code word values. Where: 0 is bad data; 1 is SNR low, GCF block
+ error; 2 is SNR good, GCF block bad; 3 is SNR low, GCF block
+ good; 4 is SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = CATHODE_CURRENT_FLAG
+ START_BIT = 7
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Cathode current off (0) or on (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = GAIN_FLAG
+ START_BIT = 8
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Gain mode low (0) or high (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = LIGHT_FLOOD_FLAG
+ START_BIT = 9
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Light flood off (0) or on (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FILTER_STEP
+ START_BIT = 10
+ BITS = 2
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Filter step indicator."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = EXPOSURE_CODE
+ START_BIT = 12
+ BITS = 5
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Exposure interval code."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = TRANSMITTED_CODE_WORD2
+ DATA_TYPE = INTEGER
+ START_BYTE = 115
+ BYTES = 2
+ DESCRIPTION = "Transmitted command code word 2 for
+ this image."
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ START_BIT = 1
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Set to 1 if data not present for the
+ following measurements."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ START_BIT = 3
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Data quality indicator associated with
+ code word values. where: 0 is bad data; 1 is SNR low, GCF block
+ error; 2 is SNR good, GCF block bad; 3 is SNR low, GCF block
+ good; 4 is SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FILTER_NUMBER
+ START_BIT = 10
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Filter number: where 1 is blue; 2 is
+ minus blue; 3 is violet; 4 is clear; 5 is green; and 6 is red."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = CAMERA_SERIAL_NUMBER
+ START_BIT = 13
+ BITS = 4
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Visual Imaging Subsystem camera serial
+ number."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = RECEIVED_CODE_WORD1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 117
+ BYTES = 2
+ DESCRIPTION = "Received command code word for the
+ image."
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ START_BIT = 1
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Set to 1 if data not present for the
+ following measurements."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ START_BIT = 3
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Data quality indicator associated with
+ code word values. where: 0 is bad data; 1 is SNR low, GCF block
+ error; 2 is SNR good, GCF block bad; 3 is SNR low, GCF block
+ good; 4 is SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = CATHODE_CURRENT_FLAG
+ START_BIT = 7
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Cathode current (beam) off (0) or on
+ (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = GAIN_FLAG
+ START_BIT = 8
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Gain mode low (0) or high (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = LIGHT_FLOOD_FLAG
+ START_BIT = 9
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Light flood off (0) or on (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FILTER_STEP
+ START_BIT = 10
+ BITS = 2
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Filter step."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = EXPOSURE_CODE
+ START_BIT = 12
+ BITS = 5
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Exposure interval code."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS50_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 121
+ BYTES = 2
+ DESCRIPTION = "Plus 50 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS15_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 123
+ BYTES = 2
+ DESCRIPTION = "Plus 15 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS12_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 125
+ BYTES = 2
+ DESCRIPTION = "Plus 12 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS5_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 127
+ BYTES = 2
+ DESCRIPTION = "Plus 5 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_MINUS15_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 129
+ BYTES = 2
+ DESCRIPTION = "Minus 15 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_MINUS23_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 131
+ BYTES = 2
+ DESCRIPTION = "Minus 23 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_AVERAGE_VIDEO
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 133
+ BYTES = 2
+ DESCRIPTION = "Average video."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = POWER_CONVERTER_INPUT_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 135
+ BYTES = 2
+ DESCRIPTION = "Power converter input current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = CATHODE_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 137
+ BYTES = 2
+ DESCRIPTION = "Cathode current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = CATHODE_VOLTAGE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 139
+ BYTES = 2
+ DESCRIPTION = "Cathode voltage."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FILAMENT_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 141
+ BYTES = 2
+ DESCRIPTION = "Filament current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FRAME_SWEEP_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 143
+ BYTES = 2
+ DESCRIPTION = "Frame sweep current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_SWEEP_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 145
+ BYTES = 2
+ DESCRIPTION = "Line sweep current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = GRID3_VOLTAGE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 147
+ BYTES = 2
+ DESCRIPTION = "Grid 3 voltage."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FOCUS_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 149
+ BYTES = 2
+ DESCRIPTION = "Focus current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DIGITAL_LADDER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 151
+ BYTES = 2
+ DESCRIPTION = "Digital ladder."
+ END_OBJECT = COLUMN
+
+END_OBJECT = ENGINEERING_TABLE_STRUCTURE
+
+END
+END_OBJECT
+OBJECT = LINE_HEADER_TABLE
+ ROWS = 1056
+ ROW_BYTES = 62
+CCSD3ZF0000100000001NJPL3IF0PDS200000001 = SFDU_LABEL
+
+OBJECT = LINE_HEADER_TABLE_STRUCTURE
+ INTERCHANGE_FORMAT = BINARY
+ BYTES = 62
+ NOTE = "Viking Orbiter Image Line-header
+ Structure. This label describes the structure of the 62-bytes
+ extracted from the end of each image line."
+
+ OBJECT = COLUMN
+ NAME = FDS_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 1
+ BYTES = 4
+ DESCRIPTION = "Flight Data Subsystem (FDS) clock
+ count."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 5
+ BYTES = 2
+ DESCRIPTION = "Flight Data Subsystem line number,
+ extracted from the telemetry record header information."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FILL_IN
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 7
+ BYTES = 1
+ DESCRIPTION = "Value used to fill in missing samples
+ (always zero)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = TRACK_PRESENCE_MASK
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 8
+ BYTES = 1
+ DESCRIPTION = "Mask indicating which tracks are
+ present in this line. The nominal value is HEX 7F, indicating
+ that all seven tracks are present."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = AVERAGE_PIXEL
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 9
+ BYTES = 2
+ DESCRIPTION = "Average pixel value for this line."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 11
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ line that contain some valid data (maximum is 7)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FULLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 13
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ that were fully synchronized (maximum is 7)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PARTLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 15
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ that were partly synchronized (maximum is 7)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI0_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 17
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 0 (maximum is 7), indicating
+ bad data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI1_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 19
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 1 (maximum is 7), indicating
+ SNR low, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI2_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 21
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 2 (maximum is 7), indicating
+ SNR good, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI3_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 23
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 3 (maximum is 7), indicating
+ SNR low, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI4_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 25
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 4 (maximum is 7), indicating
+ SNR good, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 27
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 29
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT2
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 31
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK2
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 33
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT3
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 35
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK3
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 37
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT4
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 39
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK4
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 41
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT5
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 43
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK5
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 45
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT6
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 47
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK6
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 49
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT7
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 51
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK7
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 53
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = EMBEDDED_SCIENCE_DATA
+ ITEMS = 7
+ DATA_TYPE = INTEGER
+ START_BYTE = 55
+ ITEM_BYTES = 1
+ DESCRIPTION = "Embedded low rate science data from
+ seven segments."
+ END_OBJECT = COLUMN
+
+END_OBJECT = LINE_HEADER_TABLE_STRUCTURE
+
+END
+END_OBJECT
+OBJECT = IMAGE
+ ENCODING_TYPE = HUFFMAN_FIRST_DIFFERENCE
+ LINES = 1056
+ LINE_SAMPLES = 1204
+ SAMPLE_TYPE = UNSIGNED_INTEGER
+ SAMPLE_BITS = 8
+ SAMPLE_BIT_MASK = 2#11111110#
+ CHECKSUM = 205881028
+END_OBJECT
+END
diff --git a/tests/pytests/data/f004a47/naif0012.tls b/tests/pytests/data/f004a47/naif0012.tls
new file mode 100644
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/f004a47/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/f004a47/pck00009.tpc b/tests/pytests/data/f004a47/pck00009.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..bfadaab2b26817327189ff3173e9609f49dedc9d
--- /dev/null
+++ b/tests/pytests/data/f004a47/pck00009.tpc
@@ -0,0 +1,3639 @@
+KPL/PCK
+
+
+P_constants (PcK) SPICE kernel file
+===========================================================================
+
+ By: Nat Bachman (NAIF) 2010 March 3
+
+
+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/IAG
+ 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
+
+
+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 and planets.
+ Additional items included in this section:
+
+ - Earth north geomagnetic centered dipole values
+ for epochs 1945-2000
+
+ - Mars prime meridian offset "lambda_a"
+
+ -- Orientation constants for satellites
+
+ -- Orientation constants for asteroids Eros, Gaspra, Ida,
+ Itokawa, and Vesta
+
+ -- Orientation constants for comets 19P/Borrelly
+ and 9P/Tempel 1
+
+
+ Radii of Bodies
+ ---------------
+
+ -- Radii of Sun and planets
+
+ -- Radii of satellites, where available
+
+ -- Radii of asteroids Ceres, Eros, Gaspra, Ida, Itokawa,
+ Mathilde, Toutatis, and Vesta.
+
+ -- Radii of comets 19P/Borrelly, Halley, 9P/Tempel 1,
+ and 81P/Wild 2
+
+
+
+Version Description
+--------------------------------------------------------
+
+ This file was created on March 3, 2010. This version
+ incorporates data from reference [1].
+
+ This file contains size, shape, and orientation data for all
+ objects described by the previous version of the file, except
+ for Kleopatra: a shape model for this body is not provided in [1]
+ because, according to this source, it had been "modeled from
+ low resolution radar data, and cannot be mapped from those
+ data."
+
+ New objects covered by this file but not the previous
+ version are:
+
+ 19P/Borrelly
+ Halley
+ 9P/Tempel 1
+ 81P/Wild 2
+ Ceres
+ Itokawa
+ Mathilde
+ Toutatis
+
+
+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, and version description section if you modify
+ this file.
+
+Known Limitations and Caveats
+
+ Accuracy
+ --------
+
+ In general, the orientation models given here are claimed by the
+ IAU/IAG 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]) 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. 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 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. A more
+ accurate approximation can be obtained by using both the NAIF
+ lunar frame kernel and the binary lunar orientation PCK file,
+ which 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
+ J2000 epoch 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].
+
+
+ Mars prime meridian offset
+ --------------------------
+
+ The Mars prime meridian offset given by [5] is not used by
+ SPICE geometry software for computations involving the shape
+ of Mars (for example, in sub-observer point or surface intercept
+ computations). The value 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 only planets for which such terms are used are
+ Jupiter and Neptune. Use of trigonometric polynomial terms for
+ natural satellites is and has been supported for all SPICE Toolkit
+ versions.
+
+ 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
+--------------------------------------------------------
+
+ The sources for the constants listed in this file are:
+
+
+ [1] 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."
+
+ [2] Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F.,
+ Cruikshank, D.P., Hilton, J.L., Keller, H.U., Oberst, J.,
+ Simon, J.L., Stooke, P., Tholen, D.J., and Thomas, P.C.
+ "Report of the IAU/IAG Working Group on Cartographic
+ Coordinates and Rotational Elements of the Planets and
+ Satellites: 2003."
+
+ [3] 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.
+
+ [4] Nautical Almanac Office, United States Naval Observatory,
+ H.M. Nautical Almanac Office, Royal Greenwich
+ Observatory, Jet Propulsion Laboratory, Bureau des
+ Longitudes, and The Time Service and Astronomy
+ Departments, United States Naval Observatory (1992).
+ "Explanatory Supplement to the Astronomical Almanac," P.
+ Kenneth Seidelmann, ed. University Science Books, 20
+ Edgehill Road, Mill Valley, CA 9494.
+
+ [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.
+
+
+ Most values are from [1]. All exceptions are
+ commented where they occur in this file. The exceptions are:
+
+
+ -- Radii for the Sun are from [3].
+
+ -- 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
+ [8]. The article [6] was used to check most of
+ these values, and the values were also re-computed from
+ the 9th generation IGRF [9] by Nat Bachman.
+
+ -- The Mars prime meridian offset angle is from [5].
+
+
+ "Old values" listed are from the SPICE P_constants file
+ pck00008.tpc dated September 21, 2004. Most of these values came
+ from the 2003 IAU report [2].
+
+
+
+
+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 = ( 6378.14 6378.14 6356.75 )
+
+ Any blanks preceding or following keyword names, values and equal
+ signs are ignored.
+
+ Assignments may be spread over multiple lines, for example:
+
+ BODY399_RADII = ( 6378.14
+ 6378.14
+ 6356.75 )
+
+ 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 2006 IAU/IAG 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 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 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, 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: 2006 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 = ( 284.95 870.5366420 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 term is zero for all bodies except Mars. It represents the
+ angular offset between the meridian containing the longest axis of
+ the triaxial ellipsoid used to model a body's surface and the
+ prime meridian of the body.
+
+ 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 2006 IAU report does
+ not use any other models, except in the case of Mars, where
+ separate values are given for the north and south polar radii.
+
+ 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 = ( 6378.14 6378.14 6356.75 )
+
+
+Body Numbers 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
+
+
+ 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
+ 2000004 Asteroid Vesta
+ 2000216 Asteroid Kleopatra
+ 2000253 Asteroid Mathilde
+ 2000433 Asteroid Eros
+ 2004179 Asteroid Toutatis
+ 2025143 Asteroid Itokawa
+ 2431010 Asteroid Ida
+ 9511010 Asteroid Gaspra
+
+
+Orientation Constants for the Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+
+ 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. )
+
+ 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 unchanged in the 2006 IAU report.
+
+
+ Current values:
+
+ \begindata
+
+ BODY199_POLE_RA = ( 281.01 -0.033 0. )
+ BODY199_POLE_DEC = ( 61.45 -0.005 0. )
+ BODY199_PM = ( 329.548 6.1385025 0. )
+
+ BODY199_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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:
+
+ Old 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 )
+
+
+ Current values:
+
+ 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
+
+
+ Values are given for the epoch 2000 and are from the final row
+ of the above table, which is from [8]. As shown by the table
+ these values constitute a low-accuracy approximation for epochs
+ not close to 2000.
+
+ \begindata
+
+ BODY399_N_GEOMAG_CTR_DIPOLE_LON = ( 288.43 )
+ BODY399_N_GEOMAG_CTR_DIPOLE_LAT = ( 79.54 )
+
+ \begintext
+
+
+Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 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:
+
+ Values are from the 2003 IAU report.
+
+
+ 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 )
+
+
+
+ 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 = ( 284.95 870.5366420 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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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 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.
+
+
+ \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
+ 29.80 -52.1
+ 706.64 151413.4
+ 57.44 151413.4 )
+ \begintext
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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
+
+
+
+Pluto
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ BODY999_POLE_RA = ( 313.02 0. 0. )
+ BODY999_POLE_DEC = ( 9.09 0. 0. )
+ BODY999_PM = ( 236.77 -56.3623195 0. )
+ BODY999_LONG_AXIS = ( 0. )
+
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+
+Orientation constants for the satellites
+--------------------------------------------------------
+
+
+Satellites of Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 from the 2003 IAU report.
+
+
+ body502_pole_ra = ( 268.08 -0.009 0. )
+ body502_pole_dec = ( 64.51 0.003 0. )
+ body502_pm = ( 35.67 101.3747235 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 )
+
+
+ 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+ Enceladus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Tethys
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+ Dione
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Rhea
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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. 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
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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 )
+
+ \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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Phoebe
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body609_pole_ra = ( 355.00 0. 0. )
+ body609_pole_dec = ( 68.70 0. 0. )
+ body609_pm = ( 304.70 930.8338720 0. )
+ body609_long_axis = ( 0. )
+
+ 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 2006 IAU report.
+
+ Current values:
+
+ \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. 0.023 )
+ BODY610_NUT_PREC_DEC = ( 0. -0.183 0. 0. 0. 0. 0. 0. 0.001 )
+ BODY610_NUT_PREC_PM = ( 0. 1.613 0. 0. 0. 0. 0. 0. -0.023 )
+
+ \begintext
+
+
+
+ Epimetheus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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. 0.086 0. )
+ BODY611_NUT_PREC_DEC = ( -0.356 0. 0. 0. 0. 0. 0. 0.005 0. )
+ BODY611_NUT_PREC_PM = ( 3.133 0. 0. 0. 0. 0. 0. -0.086 0. )
+
+ \begintext
+
+
+
+ Helene
+
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 report [1] states that values for Nereid are not
+ given because Nereid is not in synchronous rotation with Neptune
+ (p. 167).
+
+
+
+ Naiad
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2003 IAU report.
+
+ body901_pole_ra = ( 313.02 0. 0. )
+ body901_pole_dec = ( 9.09 0. 0. )
+ body901_pm = ( 56.77 -56.3623195 0. )
+ body901_long_axis = ( 0. )
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+Orientation constants for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+19P/Borrelly
+
+
+ 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
+
+
+
+9P/Tempel 1
+
+
+ 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
+
+
+Vesta
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2000004_POLE_RA = ( 301. 0. 0. )
+ BODY2000004_POLE_DEC = ( 41. 0. 0. )
+ BODY2000004_PM = ( 292. 1617.332776 0. )
+ BODY2000004_LONG_AXIS = ( 0. )
+
+ \begintext
+
+Eros
+
+ Old values:
+
+ Values are unchanged in the 2006 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
+
+
+Itokawa
+
+
+ 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
+
+
+
+Ida
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+Gaspra
+
+ Old values:
+
+ Values are unchanged in the 2006 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
+
+
+
+
+
+
+
+
+
+
+Radii of Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Value for the Sun is from the [3], page K7.
+
+ \begindata
+
+ BODY10_RADII = ( 696000. 696000. 696000. )
+
+ \begintext
+
+
+Mercury
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY199_RADII = ( 2439.7 2439.7 2439.7 )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY299_RADII = ( 6051.8 6051.8 6051.8 )
+
+ \begintext
+
+
+Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY399_RADII = ( 6378.14 6378.14 6356.75 )
+
+ \begintext
+
+
+Mars
+
+
+ Old values:
+
+ body499_radii = ( 3397. 3397. 3375. )
+
+ Current values:
+
+
+ The IAU report gives separate values for the north and south
+ polar radii:
+
+ north: 3373.19
+ south: 3379.21
+
+ We use the average of these values 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 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY599_RADII = ( 71492 71492 66854 )
+
+ \begintext
+
+
+
+Saturn
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY699_RADII = ( 60268 60268 54364 )
+
+ \begintext
+
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY799_RADII = ( 25559 25559 24973 )
+
+ \begintext
+
+
+
+Neptune
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ (Values are for the 1 bar pressure level.)
+
+ \begindata
+
+ BODY899_RADII = ( 24764 24764 24341 )
+
+ \begintext
+
+
+
+Pluto
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY999_RADII = ( 1195 1195 1195 )
+
+ \begintext
+
+
+
+
+Radii of Satellites
+--------------------------------------------------------
+
+
+Moon
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY301_RADII = ( 1737.4 1737.4 1737.4 )
+
+ \begintext
+
+
+
+Satellites of Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY401_RADII = ( 13.4 11.2 9.2 )
+ BODY402_RADII = ( 7.5 6.1 5.2 )
+
+ \begintext
+
+
+
+Satellites of Jupiter
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY501_RADII = ( 1829.4 1819.3 1815.7 )
+ BODY502_RADII = ( 1564.13 1561.23 1560.93 )
+ BODY503_RADII = ( 2632.4 2632.29 2632.35 )
+ BODY504_RADII = ( 2409.4 2409.2 2409.3 )
+ 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 )
+
+ \begintext
+
+ 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.
+ \begindata
+
+ BODY516_RADII = ( 21.5 21.5 21.5 )
+
+ \begintext
+
+
+
+Satellites of Saturn
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body601_radii = ( 209.1 196.2 191.4 )
+ body602_radii = ( 256.3 247.3 244.6 )
+ body603_radii = ( 535.6 528.2 525.8 )
+ body604_radii = ( 560 560 560 )
+ body605_radii = ( 764 764 764 )
+ body606_radii = ( 2575 2575 2575 )
+ body607_radii = ( 164 130 107 )
+ body608_radii = ( 718 718 718 )
+ body609_radii = ( 115 110 105 )
+ 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) was given in the
+ 2003 IAU report:
+
+ body612_radii = ( 17.5 --- --- )
+
+ The mean radius was 16km; we used this radius for all three axes, as
+ we do for the satellites for which only the mean radius is available.
+
+
+ body612_radii = ( 16 16 16 )
+ 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 )
+
+
+
+ Current values:
+
+ \begindata
+
+ 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 )
+
+ \begintext
+
+ 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.
+
+
+ \begindata
+
+ 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 )
+
+ \begintext
+
+
+ For Pan, only a mean radius is given in the 2006 report.
+
+ \begindata
+
+ BODY618_RADII = ( 10 10 10 )
+
+ \begintext
+
+
+
+Satellites of Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 IAU report.
+
+ Current values:
+
+ The 2000 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 2000
+ 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 from the 2003 IAU report.
+
+ BODY901_RADII = ( 593 593 593 )
+
+ Current values:
+
+ \begindata
+
+ BODY901_RADII = ( 605 605 605 )
+
+ \begintext
+
+
+
+Radii for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+19P/Borrelly
+
+
+ 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
+
+
+
+Halley
+
+
+ Current values:
+
+ \begindata
+
+ BODY1000036_RADII = ( 8.0 4.0 4.0 )
+
+ \begintext
+
+
+
+9P/Tempel 1
+
+
+ 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
+
+
+81P/Wild 2
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY1000107_RADII = ( 2.7 1.9 1.5 )
+
+ \begintext
+
+
+Ceres
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000001_RADII = ( 487.3 487.3 454.7 )
+
+ \begintext
+
+
+Vesta
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000004_RADII = ( 289. 280. 229. )
+
+ \begintext
+
+
+Toutatis
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2004179_RADII = ( 2.13 1.015 0.85 )
+
+ \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 2006 report.
+
+
+Mathilde
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000253_RADII = ( 33. 24. 23. )
+
+ \begintext
+
+Eros
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000433_RADII = ( 17.0 5.5 5.5 )
+
+ \begintext
+
+
+Itokawa
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2025143_RADII = ( 0.535 0.294 0.209 )
+
+ \begintext
+
+
+
+Gaspra
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY9511010_RADII = ( 9.1 5.2 4.4 )
+
+ \begintext
+
+
+
+
+Ida
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2431010_RADII = ( 26.8 12.0 7.6 )
+
+ \begintext
+
+
+
+===========================================================================
+End of file pck00009.tpc
+===========================================================================
+
+
+
diff --git a/tests/pytests/data/f004a47/vikingAddendum003.ti b/tests/pytests/data/f004a47/vikingAddendum003.ti
new file mode 100644
index 0000000000000000000000000000000000000000..98d77dabf0b8c75725cc56d8e0d7e8f530da5fa2
--- /dev/null
+++ b/tests/pytests/data/f004a47/vikingAddendum003.ti
@@ -0,0 +1,23 @@
+\begindata
+INS-27001_TRANSX = ( 0.0, 0.0117647058823529, 0.0)
+INS-27001_TRANSY = ( 0.0, 0.0, 0.0117647058823529)
+INS-27001_ITRANSS = ( 0.0, 85.0, 0.0)
+INS-27001_ITRANSL = ( 0.0, 0.0, 85.0)
+
+INS-27002_TRANSX = ( 0.0, 0.0117647058823529, 0.0)
+INS-27002_TRANSY = ( 0.0, 0.0, 0.0117647058823529)
+INS-27002_ITRANSS = ( 0.0, 85.0, 0.0)
+INS-27002_ITRANSL = ( 0.0, 0.0, 85.0)
+
+\begintext
+These are the parameters for writing c-kernels. Isis will create ck
+with the same frame endpoints as the mission ck. For Viking1 the ck
+instrument frame is VO1_PLATFORM (-27000) and the ck reference frame
+is B1950 (2) or J2000 (1), depending on the ck used. The mdim2.0_rand
+ck is in J2000.
+
+\begindata
+INS-27001_CK_FRAME_ID=-27000
+INS-27001_CK_REFERENCE_ID=2
+INS-27002_CK_FRAME_ID=-27000
+INS-27002_CK_REFERENCE_ID=2
diff --git a/tests/pytests/data/f004a47/vo1_fict.tsc b/tests/pytests/data/f004a47/vo1_fict.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..ca6eab8889dbe1ae002356ae175ce3da73dc318f
--- /dev/null
+++ b/tests/pytests/data/f004a47/vo1_fict.tsc
@@ -0,0 +1,136 @@
+KPL/SCLK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "VO1_FICT.TSC"
+MISSION_NAME = VIKING
+SPACECRAFT_NAME = "VIKING ORBITER 1"
+DATA_SET_ID = "VO1/VO2-M-SPICE-6-V1.0"
+KERNEL_TYPE_ID = SCLK
+PRODUCT_ID = "VO1_FICT.TSC"
+PRODUCT_CREATION_TIME = 2000-04-21T10:53:20
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = {
+ PRIMARY_MISSION,
+ EXTENDED_MISSION,
+ CONTINUATION_MISSION,
+ SURVEY_MISSION
+ }
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = MARS
+INSTRUMENT_NAME = "N/A"
+NAIF_INSTRUMENT_ID = "N/A"
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = CLOCK_COEFFICIENTS
+ DESCRIPTION = "SCLK file implementing fictitious clock
+used to tag orientation data in the VO1 CK files. This SCLK file does NOT
+represent real Viking Orbiter 1 on-board clock but rather is a simple
+counter of milliseconds since 1 Jan 1976 00:00:00. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+Viking Orbiter 1 "fictitious" SCLK Kernel
+--------------------------------------------------------
+
+ This file contains the data necessary to convert between the
+ 'fictitious' Viking Orbiter 1 on-board clock times used as tags
+ for pointing instances in Viking Orbiter 1 CK files and ephemeris
+ time.
+
+ NAIF suggests that you do not modify this file. If you do modify
+ it, be sure to indicate this in the `Version' section below.
+
+
+Version
+--------------------------------------------------------
+
+ Version 1.0.1 -- April 20, 2000
+
+ Comments in the file were slightly reformatted and augmented.
+
+ Version 1.0.0 -- July 22, 1996
+
+
+Implementation notes
+--------------------------------------------------------
+
+ This SPICE SCLK file is constructed so that valid SCLK strings
+ are simply the number of seconds that have passed since the UTC
+ epoch 1 Jan 1976 00:00:00. Thus 288929292.827 simply represents
+ the epoch that occurs 288929292.827 seconds past the UTC epoch
+ 1 Jan 1976.
+
+ For all time, the clock runs at the same rate as Terrestrial
+ Dynamical Time (TDT). There is only one partition for this clock.
+
+ You must load this file into the kernel pool before using any
+ of the SPICELIB SCLK routines. The code fragment
+
+ CALL LDPOOL ( < name of this file > )
+
+ performs this task. To convert between ET and UTC, you will
+ also need to load a leapseconds kernel. The additional call
+ to LDPOOL,
+
+ CALL LDPOOL ( < name of your leapsecond file > )
+
+ will accomplish this. Note that you must supply the actual names
+ of the files used on your system as arguments to LDPOOL. Because
+ the file names are system dependent, we do not list them here.
+
+ For more information, consult your SPICELIB required reading
+ files. The following areas are covered:
+
+ SCLK system SCLK required reading
+ Time systems and conversion TIME required reading
+ Kernel pool KERNEL required reading
+
+
+Kernel data
+--------------------------------------------------------
+
+ \begindata
+
+ SCLK_KERNEL_ID = ( @22-JUL-1996 )
+
+ SCLK_DATA_TYPE_27 = ( 1 )
+
+ SCLK01_TIME_SYSTEM_27 = ( 2 )
+ SCLK01_N_FIELDS_27 = ( 2 )
+ SCLK01_MODULI_27 = ( 10000000000 1000 )
+ SCLK01_OFFSETS_27 = ( 0 0 )
+ SCLK01_OUTPUT_DELIM_27 = ( 1 )
+
+ SCLK_PARTITION_START_27 = ( 0.0000000000000E+00 )
+ SCLK_PARTITION_END_27 = ( 1.00000000E+14 )
+ SCLK01_COEFFICIENTS_27 = ( 0.00000000E+00
+ @01-JAN-1976-00:00:47.184
+ 1 )
+
+ \begintext
+
+
+Contact Information
+--------------------------------------------------------
+
+ Contact NAIF node of the Planetary Data System if you have any
+ questions regarding this SCLK file.
+
+ Charles H. Acton, Jr
+ (818)-354-3869
+ chuck.acton@jpl.nasa.gov
+
+ Boris V. Semenov
+ (818)-354-8136
+ boris.semenov@jpl.nasa.gov
diff --git a/tests/pytests/data/f004a47/vo1_fsc.tsc b/tests/pytests/data/f004a47/vo1_fsc.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..aa5d9a7c0ea464b9eb1da461c207a2de2c1927e2
--- /dev/null
+++ b/tests/pytests/data/f004a47/vo1_fsc.tsc
@@ -0,0 +1,237 @@
+KPL/SCLK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "VO1_FSC.TSC"
+MISSION_NAME = VIKING
+SPACECRAFT_NAME = "VIKING ORBITER 1"
+DATA_SET_ID = "VO1/VO2-M-SPICE-6-V1.0"
+KERNEL_TYPE_ID = SCLK
+PRODUCT_ID = "VO1_FSC.TSC"
+PRODUCT_CREATION_TIME = 2000-04-21T10:53:21
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = {
+ PRIMARY_MISSION,
+ EXTENDED_MISSION,
+ CONTINUATION_MISSION,
+ SURVEY_MISSION
+ }
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = MARS
+INSTRUMENT_NAME = "N/A"
+NAIF_INSTRUMENT_ID = "N/A"
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = CLOCK_COEFFICIENTS
+ DESCRIPTION = "SCLK file containing linear piecewise
+function representing VO1 FSC on-board clock. This function was generated as
+the result of VO1 image time tags restoration. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+Viking Orbiter 1 Reconstructed Frame Start Count (FSC) SCLK file
+--------------------------------------------------------
+
+ This file contain data necessary to convert a Viking Orbiter 1
+ FSC count to the ET time corresponding to it. These data are
+ based on the results of VO1 image times reconstruction done at
+ NAIF/JPL. The process of this reconstruction is described in
+ detail in the "VO Image Time Reconstruction" document.
+
+ Note that the main purpose of this file is to store the
+ reconstructed FSC counter; the on-board clock defined by the
+ function in this file was not used to time tag any of the
+ orientation data in CK files.
+
+ To avoid confusion with the other VO1 clock used for time tagging,
+ the FSC on-board clock in this file was assigned the NAIF ID
+ code -27999.
+
+
+Version
+--------------------------------------------------------
+
+ Version 1.0.1 -- April 20, 2000
+
+ Comments in the file were slightly reformatted and augmented.
+
+ Version 1.0.0 -- July 22, 1996
+
+
+Implementation notes
+--------------------------------------------------------
+
+ This SPICE SCLK file is constructed so that valid SCLK strings
+ are the eight digit VO1 FSC count associated with each VO1 image.
+ Note that the actual "image time" (the time of the beginning,
+ middle or the end of exposure) has a significant offset from
+ the FSC tick start time. This offset depends on the exposure
+ duration and is described in the "VO Image Time Reconstruction"
+ document.
+
+ You must load this file into the kernel pool before using any
+ of the SPICELIB SCLK routines. The code fragment
+
+ CALL LDPOOL ( < name of this file > )
+
+ performs this task. To convert between ET and UTC, you will also
+ need to load a leapseconds kernel. The additional call to LDPOOL,
+
+ CALL LDPOOL ( < name of your leapsecond file > )
+
+ will accomplish this. Note that you must supply the actual names
+ of the files used on your system as arguments to LDPOOL. Because
+ the file names are system dependent, we do not list them here.
+
+ For more information, consult your SPICELIB required reading
+ files. The following areas are covered:
+
+ SCLK system SCLK required reading
+ Time systems and conversion TIME required reading
+ Kernel pool KERNEL required reading
+
+
+Kernel data
+--------------------------------------------------------
+
+\begindata
+
+ SCLK_KERNEL_ID = ( @22-JUL-1996 )
+
+ SCLK_DATA_TYPE_27999 = ( 1 )
+ SCLK01_TIME_SYSTEM_27999 = ( 2 )
+ SCLK01_N_FIELDS_27999 = ( 1 )
+ SCLK01_MODULI_27999 = ( 60000000 )
+ SCLK01_OFFSETS_27999 = ( 25837050 )
+ SCLK01_OUTPUT_DELIM_27999 = ( 1 )
+
+ SCLK_PARTITION_START_27999 = (
+ 0
+ 231791
+ 644942
+ 1569121
+ 3367553
+ 5555717
+ 6396566
+ 7572950
+ 8087730
+ 9835672
+ 10866610
+ 11503583
+ 12217716
+ 13159619
+ 13679685
+ 14664700
+ 15449939
+ 16432925
+ 17479492
+ 17896518
+ 18344818
+ 20321730
+ 23280832
+ 24166658
+ 24262845
+ 24359029
+ 24609280
+ 25992950
+ 26522392
+ 27368930
+ 27915783
+ )
+
+ SCLK_PARTITION_END_27999 = (
+ 231791
+ 644942
+ 1569121
+ 3367553
+ 5555717
+ 6396566
+ 7572950
+ 8087730
+ 9835672
+ 10866610
+ 11503583
+ 12217716
+ 13159619
+ 13679685
+ 14664700
+ 15449939
+ 16432925
+ 17479492
+ 17896518
+ 18344818
+ 20321730
+ 23280832
+ 24166658
+ 24262845
+ 24359029
+ 24609280
+ 25992950
+ 26522392
+ 27368930
+ 27915783
+ 59999999
+ )
+
+ SCLK01_COEFFICIENTS_27999 = (
+
+ 0 -742936101.084011 4.480002320
+ 231791 -741897676.845143 4.480001506
+ 644942 -740046759.578601 4.480001685
+ 1569121 -735906436.111559 4.480001416
+ 3367553 -727849458.210550 4.480001972
+ 5555717 -718046479.059529 4.480002284
+ 6396566 -714279473.752967 4.480001816
+ 7572950 -709009271.245943 4.480001816
+ 8087730 -706703055.797485 4.480001869
+ 9835672 -698872272.708142 4.480001557
+ 10866610 -694253669.451953 4.480001151
+ 11503583 -691400029.539901 4.480000884
+ 12217716 -688200712.915836 4.480000934
+ 13159619 -683980986.490315 4.480000934
+ 13679685 -681651090.175512 4.480000934
+ 14664700 -677238222.129167 4.480000778
+ 15449939 -673720350.640383 4.480000830
+ 16432925 -669316572.195161 4.480000882
+ 17479492 -664627950.891482 4.480000922
+ 17896518 -662759673.743136 4.480000929
+ 18344818 -660751289.419364 4.480000581
+ 20321730 -651894716.843243 4.480001297
+ 23280832 -638637935.825957 4.480001191
+ 24166658 -634669434.296886 4.480000989
+ 24262845 -634238516.448398 4.480001715
+ 24359029 -633807611.943517 4.480001275
+ 24609280 -632686487.136533 4.480001142
+ 25992950 -626487643.963656 4.480001192
+ 26522392 -624115743.164982 4.480000986
+ 27368930 -620323251.820923 4.480001408
+ 27915783 -617873349.601991 4.480001089
+
+ )
+
+\begintext
+
+
+Contact Information
+--------------------------------------------------------
+
+ Contact NAIF node of the Planetary Data System if you have any
+ questions regarding this SCLK file.
+
+ Charles H. Acton, Jr
+ (818)-354-3869
+ chuck.acton@jpl.nasa.gov
+
+ Boris V. Semenov
+ (818)-354-8136
+ boris.semenov@jpl.nasa.gov
diff --git a/tests/pytests/data/f004a47/vo1_sedr_ck2_0_sliced_-27000.xc b/tests/pytests/data/f004a47/vo1_sedr_ck2_0_sliced_-27000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..71e8535b39eeb49512ba1fdde733bcfbed01e6be
--- /dev/null
+++ b/tests/pytests/data/f004a47/vo1_sedr_ck2_0_sliced_-27000.xc
@@ -0,0 +1,851 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+'VO1 PLATFORM ATTITUDE; CREATED BY BVS/NAIF; 2006-FEB-09 '
+BEGIN_ARRAY 1 830
+'VO1 ATT. BASED ON GEM AND SEDR FILES '
+'383F9F574^9'
+'384251F5D^9'
+'-6978'
+'2'
+'2'
+'1'
+830
+'CA965B2A89E4C^0'
+'-1294393B76A31A^0'
+'74CD97638987A8^0'
+'-667FFA8FFDAFC4^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'CB0193CF5439A^0'
+'-1235EDEA0A6DD3^0'
+'741359CF2F48A^0'
+'-6690537EF1F8E8^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'CB8639113D6618^0'
+'-11C0159EB60E12^0'
+'7329C313EF7794^0'
+'-66A56ADD6B6094^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'CC0ABC22E8FE1^0'
+'-1149F7DCECB019^0'
+'723EF767BC44BC^0'
+'-66B8DF77A0E3D^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'CCA813B03C7AD^0'
+'-10CCA4EBC68E52^0'
+'713A0CF436B66^0'
+'-66B58D70A6C3E4^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9C1021E72F785^0'
+'-30A8A36F477D8C^0'
+'AFAACFF6E7AD18^0'
+'-592EF5088A89D^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9C3E339F55DC2^0'
+'-3085B14103FB1^0'
+'AF82E56FB93EE8^0'
+'-593FEA96CCD92C^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9C3E32E2798D48^0'
+'-308568E06CDEB8^0'
+'AF830ABB3C7FF8^0'
+'-593FC9E3499E98^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9C36043B276778^0'
+'-308318B31DFF64^0'
+'AF8AA68A6EC79^0'
+'-594067A3277168^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9C2DAC40C8F968^0'
+'-30806A4B0A495A^0'
+'AF91E28CD03C08^0'
+'-59423BE12910A8^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9C2ACE9CBD185^0'
+'-30855BE6794DB2^0'
+'AF8E87EE73EDF^0'
+'-594B28087FEF64^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9C26E4331DCFC^0'
+'-3085420D12F88E^0'
+'AF9103856AD64^0'
+'-594D2D770EF02^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9C26E6FA26D1B^0'
+'-308591E7106F08^0'
+'AF90F3503C3508^0'
+'-594D1D160BD068^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9C26E4331DCFC^0'
+'-3085420D12F88E^0'
+'AF9103856AD64^0'
+'-594D2D770EF02^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9C2718D6237E1^0'
+'-3085F6F5D24C54^0'
+'AF90D89908DCB^0'
+'-594CC38380E96^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9C271880EF0498^0'
+'-3085A5D52E0CDE^0'
+'AF90E6AA0B2F38^0'
+'-594CD485D2C754^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9C2FAD57091248^0'
+'-30889057F6982E^0'
+'AF8918B7140178^0'
+'-594B94A6C1915C^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9BFD4D8DE739E8^0'
+'-30A8794A1DEC36^0'
+'AFB5D45877EC1^0'
+'-593A486E652D6C^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9BFD811B51F92^0'
+'-30A8F81F4B5B18^0'
+'AFB5897FF5EDF^0'
+'-593A3C872CE24^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9BF951A0B851D^0'
+'-30BCE9E7024646^0'
+'AFB92B24241E28^0'
+'-592F8392DA5DC4^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9BF91C3EB9D258^0'
+'-30BD5E9A52F7F4^0'
+'AFB932D7A68578^0'
+'-592F91FBD5E888^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'9BF951A0B851D^0'
+'-30BCE9E7024646^0'
+'AFB92B24241E28^0'
+'-592F8392DA5DC4^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CF549817F38^0'
+'-3A36AEBAC8FEDA^0'
+'BFAE842AC7A59^0'
+'-536EB5E4A91654^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CF9D101D80A8^0'
+'-3A37133CDF6428^0'
+'BFAE485B0EE3E8^0'
+'-536E8336A4F43^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CFB5780E2138^0'
+'-3A36932BAB95AC^0'
+'BFAE2D46811698^0'
+'-536EF30EDD53A8^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CF9D101D80A8^0'
+'-3A37133CDF6428^0'
+'BFAE485B0EE3E8^0'
+'-536E8336A4F43^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CFE687BFF32^0'
+'-3A37003505B468^0'
+'BFAE0B0504A3A^0'
+'-536EA5D1464E38^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87D02F1723C498^0'
+'-3A368C2496921A^0'
+'BFAE121F3DCAA8^0'
+'-536E705E1AF5AC^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CBED30CBED18^0'
+'-3A371FE610FE98^0'
+'BFAFE48988121^0'
+'-5370C7BA211594^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CC0AACDF33E^0'
+'-3A3721F2E4D186^0'
+'BFB01AC68926B8^0'
+'-537019B510605^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CC4DF9B94AB8^0'
+'-3A371F4FBEA326^0'
+'BFAFE3931DFCE8^0'
+'-53702CD4B95394^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CC0AACDF33E^0'
+'-3A3721F2E4D186^0'
+'BFB01AC68926B8^0'
+'-537019B510605^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CC4DF9B94AB8^0'
+'-3A371F4FBEA326^0'
+'BFAFE3931DFCE8^0'
+'-53702CD4B95394^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87C9F88612292^0'
+'-3A40D468506E14^0'
+'BFB151B774C848^0'
+'-5369E9550BF0DC^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CC044EF3ACB^0'
+'-3A494053DAE93A^0'
+'BFB0EAB94A004^0'
+'-53619EDE7BDF^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CC0610B6771^0'
+'-3A4A0B31F4F8E2^0'
+'BFB0D7FAF9FCD^0'
+'-53613948665FD8^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CC35570AC3E8^0'
+'-3A49AD5EDE2B12^0'
+'BFB0C86D264D18^0'
+'-536151A3232B34^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CC0610B6771^0'
+'-3A4A0B31F4F8E2^0'
+'BFB0D7FAF9FCD^0'
+'-53613948665FD8^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CC35570AC3E8^0'
+'-3A49AD5EDE2B12^0'
+'BFB0C86D264D18^0'
+'-536151A3232B34^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'87CC6867FFC6B8^0'
+'-3A49F1B357DD12^0'
+'BFB0807BD2209^0'
+'-536174187EA0F^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
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+END_ARRAY 1 830
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /home/pgiroux/Desktop/f004a47.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/f004a47/vo1_v10.tf b/tests/pytests/data/f004a47/vo1_v10.tf
new file mode 100644
index 0000000000000000000000000000000000000000..0ce54d5df53a7c50b1257e28f7d0ac9fb7ad9ffb
--- /dev/null
+++ b/tests/pytests/data/f004a47/vo1_v10.tf
@@ -0,0 +1,470 @@
+KPL/FK
+
+Viking Orbiter 1 Frames Kernel
+===============================================================================
+
+ This frame kernel contains the complete set of frame definitions for
+ the Viking Orbiter 1 (VO1) spacecraft including definitions for the
+ spacecraft frame, instrument platform frame, and science instrument
+ frames.
+
+
+Version and Date
+-------------------------------------------------------------------------------
+
+ Version 1.0 -- December 1, 2005 -- Boris Semenov, NAIF
+
+ Initial Release.
+
+
+References
+-------------------------------------------------------------------------------
+
+ 1. ``Frames Required Reading''
+
+ 2. ``Kernel Pool Required Reading''
+
+ 3. ``C-Kernel Required Reading''
+
+ 4. VO1 Supplemental Experiment Data Record (SEDR) file, 1976-1980.
+
+ 5. Thomas C. Duxbury/JPL, March-July, 1996
+
+
+Contact Information
+-------------------------------------------------------------------------------
+
+ Boris V. 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/CSPICE/ICY routine FURNSH loads
+ a kernel file into the pool as shown below.
+
+ CALL FURNSH ( 'frame_kernel_name' ) SPICELIB/FORTRAN
+
+ furnsh_c ( "frame_kernel_name" ); CSPICE/C
+
+ cspice_furnsh, "frame_kernel_name" ICY/IDL
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+VO1 Frames
+-------------------------------------------------------------------------------
+
+ The following VO1 frames are defined in this kernel file:
+
+ Name Relative to Type NAIF ID
+ ====================== =================== ============ =======
+
+ Spacecraft frame:
+ -----------------
+ VO1_SPACECRAFT rel.to B1950 CK -27900
+
+ Instrument Platform frame:
+ --------------------------
+ VO1_PLATFORM rel.to B1950 CK -27000
+
+ Science Instrument frames:
+ --------------------------
+ VO1_VISA rel.to PLATFORM FIXED -27001
+ VO1_VISA_TD rel.to PLATFORM FIXED -27011
+ VO1_VISB rel.to PLATFORM FIXED -27002
+ VO1_VISB_TD rel.to PLATFORM FIXED -27012
+ VO1_IRTM rel.to PLATFORM FIXED -27003
+ VO1_MAWD rel.to PLATFORM FIXED -27004
+
+
+VO1 Frames Hierarchy
+-------------------------------------------------------------------------------
+
+ The diagram below shows VO1 frames hierarchy:
+
+
+ "B1950" INERTIAL
+ +-----------------------------------------------------------+
+ | | | |
+ | <--pck | <--ck | <--ck | <--pck
+ | | | |
+ V V | V
+ "IAU_MARS" "V01_SPACECRAFT" | "IAU_EARTH"
+ ----------- ---------------- | ------------
+ |
+ |
+ V
+ "VO1_PLATFORM"
+ +---------------------------------------------------------+
+ | | | | | |
+ | <--fixed | <--fixed fixed--> | | | | <--fixed
+ | | | | | |
+ V V V | | V
+ "VO1_IRTM" "VO1_MAWD" "VO1_VISA" | | "VO1_VISB"
+ ---------- ---------- ---------- | | ----------
+ | |
+ | |
+ fixed--> | | <--fixed
+ | |
+ V V
+ "VO1_VISA_TD" "VO1_VISB_TD"
+ ------------- -------------
+
+
+Spacecraft Bus Frame
+-------------------------------------------------------------------------------
+
+ The spacecraft frame is defined as follows:
+
+ [TBD]
+
+ This diagram illustrates the spacecraft bus frame:
+
+ [TBD]
+
+ Since the S/C bus attitude with respect to an inertial frame is
+ provided by a C kernel (see [3] for more information), this frame is
+ defined as a CK-based frame.
+
+ \begindata
+
+ FRAME_VO1_SPACECRAFT = -27900
+ FRAME_-27900_NAME = 'VO1_SPACECRAFT'
+ FRAME_-27900_CLASS = 3
+ FRAME_-27900_CLASS_ID = -27900
+ FRAME_-27900_CENTER = -27
+ CK_-27900_SCLK = -27
+ CK_-27900_SPK = -27
+
+ \begintext
+
+
+Instrument Platform Frame
+-------------------------------------------------------------------------------
+
+ The instrument platform frame is defined as follows:
+
+ [TBD]
+
+ This diagram illustrates the instrument platform frame:
+
+ [TBD]
+
+ Since the platform attitude with respect to an inertial frame is
+ provided by a C kernel (see [3] for more information), this frame is
+ defined as a CK-based frame.
+
+ \begindata
+
+ FRAME_VO1_PLATFORM = -27000
+ FRAME_-27000_NAME = 'VO1_PLATFORM'
+ FRAME_-27000_CLASS = 3
+ FRAME_-27000_CLASS_ID = -27000
+ FRAME_-27000_CENTER = -27
+ CK_-27000_SCLK = -27
+ CK_-27000_SPK = -27
+
+ \begintext
+
+
+VISA and VISB Frames
+-------------------------------------------------------------------------------
+
+ The frames for the Visual Imaging Subsystem Camera A (VISA) and
+ Camera B (VISB) -- VO1_VISA and VO1_VISB -- are defined as follows:
+
+ - Z axis is along the camera boresight;
+
+ - X axis is along detector lines and points toward the right
+ side of the image;
+
+ - Y axis completes the right hand frame;
+
+ - the origin of this frame is located at the camera focal point.
+
+ This diagram illustrates the camera frames:
+
+ [TBD]
+
+ Since the cameras were rigidly mounted on the instrument platform
+ their frames are defined as fixed offset frames with respect to the
+ platform frame.
+
+ The camera orientation with respect to the platform was specified in
+ [4] as the following three rotation angles:
+
+ T pl-cam = R (RASTER_ORIENTATION) R (CONE) R (-CROSS_CONE)
+ Z Y X
+
+ with the following angle values for each of the two cameras:
+
+ VISA:
+
+ CROSS_CONE = -0.707350, deg
+ CONE = -0.007580, deg
+ RASTER_ORIENTATION = 89.735690, deg
+
+ VISB:
+
+ CROSS_CONE = 0.681000, deg
+ CONE = -0.032000, deg
+ RASTER_ORIENTATION = 90.022800, deg
+
+ These angles are used in the frame definition below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the camera to the platform frame -- see [1].)
+
+ \begindata
+
+ FRAME_VO1_VISA = -27001
+ FRAME_-27001_NAME = 'VO1_VISA'
+ FRAME_-27001_CLASS = 4
+ FRAME_-27001_CLASS_ID = -27001
+ FRAME_-27001_CENTER = -27
+ TKFRAME_-27001_SPEC = 'ANGLES'
+ TKFRAME_-27001_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-27001_ANGLES = ( -0.707350, 0.007580, -89.735690 )
+ TKFRAME_-27001_AXES = ( 1, 2, 3 )
+ TKFRAME_-27001_UNITS = 'DEGREES'
+
+ FRAME_VO1_VISB = -27002
+ FRAME_-27002_NAME = 'VO1_VISB'
+ FRAME_-27002_CLASS = 4
+ FRAME_-27002_CLASS_ID = -27002
+ FRAME_-27002_CENTER = -27
+ TKFRAME_-27002_SPEC = 'ANGLES'
+ TKFRAME_-27002_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-27002_ANGLES = ( 0.681000, 0.032000, -90.022800 )
+ TKFRAME_-27002_AXES = ( 1, 2, 3 )
+ TKFRAME_-27002_UNITS = 'DEGREES'
+
+ \begintext
+
+ Thomas Duxbury provided a different set of angle values for the cameras
+ (see [5]):
+
+ VISA:
+
+ CROSS_CONE = -0.707400, deg
+ CONE = -0.007600, deg
+ RASTER_ORIENTATION = 89.735400, deg
+
+ VISB:
+
+ CROSS_CONE = 0.681300, deg
+ CONE = -0.032100, deg
+ RASTER_ORIENTATION = 90.083900, deg
+
+ To make this alignment solution available, two more frames parallel
+ to the camera frames and including the ``_TB'' suffix in the name
+ and defined below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the camera to the platform frame -- see [1].)
+
+ \begindata
+
+ FRAME_VO1_VISA_TD = -27011
+ FRAME_-27011_NAME = 'VO1_VISA_TD'
+ FRAME_-27011_CLASS = 4
+ FRAME_-27011_CLASS_ID = -27011
+ FRAME_-27011_CENTER = -27
+ TKFRAME_-27011_SPEC = 'ANGLES'
+ TKFRAME_-27011_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-27011_ANGLES = ( -0.707400, 0.007600, -89.735400 )
+ TKFRAME_-27011_AXES = ( 1, 2, 3 )
+ TKFRAME_-27011_UNITS = 'DEGREES'
+
+ FRAME_VO1_VISB_TD = -27012
+ FRAME_-27012_NAME = 'VO1_VISB_TD'
+ FRAME_-27012_CLASS = 4
+ FRAME_-27012_CLASS_ID = -27012
+ FRAME_-27012_CENTER = -27
+ TKFRAME_-27012_SPEC = 'ANGLES'
+ TKFRAME_-27012_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-27012_ANGLES = ( 0.681300, 0.032100, -90.083900 )
+ TKFRAME_-27012_AXES = ( 1, 2, 3 )
+ TKFRAME_-27012_UNITS = 'DEGREES'
+
+ \begintext
+
+
+IRTM Frame
+-------------------------------------------------------------------------------
+
+ The frame for the Infrared Thermal Mapper -- VO1_IRTM -- is defined
+ as follows:
+
+ [TBD]
+
+ This diagram illustrates the IRTM frame:
+
+ [TBD]
+
+ Since the IRTM instrument was rigidly mounted on the instrument
+ platform its frame is defined as fixed offset frames with respect to
+ the platform frame.
+
+ The instrument orientation with respect to the platform can be
+ specified using the following three rotation angles:
+
+ T pl-cam = R (RASTER_ORIENTATION) R (CONE) R (-CROSS_CONE)
+ Z Y X
+
+ with the nominal angle values:
+
+ CROSS_CONE = 0.0, deg
+ CONE = 0.0, deg
+ RASTER_ORIENTATION = 90.0, deg
+
+ These angles are used in the frame definition below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the instrument to the platform frame -- see
+ [1].)
+
+ \begindata
+
+ FRAME_VO1_IRTM = -27003
+ FRAME_-27003_NAME = 'VO1_IRTM'
+ FRAME_-27003_CLASS = 4
+ FRAME_-27003_CLASS_ID = -27003
+ FRAME_-27003_CENTER = -27
+ TKFRAME_-27003_SPEC = 'ANGLES'
+ TKFRAME_-27003_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-27003_ANGLES = ( 0.0, 0.0, -90.0 )
+ TKFRAME_-27003_AXES = ( 1, 2, 3 )
+ TKFRAME_-27003_UNITS = 'DEGREES'
+
+ \begintext
+
+
+MAWD Frame
+-------------------------------------------------------------------------------
+
+ The frame for the Mars Atmosphere Water Detector (MAWD) -- VO1_MAWD
+ -- is defined as follows:
+
+ [TBD]
+
+ This diagram illustrates the MAWD frame:
+
+ [TBD]
+
+ Since the MAWD instrument was rigidly mounted on the instrument
+ platform its frame is defined as fixed offset frames with respect to
+ the platform frame.
+
+ The instrument orientation with respect to the platform can be
+ specified using the following three rotation angles:
+
+ T pl-cam = R (RASTER_ORIENTATION) R (CONE) R (-CROSS_CONE)
+ Z Y X
+
+ with the nominal angle values:
+
+ CROSS_CONE = 0.0, deg
+ CONE = 0.0, deg
+ RASTER_ORIENTATION = 90.0, deg
+
+ These angles are used in the frame definition below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the instrument to the platform frame -- see
+ [1].)
+
+ \begindata
+
+ FRAME_VO1_MAWD = -27004
+ FRAME_-27004_NAME = 'VO1_MAWD'
+ FRAME_-27004_CLASS = 4
+ FRAME_-27004_CLASS_ID = -27004
+ FRAME_-27004_CENTER = -27
+ TKFRAME_-27004_SPEC = 'ANGLES'
+ TKFRAME_-27004_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-27004_ANGLES = ( 0.0, 0.0, -90.0 )
+ TKFRAME_-27004_AXES = ( 1, 2, 3 )
+ TKFRAME_-27004_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Viking Orbiter 1 NAIF ID Codes -- Definition Section
+========================================================================
+
+ This section contains name to NAIF ID mappings for the VO1. Once the
+ contents of this file is loaded into the KERNEL POOL, these mappings
+ become available within SPICE, making it possible to use names
+ instead of ID code in the high level SPICE routine calls.
+
+ Spacecraft and its structures:
+ ------------------------------
+
+ VIKING ORBITER 1 -27
+ VO1 -27
+
+ VO1_SPACECRAFT_BUS -27900
+ VO1_SC_BUS -27900
+ VO1_SPACECRAFT -27900
+
+ VO1_INSTRUMENT_PLATFORM -27000
+ VO1_PLATFORM -27000
+
+ Science Instruments:
+ --------------------
+
+ VO1_VISA -27001
+ VO1_VISB -27002
+
+ VO1_IRTM -27003
+
+ VO1_MAWD -27004
+
+ The mappings summarized in this table are implemented by the keywords
+ below.
+
+ \begindata
+
+ NAIF_BODY_NAME += ( 'VIKING ORBITER 1' )
+ NAIF_BODY_CODE += ( -27 )
+
+ NAIF_BODY_NAME += ( 'VO1' )
+ NAIF_BODY_CODE += ( -27 )
+
+ NAIF_BODY_NAME += ( 'VO1_SPACECRAFT_BUS' )
+ NAIF_BODY_CODE += ( -27900 )
+
+ NAIF_BODY_NAME += ( 'VO1_SC_BUS' )
+ NAIF_BODY_CODE += ( -27900 )
+
+ NAIF_BODY_NAME += ( 'VO1_SPACECRAFT' )
+ NAIF_BODY_CODE += ( -27900 )
+
+ NAIF_BODY_NAME += ( 'VO1_INSTRUMENT_PLATFORM' )
+ NAIF_BODY_CODE += ( -27000 )
+
+ NAIF_BODY_NAME += ( 'VO1_PLATFORM' )
+ NAIF_BODY_CODE += ( -27000 )
+
+ NAIF_BODY_NAME += ( 'VO1_VISA' )
+ NAIF_BODY_CODE += ( -27001 )
+
+ NAIF_BODY_NAME += ( 'VO1_VISB' )
+ NAIF_BODY_CODE += ( -27002 )
+
+ NAIF_BODY_NAME += ( 'VO1_IRTM' )
+ NAIF_BODY_CODE += ( -27003 )
+
+ NAIF_BODY_NAME += ( 'VO1_MAWD' )
+ NAIF_BODY_CODE += ( -27004 )
+
+ \begintext
diff --git a/tests/pytests/data/f004b65/f004b65_0.xsp b/tests/pytests/data/f004b65/f004b65_0.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..54652f23fcb2d432d0fca3d0d7563ec758dfcbfb
--- /dev/null
+++ b/tests/pytests/data/f004b65/f004b65_0.xsp
@@ -0,0 +1,706 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
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+END_ARRAY 1 39
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+'7DDBCC90E7843C^-9'
+'774943F3640A08^-9'
+'1065E2090F5E39^-9'
+'-1290556FF903A2^-A'
+'-3C91ADF4CCCCCC^-A'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'27943FDC85DD28^-2'
+'-141906E3926759^-3'
+'-E872A5DEACE968^-5'
+'66AD29B4E7EE7^-6'
+'11E7971C2CFCCB^-6'
+'19D0994651BF32^-8'
+'-27716C571C1D86^-8'
+'-3B7F3356476CBC^-9'
+'3647BCD6C5BF2A^-A'
+'46FC3645625134^-A'
+'1E323A09265D3C^-A'
+'-BB0271801527^-C'
+'-A0FEC2B50F7578^-B'
+'-5773E^-B'
+'0^0'
+'-1387EA04A1A5A1^-2'
+'-22DCA00D0A5FBE^-3'
+'-3C361982E54E12^-5'
+'12974D0A7CAA16^-5'
+'D25CAB6230D67^-7'
+'-14D5441A988592^-7'
+'-31C53CC4A30266^-8'
+'167590357689E^-A'
+'12F6CE9BEC45B^-9'
+'5F3F71D602F9B8^-A'
+'3DC7E1624BAF2^-B'
+'-138F14C77D1C68^-A'
+'-B0907F82E00278^-B'
+'1824D^-B'
+'0^0'
+'E^1'
+'A^1'
+'D^1'
+'D^1'
+'-2BFE0014E41F52^8'
+'1C603557F18^2'
+'38C06AAFE3^2'
+'5520A007D48^2'
+'7180D55FC6^2'
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+'AA41400FA9^2'
+'C6A175679A8^2'
+'E301AABF8C^2'
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+'15482801F52^3'
+'170E2B577438^3'
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+'1FEC3C02EFB^3'
+'1176C8A23BB7BC^4'
+'-940BE7973C9E18^0'
+'-3F94A89944FA82^3'
+'27EF6CD718E7C6^1'
+'6ABE553FFE10A4^3'
+'2FF2C375E1E19E^1'
+'-6AF34B019C737C^-2'
+'5842A4512CF3D8^-4'
+'1AE60EB2AD7DA7^-4'
+'-14EC6E431DEEAA^-6'
+'-1C647C819BA785^-6'
+'-2FA811A6D48E14^-8'
+'4378D5098B1B3^-8'
+'1085C727634F5F^-9'
+'-14932A9AA63525^-9'
+'1AA8AFA7955F26^-A'
+'17DF7CA2E8BA2F^-A'
+'-5CD54^-B'
+'0^0'
+'0^0'
+'0^0'
+'186D321415B062^-2'
+'-1AE7B2EADFCF4E^-3'
+'-71253E61D8DCA^-5'
+'F8F9191C25739^-6'
+'97B2991C4A2288^-7'
+'-183E8A0F68E3CF^-7'
+'-1C3D983CE3A362^-8'
+'4F6F6A379396C4^-9'
+'70CA4B2CE58878^-A'
+'-395115BDE76348^-A'
+'-192CE78D7F971^-B'
+'8B2B2^-B'
+'0^0'
+'0^0'
+'0^0'
+'-2909E89D6039A6^-2'
+'-20D228F5F40BFE^-3'
+'91F31EF79941C^-5'
+'144E972122357F^-5'
+'-6F89B42F7D0E44^-7'
+'-23319AB71BBC5C^-7'
+'98B3240221F37^-9'
+'770C2F652EC7B^-9'
+'-670C5299C66108^-A'
+'-3871D5E3015374^-A'
+'133C69E682DF3C^-A'
+'78A8E^-B'
+'-34DFC^-B'
+'C292^-C'
+'0^0'
+'E^1'
+'B^1'
+'B^1'
+'D^1'
+'-2BFDFF31E27492^8'
+'1C603557F18^2'
+'38C06AAFE3^2'
+'5520A007D48^2'
+'7180D55FC6^2'
+'8DE10AB7B78^2'
+'AA41400FA9^2'
+'C6A175679A8^2'
+'E301AABF8C^2'
+'FF61E0177D8^2'
+'11BC2156F6F^3'
+'138224AC7608^3'
+'15482801F52^3'
+'170E2B577438^3'
+'18D42EACF35^3'
+'1C603557F18^3'
+'10CA1606687D98^4'
+'-F084F3EFBCD988^0'
+'-1BAE6F78DE9C63^3'
+'28E77CD3F79784^1'
+'9420444AC44F58^3'
+'2D40A80523B9F^1'
+'-64961E97B09CB^-2'
+'11FBFC4DA1BD08^-3'
+'167DDF8DF01FD3^-4'
+'-E0BDB10F8C5F18^-6'
+'-1518F1BFFAF596^-6'
+'1A7080BEC7A47A^-7'
+'2DAA8292A64442^-8'
+'-5107D017A6FDE^-9'
+'-A9B8336DB8592^-A'
+'-4817086F643BF^-B'
+'E9D8^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'A768B491D5EBE^-3'
+'-1C1C147C778344^-3'
+'140C5CB67C6699^-5'
+'107CBB4F9E6859^-5'
+'-4280A675C3CF2^-7'
+'-1A9C9CFC4A67B8^-7'
+'D29C66AF6355C^-9'
+'4F60A485B54258^-9'
+'-1AB080C5B6551F^-A'
+'-9A4B6^-B'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'-37A1812E588B9^-2'
+'-19C4A7A4228AAE^-3'
+'1163409B8C6D55^-4'
+'CA57E7F20E4DD8^-6'
+'-146F34CB6F4AEB^-6'
+'-11B33EC7277DE1^-7'
+'3202FCCBEF2F3^-8'
+'3418301BF5F7B8^-9'
+'-93031D2DEC777^-A'
+'-1427C4956D38D^-A'
+'-B599A^-B'
+'2E74A197D20C4^-B'
+'0^0'
+'0^0'
+'0^0'
+'C^1'
+'A^1'
+'9^1'
+'B^1'
+'-2BFDFE16205F22^8'
+'1C603557F18^2'
+'38C06AAFE3^2'
+'5520A007D48^2'
+'7180D55FC6^2'
+'8DE10AB7B78^2'
+'AA41400FA9^2'
+'C6A175679A8^2'
+'E301AABF8C^2'
+'FF61E0177D8^2'
+'11BC2156F6F^3'
+'138224AC7608^3'
+'15482801F52^3'
+'170E2B577438^3'
+'18D42EACF35^3'
+'1A9A32027268^3'
+'F8478FE99C543^3'
+'-158307F49D5A69^1'
+'11D7348475383^3'
+'290ADE5EBCC4D4^1'
+'C3F8C253AF0BC8^3'
+'28F0A5199BD012^1'
+'-557053DB609B08^-2'
+'1C3C7A8CA9AA3^-3'
+'AE75CB63EE6158^-5'
+'-143995D31646DB^-5'
+'-6170EB789200C^-8'
+'20390C4866EADC^-7'
+'-143ABB24B057C9^-8'
+'-58F2A7CC28BE78^-9'
+'9A4CCF4CA9016^-A'
+'19C3CF7909BC4^-A'
+'-7D044^-B'
+'-DCB4^-C'
+'0^0'
+'0^0'
+'0^0'
+'-60A3C490ED624^-3'
+'-1840924CE2C4A1^-3'
+'981EE8DB4B5678^-5'
+'996CF991598D8^-6'
+'-EAA270A68A03D^-7'
+'-69DC8CE32202E4^-8'
+'268BB83425528C^-8'
+'-517158F5CB2D6^-A'
+'-A6C7168DB6552^-A'
+'9BF1618^-B'
+'56CFDD^-B'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'-438FD27941FA48^-2'
+'-D5F37AB582B4D8^-4'
+'14893E291E638E^-4'
+'-10F9618147DF76^-6'
+'-1432807934F3FE^-6'
+'D96D0A1E2E391^-8'
+'25F7D442213F86^-8'
+'-46A24222654638^-9'
+'-726BF30430AF9^-A'
+'2217736A92C73^-A'
+'19B92^-B'
+'-2EA68^-B'
+'-76BC^-C'
+'0^0'
+'0^0'
+'D^1'
+'B^1'
+'A^1'
+'C^1'
+'-2BFDFBDE9C3444^8'
+'38C06AAFE3^2'
+'7180D55FC6^2'
+'AA41400FA9^2'
+'E301AABF8C^2'
+'11BC2156F6F^3'
+'15482801F52^3'
+'18D42EACF35^3'
+'1C603557F18^3'
+'1E2638AD7098^3'
+'1FEC3C02EFB^3'
+'21B23F586EC8^3'
+'237842ADEDE^3'
+'253E46036CF8^3'
+'27044958EC1^3'
+'28CA4CAE6B28^3'
+'BD658485F5D81^3'
+'-1EBBC341D1982B^1'
+'6A97DC2D4B1B2C^3'
+'268C0F53834436^1'
+'113EAFB4C16F68^4'
+'1F242B55B582BB^1'
+'-2FE33B775F79DA^-2'
+'38C3C26F4B1984^-3'
+'-1A76B56B445D6C^-4'
+'-40A2234B493AA^-5'
+'D3E1E6EE869E98^-6'
+'-6DC448F679489^-7'
+'-5A393082FD1728^-7'
+'14145256598EB7^-7'
+'1946C24DC0E467^-8'
+'-1C146E7EA13A8B^-8'
+'3B1A4B210B565C^-9'
+'27D4D5E444443^-9'
+'-BDD0483F1565C^-A'
+'-D180FC^-A'
+'0^0'
+'-1ADD7F8B18AC5E^-2'
+'-1404D85FE805BD^-3'
+'2C95474FFDACD^-4'
+'-1E232A91C155FB^-5'
+'-621E86C755BEB^-6'
+'17EE9243616981^-6'
+'-93C9AEA13D64A^-8'
+'-F46F1735B2D84^-8'
+'36A2D8D1B2BB9C^-8'
+'6BDB16B64C4D8C^-9'
+'-67EEB18133702C^-9'
+'A9D3CFF4A9799^-A'
+'FA2631^-A'
+'128669^-A'
+'0^0'
+'-45CAD8D934DC2^-2'
+'C3824460B4EDD8^-4'
+'2A3BC4D5456B98^-4'
+'-55FCB133996818^-5'
+'E235B2467E142^-7'
+'1BBEA54862944^-6'
+'-4B0537303BCEE4^-7'
+'-6DC7CDDB1B20C^-8'
+'599E561EC7A5F^-8'
+'-962619419F9658^-9'
+'-593EBD334279CC^-9'
+'229C0AB29A6F78^-9'
+'ACD89C^-A'
+'-30B294^-A'
+'0^0'
+'E^1'
+'D^1'
+'D^1'
+'D^1'
+'-2BFE0511CD7FB6^8'
+'-2BFE02A188E9F6^8'
+'-2BFE0130A63498^8'
+'-2BFE0014E41F22^8'
+'-2BFDFF31E2747E^8'
+'-2BFDFE16205F06^8'
+'-2BFDFBDE9C341A^8'
+'7^1'
+END_ARRAY 4 505
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /home/pgiroux/Desktop/f004b65/f004b65_0.bsp LOG FILE
+
+; Created 2019-09-30/11:09:12.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /home/pgiroux/Desktop/f004b65/f004b65_0.bsp
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/spk/mar097.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 4, 10, 499
+ BEGIN_TIME = 1976 AUG 12 00:57:58.590
+ END_TIME = 1976 AUG 12 01:44:54.265
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/viking2/kernels/spk/vo2_rcon.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -30
+ BEGIN_TIME = 1976 AUG 12 00:57:58.590
+ END_TIME = 1976 AUG 12 01:44:54.265
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/f004b65/f004b65_isis3.lbl b/tests/pytests/data/f004b65/f004b65_isis3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..c0f4dfc4b386e831a7d43659d60954eaffed5148
--- /dev/null
+++ b/tests/pytests/data/f004b65/f004b65_isis3.lbl
@@ -0,0 +1,103 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 1204
+ TileLines = 1056
+
+ Group = Dimensions
+ Samples = 1204
+ Lines = 1056
+ Bands = 1
+ End_Group
+
+ Group = Pixels
+ Type = UnsignedByte
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftName = VIKING_ORBITER_2
+ InstrumentId = VISUAL_IMAGING_SUBSYSTEM_CAMERA_A
+ TargetName = MARS
+ StartTime = 1976-08-12T01:28:18
+ ExposureDuration = 0.033940 <seconds>
+ SpacecraftClockCount = 46570746
+ FloodModeId = ON
+ GainModeId = HIGH
+ OffsetModeId = ON
+ End_Group
+
+ Group = Archive
+ DataSetId = VO1/VO2-M-VIS-2-EDR-V2.0
+ ProductId = 004B65
+ MissonPhaseName = PRIMARY_MISSION
+ ImageNumber = 46570746
+ OrbitNumber = 4
+ End_Group
+
+ Group = BandBin
+ FilterName = GREEN
+ FilterId = 5
+ Center = 0.53 <micrometers>
+ Width = 0.1 <micrometers>
+ End_Group
+
+ Group = Kernels
+ NaifFrameCode = -30001
+ CameraVersion = 1
+ End_Group
+
+ Group = Reseaus
+ Line = (2, 6, 9, 12, 14, 15, 17, 18, 20, 21, 22, 131, 132, 135, 138,
+ 140, 142, 143, 145, 146, 147, 149, 150, 260, 263, 265, 267,
+ 269, 271, 272, 274, 275, 277, 278, 389, 390, 393, 395, 397,
+ 398, 400, 401, 403, 404, 406, 407, 518, 520, 523, 524, 526,
+ 528, 529, 531, 532, 534, 536, 647, 648, 650, 652, 654, 656,
+ 657, 658, 660, 661, 663, 664, 776, 778, 780, 782, 783, 785,
+ 786, 788, 789, 791, 793, 905, 906, 908, 910, 911, 913, 914,
+ 915, 917, 918, 920, 921, 1034, 1035, 1037, 1039, 1040, 1041,
+ 1043, 1044, 1045, 1046, 1049)
+ Sample = (25, 142, 259, 375, 491, 606, 722, 838, 953, 1069, 1184, 25,
+ 84, 200, 316, 432, 548, 663, 778, 894, 1009, 1124, 1181, 25,
+ 142, 258, 374, 489, 604, 720, 835, 950, 1065, 1180, 26, 84,
+ 200, 316, 431, 546, 662, 777, 892, 1007, 1122, 1179, 26, 142,
+ 258, 373, 489, 604, 719, 834, 949, 1064, 1179, 26, 84, 200,
+ 316, 431, 546, 661, 776, 891, 1006, 1121, 1177, 25, 142, 257,
+ 373, 488, 603, 718, 833, 948, 1063, 1177, 24, 83, 199, 315,
+ 430, 545, 660, 775, 890, 1005, 1120, 1177, 23, 140, 256, 371,
+ 487, 602, 717, 832, 947, 1062, 1176)
+ Type = (1, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6)
+ Valid = (0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0)
+ Template = $viking2/reseaus/vo2.visa.template.cub
+ Status = Nominal
+ End_Group
+End_Object
+
+Object = Label
+ Bytes = 65536
+End_Object
+
+Object = History
+ Name = IsisCube
+ StartByte = 1336961
+ Bytes = 428
+End_Object
+
+Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 1337389
+ Bytes = 2052
+End_Object
+End
diff --git a/tests/pytests/data/f004b65/f004b65_pds3.lbl b/tests/pytests/data/f004b65/f004b65_pds3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..359c0ac2d359abaa9fc0ca6300ebbb3aabd4bfea
--- /dev/null
+++ b/tests/pytests/data/f004b65/f004b65_pds3.lbl
@@ -0,0 +1,1633 @@
+CCSD3ZF0000100000001NJPL3IF0PDS200000001 = SFDU_LABEL
+/* FILE FORMAT AND LENGTH */
+RECORD_TYPE = VARIABLE_LENGTH
+RECORD_BYTES = 1204
+FILE_RECORDS = 2177
+LABEL_RECORDS = 61
+/* POINTERS TO START RECORDS OF MAJOR OBJECTS IN FILE */
+^IMAGE_HISTOGRAM = 62
+^ENCODING_HISTOGRAM = 63
+^ENGINEERING_TABLE = 65
+^LINE_HEADER_TABLE = 66
+^IMAGE = 1122
+/* IMAGE DESCRIPTION */
+DATA_SET_ID = 'VO1/VO2-M-VIS-2-EDR-V2.0'
+SPACECRAFT_NAME = VIKING_ORBITER_2
+MISSION_PHASE_NAME = PRIMARY_MISSION
+TARGET_NAME = MARS
+IMAGE_ID = '004B65'
+IMAGE_NUMBER = 46570746
+IMAGE_TIME = 1976-08-12T01:28:18Z
+EARTH_RECEIVED_TIME = 1976-08-13T01:00:48Z
+ORBIT_NUMBER = 4
+INSTRUMENT_NAME = VISUAL_IMAGING_SUBSYSTEM_CAMERA_A
+GAIN_MODE_ID = HIGH
+FLOOD_MODE_ID = ON
+OFFSET_MODE_ID = ON
+FILTER_NAME = GREEN
+EXPOSURE_DURATION = 0.033940 <SECONDS>
+NOTE = "HIGH RESOLUTION MAPPING SEQUENCE OF
+ THE B2 LANDING SITE"
+/* DESCRIPTION OF THE OBJECTS CONTAINED IN FILE */
+OBJECT = IMAGE_HISTOGRAM
+ ITEMS = 256
+ ITEM_TYPE = VAX_INTEGER
+ ITEM_BITS = 32
+END_OBJECT
+OBJECT = ENCODING_HISTOGRAM
+ ITEMS = 511
+ ITEM_TYPE = VAX_INTEGER
+ ITEM_BITS = 32
+END_OBJECT
+OBJECT = ENGINEERING_TABLE
+ ROWS = 1
+ ROW_BYTES = 152
+CCSD3ZF0000100000001NJPL3IF0PDS200000001 = SFDU_LABEL
+
+OBJECT = ENGINEERING_TABLE_STRUCTURE
+ INTERCHANGE_FORMAT = BINARY
+ BYTES = 152
+ NOTE = "This structure describes the format of
+ the engineering record that is included in each image file.
+ This record contains the first 152 bytes of data extracted from
+ the Mission and Test Imaging System (MTIS) header record on each
+ file of an imaging EDR tape."
+
+ OBJECT = COLUMN
+ NAME = MTIS_RECORD_ID
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 1
+ BYTES = 2
+ DESCRIPTION = "Mission and Test Imaging System record
+ ID."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PHYSICAL_SEQUENCE_NUMBER
+ DATA_TYPE = VAX_UNSIGNED_INTEGER
+ START_BYTE = 3
+ BYTES = 2
+ DESCRIPTION = "Physical sequence number on Experiment
+ Data Record tape. Not used."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LOGICAL_SEQUENCE_NUMBER
+ DATA_TYPE = VAX_UNSIGNED_INTEGER
+ START_BYTE = 5
+ BYTES = 2
+ DESCRIPTION = "Logical sequence number on Experiment
+ Data Record tape. Not used."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_ERT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 7
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time year and day
+ value. Time of first line segment in the file containing valid
+ data. This field is NOT stored in VAX least significant byte
+ first format."
+
+ OBJECT = BIT_COLUMN
+ NAME = FIRST_ERT_YEAR
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 1
+ BITS = 7
+ DESCRIPTION = "Earth Received Time year of century
+ (1900). Time of first line record in the file containing valid
+ data. This field is often incorrect."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FIRST_ERT_DAY
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 7
+ BITS = 9
+ DESCRIPTION = "Earth Received Time day of year."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_ERT_MINUTE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 9
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time minute of day."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_ERT_MILLISECOND
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 11
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time millisecond of
+ minute."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_ERT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 13
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time year and day
+ value. Time of last line segment of the file containing valid
+ data."
+
+ OBJECT = BIT_COLUMN
+ NAME = LAST_ERT_YEAR
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 1
+ BITS = 7
+ DESCRIPTION = "Earth Received Time year of century
+ (1900). This field is often incorrect."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = LAST_ERT_DAY
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 8
+ BITS = 9
+ DESCRIPTION = "Earth Received Time day of year."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_ERT_MINUTE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 15
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time minute of day."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_ERT_MILLISECOND
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 17
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time millisecond of
+ minute."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_FDS_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 19
+ BYTES = 4
+ DESCRIPTION = "Flight Data Subsystem count for the
+ first line segment of the file containing valid data. Note that
+ this may not correspond to the FDS count for line 1, segment 1."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_FDS_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 23
+ BYTES = 4
+ DESCRIPTION = "Flight Data Subsystem count for the
+ last line segment of the file containing valid data. Note that
+ this may not correspond to the FDS count for segment 7 of line
+ 1056."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = EDR_ID
+ DATA_TYPE = CHARACTER
+ START_BYTE = 27
+ BYTES = 6
+ DESCRIPTION = "Tape reel identifier of the original
+ EDR tape for this image."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = EDR_FILE_NUMBER
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 33
+ BYTES = 2
+ DESCRIPTION = "File number of image on original EDR
+ tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FILL_IN
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 34
+ BYTES = 1
+ DESCRIPTION = "Value used to fill in missing samples
+ (always zero)."
+ END_OBJECT = COLUMN
+ OBJECT = COLUMN
+ NAME = TRACK_PRESENCE_MASK
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 36
+ BYTES = 1
+ DESCRIPTION = "Mask indicating which tracks are
+ present in the image. The nominal value is HEX 7F, indicating
+ that all seven tracks are present."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = AVERAGE_PIXEL
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 37
+ BYTES = 2
+ DESCRIPTION = "Average pixel value for image."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_1
+ DATA_TYPE = CHARACTER
+ START_BYTE = 39
+ BYTES = 4
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MINIMUM_SNR
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 43
+ BYTES = 2
+ FACTOR = 0.03125
+ DESCRIPTION = "Minimum signal to noise ratio. The
+ minimum noise level found for the scan lines. Divide by 32 to
+ get the actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MAXIMUM_SNR
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 45
+ BYTES = 2
+ FACTOR = 0.03125
+ DESCRIPTION = "Maximum signal to noise ratio. The
+ maximum noise level found for the scan lines. Divide by 32 to
+ get the actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_2
+ DATA_TYPE = CHARACTER
+ START_BYTE = 47
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MINIMUM_AGC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 49
+ BYTES = 2
+ FACTOR = 0.0625
+ DESCRIPTION = "Automatic gain control minimum.
+ Divide by 16 to get actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MAXIMUM_AGC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 51
+ BYTES = 2
+ FACTOR = 0.0625
+ DESCRIPTION = "Automatic gain control maximum.
+ Divide by 16 to get actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_3
+ DATA_TYPE = CHARACTER
+ START_BYTE = 53
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 55
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that contain some valid data (maximum is 7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FULLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 57
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that were fully synchronized (maximum is 7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PARTLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 59
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that were partly synchronized (maximum is 7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI0_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 61
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 0 (maximum is 7 x 1056).
+ DQI0 indicates bad data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI1_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 63
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 1 (maximum is 7 x 1056).
+ DQI1 means SNR low, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI2_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 65
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 2 (maximum is 7 x 1056).
+ DQI2 means SNR good, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI3_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 67
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 3 (maximum is 7 x 1056).
+ DQI3 means SNR low, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI4_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 69
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 4 (maximum is 7 x 1056).
+ DQI4 means SNR good, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FDS_CORRECTIONS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 71
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with corrected FDS counts."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PNERROR_CORRECTIONS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 73
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with corrected pseudonoise codes."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = ADJUSTED_PNERROR_CORRECTIONS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 75
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with corrected pseudonoise codes adjusted based on the
+ number of line segments processed versus the total in a full
+ image (7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNREADABLE_RECORDS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 77
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that could not be read from the Master Data Record tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LOGICAL_SEQUENCE_BREAKS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 79
+ BYTES = 2
+ DESCRIPTION = "Total number of breaks in logical
+ sequence number in reading the System/Master Data Record tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DATA_BREAKS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 81
+ BYTES = 2
+ DESCRIPTION = "Total number of breaks in data
+ sequence in reading the System/Master Data Record tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_4
+ DATA_TYPE = CHARACTER
+ START_BYTE = 83
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINES
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 85
+ BYTES = 2
+ DESCRIPTION = "Total number of lines in the file that
+ contain some valid data (nominal is 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FULL_LINES
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 87
+ BYTES = 2
+ DESCRIPTION = "Number of lines in the file that are
+ composed of seven line segments."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PARTIAL_LINES
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 89
+ BYTES = 2
+ DESCRIPTION = "Total number of line records in the
+ file that contain some valid data but are not composed of seven
+ line segments."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_LINE_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 91
+ BYTES = 2
+ DESCRIPTION = "First line in image containing valid
+ data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_LINE_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 93
+ BYTES = 2
+ DESCRIPTION = "Last line in image containing valid
+ data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_5
+ DATA_TYPE = CHARACTER
+ START_BYTE = 95
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = IMAGE_ID
+ DATA_TYPE = CHARACTER
+ START_BYTE = 97
+ BYTES = 6
+ DESCRIPTION = "Image identifier (PICNO) for this
+ image, formatted OOOSNN, where OOO is orbit number, S is
+ spacecraft identifier (A for Viking Orbiter 1 prime and extended
+ missions; B for Viking Orbiter 2; and S for Viking Orbiter 1
+ Survey mission)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VRP_RUN_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 103
+ BYTES = 2
+ DESCRIPTION = "Viking Reconstruction Processing run
+ number."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DISK_ID
+ DATA_TYPE = CHARACTER
+ START_BYTE = 105
+ BYTES = 6
+ DESCRIPTION = "MTIS disk identifier of the original
+ EDR file for this image."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_6
+ DATA_TYPE = CHARACTER
+ START_BYTE = 111
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = TRANSMITTED_CODE_WORD1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 113
+ BYTES = 2
+ DESCRIPTION = "Transmitted command code word for the
+ image."
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ START_BIT = 1
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Set to 1 if data not present for the
+ following measurements."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ START_BIT = 3
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Data quality indicator associated with
+ code word values. Where: 0 is bad data; 1 is SNR low, GCF block
+ error; 2 is SNR good, GCF block bad; 3 is SNR low, GCF block
+ good; 4 is SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = CATHODE_CURRENT_FLAG
+ START_BIT = 7
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Cathode current off (0) or on (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = GAIN_FLAG
+ START_BIT = 8
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Gain mode low (0) or high (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = LIGHT_FLOOD_FLAG
+ START_BIT = 9
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Light flood off (0) or on (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FILTER_STEP
+ START_BIT = 10
+ BITS = 2
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Filter step indicator."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = EXPOSURE_CODE
+ START_BIT = 12
+ BITS = 5
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Exposure interval code."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = TRANSMITTED_CODE_WORD2
+ DATA_TYPE = INTEGER
+ START_BYTE = 115
+ BYTES = 2
+ DESCRIPTION = "Transmitted command code word 2 for
+ this image."
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ START_BIT = 1
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Set to 1 if data not present for the
+ following measurements."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ START_BIT = 3
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Data quality indicator associated with
+ code word values. where: 0 is bad data; 1 is SNR low, GCF block
+ error; 2 is SNR good, GCF block bad; 3 is SNR low, GCF block
+ good; 4 is SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FILTER_NUMBER
+ START_BIT = 10
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Filter number: where 1 is blue; 2 is
+ minus blue; 3 is violet; 4 is clear; 5 is green; and 6 is red."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = CAMERA_SERIAL_NUMBER
+ START_BIT = 13
+ BITS = 4
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Visual Imaging Subsystem camera serial
+ number."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = RECEIVED_CODE_WORD1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 117
+ BYTES = 2
+ DESCRIPTION = "Received command code word for the
+ image."
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ START_BIT = 1
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Set to 1 if data not present for the
+ following measurements."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ START_BIT = 3
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Data quality indicator associated with
+ code word values. where: 0 is bad data; 1 is SNR low, GCF block
+ error; 2 is SNR good, GCF block bad; 3 is SNR low, GCF block
+ good; 4 is SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = CATHODE_CURRENT_FLAG
+ START_BIT = 7
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Cathode current (beam) off (0) or on
+ (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = GAIN_FLAG
+ START_BIT = 8
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Gain mode low (0) or high (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = LIGHT_FLOOD_FLAG
+ START_BIT = 9
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Light flood off (0) or on (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FILTER_STEP
+ START_BIT = 10
+ BITS = 2
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Filter step."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = EXPOSURE_CODE
+ START_BIT = 12
+ BITS = 5
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Exposure interval code."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS50_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 121
+ BYTES = 2
+ DESCRIPTION = "Plus 50 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS15_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 123
+ BYTES = 2
+ DESCRIPTION = "Plus 15 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS12_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 125
+ BYTES = 2
+ DESCRIPTION = "Plus 12 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS5_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 127
+ BYTES = 2
+ DESCRIPTION = "Plus 5 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_MINUS15_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 129
+ BYTES = 2
+ DESCRIPTION = "Minus 15 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_MINUS23_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 131
+ BYTES = 2
+ DESCRIPTION = "Minus 23 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_AVERAGE_VIDEO
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 133
+ BYTES = 2
+ DESCRIPTION = "Average video."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = POWER_CONVERTER_INPUT_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 135
+ BYTES = 2
+ DESCRIPTION = "Power converter input current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = CATHODE_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 137
+ BYTES = 2
+ DESCRIPTION = "Cathode current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = CATHODE_VOLTAGE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 139
+ BYTES = 2
+ DESCRIPTION = "Cathode voltage."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FILAMENT_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 141
+ BYTES = 2
+ DESCRIPTION = "Filament current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FRAME_SWEEP_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 143
+ BYTES = 2
+ DESCRIPTION = "Frame sweep current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_SWEEP_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 145
+ BYTES = 2
+ DESCRIPTION = "Line sweep current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = GRID3_VOLTAGE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 147
+ BYTES = 2
+ DESCRIPTION = "Grid 3 voltage."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FOCUS_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 149
+ BYTES = 2
+ DESCRIPTION = "Focus current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DIGITAL_LADDER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 151
+ BYTES = 2
+ DESCRIPTION = "Digital ladder."
+ END_OBJECT = COLUMN
+
+END_OBJECT = ENGINEERING_TABLE_STRUCTURE
+
+END
+END_OBJECT
+OBJECT = LINE_HEADER_TABLE
+ ROWS = 1056
+ ROW_BYTES = 62
+CCSD3ZF0000100000001NJPL3IF0PDS200000001 = SFDU_LABEL
+
+OBJECT = LINE_HEADER_TABLE_STRUCTURE
+ INTERCHANGE_FORMAT = BINARY
+ BYTES = 62
+ NOTE = "Viking Orbiter Image Line-header
+ Structure. This label describes the structure of the 62-bytes
+ extracted from the end of each image line."
+
+ OBJECT = COLUMN
+ NAME = FDS_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 1
+ BYTES = 4
+ DESCRIPTION = "Flight Data Subsystem (FDS) clock
+ count."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 5
+ BYTES = 2
+ DESCRIPTION = "Flight Data Subsystem line number,
+ extracted from the telemetry record header information."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FILL_IN
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 7
+ BYTES = 1
+ DESCRIPTION = "Value used to fill in missing samples
+ (always zero)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = TRACK_PRESENCE_MASK
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 8
+ BYTES = 1
+ DESCRIPTION = "Mask indicating which tracks are
+ present in this line. The nominal value is HEX 7F, indicating
+ that all seven tracks are present."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = AVERAGE_PIXEL
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 9
+ BYTES = 2
+ DESCRIPTION = "Average pixel value for this line."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 11
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ line that contain some valid data (maximum is 7)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FULLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 13
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ that were fully synchronized (maximum is 7)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PARTLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 15
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ that were partly synchronized (maximum is 7)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI0_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 17
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 0 (maximum is 7), indicating
+ bad data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI1_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 19
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 1 (maximum is 7), indicating
+ SNR low, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI2_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 21
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 2 (maximum is 7), indicating
+ SNR good, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI3_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 23
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 3 (maximum is 7), indicating
+ SNR low, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI4_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 25
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 4 (maximum is 7), indicating
+ SNR good, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 27
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 29
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT2
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 31
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK2
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 33
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT3
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 35
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK3
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 37
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT4
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 39
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK4
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 41
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT5
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 43
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK5
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 45
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT6
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 47
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK6
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 49
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT7
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 51
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK7
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 53
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = EMBEDDED_SCIENCE_DATA
+ ITEMS = 7
+ DATA_TYPE = INTEGER
+ START_BYTE = 55
+ ITEM_BYTES = 1
+ DESCRIPTION = "Embedded low rate science data from
+ seven segments."
+ END_OBJECT = COLUMN
+
+END_OBJECT = LINE_HEADER_TABLE_STRUCTURE
+
+END
+END_OBJECT
+OBJECT = IMAGE
+ ENCODING_TYPE = HUFFMAN_FIRST_DIFFERENCE
+ LINES = 1056
+ LINE_SAMPLES = 1204
+ SAMPLE_TYPE = UNSIGNED_INTEGER
+ SAMPLE_BITS = 8
+ SAMPLE_BIT_MASK = 2#11111110#
+ CHECKSUM = 200755970
+END_OBJECT
+END
diff --git a/tests/pytests/data/f004b65/naif0012.tls b/tests/pytests/data/f004b65/naif0012.tls
new file mode 100644
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/f004b65/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/f004b65/pck00009.tpc b/tests/pytests/data/f004b65/pck00009.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..bfadaab2b26817327189ff3173e9609f49dedc9d
--- /dev/null
+++ b/tests/pytests/data/f004b65/pck00009.tpc
@@ -0,0 +1,3639 @@
+KPL/PCK
+
+
+P_constants (PcK) SPICE kernel file
+===========================================================================
+
+ By: Nat Bachman (NAIF) 2010 March 3
+
+
+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/IAG
+ 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
+
+
+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 and planets.
+ Additional items included in this section:
+
+ - Earth north geomagnetic centered dipole values
+ for epochs 1945-2000
+
+ - Mars prime meridian offset "lambda_a"
+
+ -- Orientation constants for satellites
+
+ -- Orientation constants for asteroids Eros, Gaspra, Ida,
+ Itokawa, and Vesta
+
+ -- Orientation constants for comets 19P/Borrelly
+ and 9P/Tempel 1
+
+
+ Radii of Bodies
+ ---------------
+
+ -- Radii of Sun and planets
+
+ -- Radii of satellites, where available
+
+ -- Radii of asteroids Ceres, Eros, Gaspra, Ida, Itokawa,
+ Mathilde, Toutatis, and Vesta.
+
+ -- Radii of comets 19P/Borrelly, Halley, 9P/Tempel 1,
+ and 81P/Wild 2
+
+
+
+Version Description
+--------------------------------------------------------
+
+ This file was created on March 3, 2010. This version
+ incorporates data from reference [1].
+
+ This file contains size, shape, and orientation data for all
+ objects described by the previous version of the file, except
+ for Kleopatra: a shape model for this body is not provided in [1]
+ because, according to this source, it had been "modeled from
+ low resolution radar data, and cannot be mapped from those
+ data."
+
+ New objects covered by this file but not the previous
+ version are:
+
+ 19P/Borrelly
+ Halley
+ 9P/Tempel 1
+ 81P/Wild 2
+ Ceres
+ Itokawa
+ Mathilde
+ Toutatis
+
+
+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, and version description section if you modify
+ this file.
+
+Known Limitations and Caveats
+
+ Accuracy
+ --------
+
+ In general, the orientation models given here are claimed by the
+ IAU/IAG 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]) 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. 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 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. A more
+ accurate approximation can be obtained by using both the NAIF
+ lunar frame kernel and the binary lunar orientation PCK file,
+ which 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
+ J2000 epoch 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].
+
+
+ Mars prime meridian offset
+ --------------------------
+
+ The Mars prime meridian offset given by [5] is not used by
+ SPICE geometry software for computations involving the shape
+ of Mars (for example, in sub-observer point or surface intercept
+ computations). The value 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 only planets for which such terms are used are
+ Jupiter and Neptune. Use of trigonometric polynomial terms for
+ natural satellites is and has been supported for all SPICE Toolkit
+ versions.
+
+ 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
+--------------------------------------------------------
+
+ The sources for the constants listed in this file are:
+
+
+ [1] 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."
+
+ [2] Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F.,
+ Cruikshank, D.P., Hilton, J.L., Keller, H.U., Oberst, J.,
+ Simon, J.L., Stooke, P., Tholen, D.J., and Thomas, P.C.
+ "Report of the IAU/IAG Working Group on Cartographic
+ Coordinates and Rotational Elements of the Planets and
+ Satellites: 2003."
+
+ [3] 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.
+
+ [4] Nautical Almanac Office, United States Naval Observatory,
+ H.M. Nautical Almanac Office, Royal Greenwich
+ Observatory, Jet Propulsion Laboratory, Bureau des
+ Longitudes, and The Time Service and Astronomy
+ Departments, United States Naval Observatory (1992).
+ "Explanatory Supplement to the Astronomical Almanac," P.
+ Kenneth Seidelmann, ed. University Science Books, 20
+ Edgehill Road, Mill Valley, CA 9494.
+
+ [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.
+
+
+ Most values are from [1]. All exceptions are
+ commented where they occur in this file. The exceptions are:
+
+
+ -- Radii for the Sun are from [3].
+
+ -- 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
+ [8]. The article [6] was used to check most of
+ these values, and the values were also re-computed from
+ the 9th generation IGRF [9] by Nat Bachman.
+
+ -- The Mars prime meridian offset angle is from [5].
+
+
+ "Old values" listed are from the SPICE P_constants file
+ pck00008.tpc dated September 21, 2004. Most of these values came
+ from the 2003 IAU report [2].
+
+
+
+
+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 = ( 6378.14 6378.14 6356.75 )
+
+ Any blanks preceding or following keyword names, values and equal
+ signs are ignored.
+
+ Assignments may be spread over multiple lines, for example:
+
+ BODY399_RADII = ( 6378.14
+ 6378.14
+ 6356.75 )
+
+ 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 2006 IAU/IAG 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 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 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, 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: 2006 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 = ( 284.95 870.5366420 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 term is zero for all bodies except Mars. It represents the
+ angular offset between the meridian containing the longest axis of
+ the triaxial ellipsoid used to model a body's surface and the
+ prime meridian of the body.
+
+ 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 2006 IAU report does
+ not use any other models, except in the case of Mars, where
+ separate values are given for the north and south polar radii.
+
+ 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 = ( 6378.14 6378.14 6356.75 )
+
+
+Body Numbers 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
+
+
+ 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
+ 2000004 Asteroid Vesta
+ 2000216 Asteroid Kleopatra
+ 2000253 Asteroid Mathilde
+ 2000433 Asteroid Eros
+ 2004179 Asteroid Toutatis
+ 2025143 Asteroid Itokawa
+ 2431010 Asteroid Ida
+ 9511010 Asteroid Gaspra
+
+
+Orientation Constants for the Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+
+ 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. )
+
+ 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 unchanged in the 2006 IAU report.
+
+
+ Current values:
+
+ \begindata
+
+ BODY199_POLE_RA = ( 281.01 -0.033 0. )
+ BODY199_POLE_DEC = ( 61.45 -0.005 0. )
+ BODY199_PM = ( 329.548 6.1385025 0. )
+
+ BODY199_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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:
+
+ Old 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 )
+
+
+ Current values:
+
+ 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
+
+
+ Values are given for the epoch 2000 and are from the final row
+ of the above table, which is from [8]. As shown by the table
+ these values constitute a low-accuracy approximation for epochs
+ not close to 2000.
+
+ \begindata
+
+ BODY399_N_GEOMAG_CTR_DIPOLE_LON = ( 288.43 )
+ BODY399_N_GEOMAG_CTR_DIPOLE_LAT = ( 79.54 )
+
+ \begintext
+
+
+Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 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:
+
+ Values are from the 2003 IAU report.
+
+
+ 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 )
+
+
+
+ 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 = ( 284.95 870.5366420 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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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 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.
+
+
+ \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
+ 29.80 -52.1
+ 706.64 151413.4
+ 57.44 151413.4 )
+ \begintext
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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
+
+
+
+Pluto
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ BODY999_POLE_RA = ( 313.02 0. 0. )
+ BODY999_POLE_DEC = ( 9.09 0. 0. )
+ BODY999_PM = ( 236.77 -56.3623195 0. )
+ BODY999_LONG_AXIS = ( 0. )
+
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+
+Orientation constants for the satellites
+--------------------------------------------------------
+
+
+Satellites of Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 from the 2003 IAU report.
+
+
+ body502_pole_ra = ( 268.08 -0.009 0. )
+ body502_pole_dec = ( 64.51 0.003 0. )
+ body502_pm = ( 35.67 101.3747235 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 )
+
+
+ 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+ Enceladus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Tethys
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+ Dione
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Rhea
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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. 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
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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 )
+
+ \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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Phoebe
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body609_pole_ra = ( 355.00 0. 0. )
+ body609_pole_dec = ( 68.70 0. 0. )
+ body609_pm = ( 304.70 930.8338720 0. )
+ body609_long_axis = ( 0. )
+
+ 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 2006 IAU report.
+
+ Current values:
+
+ \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. 0.023 )
+ BODY610_NUT_PREC_DEC = ( 0. -0.183 0. 0. 0. 0. 0. 0. 0.001 )
+ BODY610_NUT_PREC_PM = ( 0. 1.613 0. 0. 0. 0. 0. 0. -0.023 )
+
+ \begintext
+
+
+
+ Epimetheus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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. 0.086 0. )
+ BODY611_NUT_PREC_DEC = ( -0.356 0. 0. 0. 0. 0. 0. 0.005 0. )
+ BODY611_NUT_PREC_PM = ( 3.133 0. 0. 0. 0. 0. 0. -0.086 0. )
+
+ \begintext
+
+
+
+ Helene
+
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 report [1] states that values for Nereid are not
+ given because Nereid is not in synchronous rotation with Neptune
+ (p. 167).
+
+
+
+ Naiad
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2003 IAU report.
+
+ body901_pole_ra = ( 313.02 0. 0. )
+ body901_pole_dec = ( 9.09 0. 0. )
+ body901_pm = ( 56.77 -56.3623195 0. )
+ body901_long_axis = ( 0. )
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+Orientation constants for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+19P/Borrelly
+
+
+ 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
+
+
+
+9P/Tempel 1
+
+
+ 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
+
+
+Vesta
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2000004_POLE_RA = ( 301. 0. 0. )
+ BODY2000004_POLE_DEC = ( 41. 0. 0. )
+ BODY2000004_PM = ( 292. 1617.332776 0. )
+ BODY2000004_LONG_AXIS = ( 0. )
+
+ \begintext
+
+Eros
+
+ Old values:
+
+ Values are unchanged in the 2006 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
+
+
+Itokawa
+
+
+ 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
+
+
+
+Ida
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+Gaspra
+
+ Old values:
+
+ Values are unchanged in the 2006 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
+
+
+
+
+
+
+
+
+
+
+Radii of Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Value for the Sun is from the [3], page K7.
+
+ \begindata
+
+ BODY10_RADII = ( 696000. 696000. 696000. )
+
+ \begintext
+
+
+Mercury
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY199_RADII = ( 2439.7 2439.7 2439.7 )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY299_RADII = ( 6051.8 6051.8 6051.8 )
+
+ \begintext
+
+
+Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY399_RADII = ( 6378.14 6378.14 6356.75 )
+
+ \begintext
+
+
+Mars
+
+
+ Old values:
+
+ body499_radii = ( 3397. 3397. 3375. )
+
+ Current values:
+
+
+ The IAU report gives separate values for the north and south
+ polar radii:
+
+ north: 3373.19
+ south: 3379.21
+
+ We use the average of these values 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 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY599_RADII = ( 71492 71492 66854 )
+
+ \begintext
+
+
+
+Saturn
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY699_RADII = ( 60268 60268 54364 )
+
+ \begintext
+
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY799_RADII = ( 25559 25559 24973 )
+
+ \begintext
+
+
+
+Neptune
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ (Values are for the 1 bar pressure level.)
+
+ \begindata
+
+ BODY899_RADII = ( 24764 24764 24341 )
+
+ \begintext
+
+
+
+Pluto
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY999_RADII = ( 1195 1195 1195 )
+
+ \begintext
+
+
+
+
+Radii of Satellites
+--------------------------------------------------------
+
+
+Moon
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY301_RADII = ( 1737.4 1737.4 1737.4 )
+
+ \begintext
+
+
+
+Satellites of Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY401_RADII = ( 13.4 11.2 9.2 )
+ BODY402_RADII = ( 7.5 6.1 5.2 )
+
+ \begintext
+
+
+
+Satellites of Jupiter
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY501_RADII = ( 1829.4 1819.3 1815.7 )
+ BODY502_RADII = ( 1564.13 1561.23 1560.93 )
+ BODY503_RADII = ( 2632.4 2632.29 2632.35 )
+ BODY504_RADII = ( 2409.4 2409.2 2409.3 )
+ 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 )
+
+ \begintext
+
+ 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.
+ \begindata
+
+ BODY516_RADII = ( 21.5 21.5 21.5 )
+
+ \begintext
+
+
+
+Satellites of Saturn
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body601_radii = ( 209.1 196.2 191.4 )
+ body602_radii = ( 256.3 247.3 244.6 )
+ body603_radii = ( 535.6 528.2 525.8 )
+ body604_radii = ( 560 560 560 )
+ body605_radii = ( 764 764 764 )
+ body606_radii = ( 2575 2575 2575 )
+ body607_radii = ( 164 130 107 )
+ body608_radii = ( 718 718 718 )
+ body609_radii = ( 115 110 105 )
+ 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) was given in the
+ 2003 IAU report:
+
+ body612_radii = ( 17.5 --- --- )
+
+ The mean radius was 16km; we used this radius for all three axes, as
+ we do for the satellites for which only the mean radius is available.
+
+
+ body612_radii = ( 16 16 16 )
+ 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 )
+
+
+
+ Current values:
+
+ \begindata
+
+ 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 )
+
+ \begintext
+
+ 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.
+
+
+ \begindata
+
+ 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 )
+
+ \begintext
+
+
+ For Pan, only a mean radius is given in the 2006 report.
+
+ \begindata
+
+ BODY618_RADII = ( 10 10 10 )
+
+ \begintext
+
+
+
+Satellites of Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 IAU report.
+
+ Current values:
+
+ The 2000 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 2000
+ 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 from the 2003 IAU report.
+
+ BODY901_RADII = ( 593 593 593 )
+
+ Current values:
+
+ \begindata
+
+ BODY901_RADII = ( 605 605 605 )
+
+ \begintext
+
+
+
+Radii for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+19P/Borrelly
+
+
+ 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
+
+
+
+Halley
+
+
+ Current values:
+
+ \begindata
+
+ BODY1000036_RADII = ( 8.0 4.0 4.0 )
+
+ \begintext
+
+
+
+9P/Tempel 1
+
+
+ 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
+
+
+81P/Wild 2
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY1000107_RADII = ( 2.7 1.9 1.5 )
+
+ \begintext
+
+
+Ceres
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000001_RADII = ( 487.3 487.3 454.7 )
+
+ \begintext
+
+
+Vesta
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000004_RADII = ( 289. 280. 229. )
+
+ \begintext
+
+
+Toutatis
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2004179_RADII = ( 2.13 1.015 0.85 )
+
+ \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 2006 report.
+
+
+Mathilde
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000253_RADII = ( 33. 24. 23. )
+
+ \begintext
+
+Eros
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000433_RADII = ( 17.0 5.5 5.5 )
+
+ \begintext
+
+
+Itokawa
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2025143_RADII = ( 0.535 0.294 0.209 )
+
+ \begintext
+
+
+
+Gaspra
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY9511010_RADII = ( 9.1 5.2 4.4 )
+
+ \begintext
+
+
+
+
+Ida
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2431010_RADII = ( 26.8 12.0 7.6 )
+
+ \begintext
+
+
+
+===========================================================================
+End of file pck00009.tpc
+===========================================================================
+
+
+
diff --git a/tests/pytests/data/f004b65/vikingAddendum003.ti b/tests/pytests/data/f004b65/vikingAddendum003.ti
new file mode 100644
index 0000000000000000000000000000000000000000..b84e8a81eddcfdd2ab1919dab123bf5f08d5399a
--- /dev/null
+++ b/tests/pytests/data/f004b65/vikingAddendum003.ti
@@ -0,0 +1,23 @@
+\begindata
+INS-30001_TRANSX = ( 0.0, 0.0117647058823529, 0.0)
+INS-30001_TRANSY = ( 0.0, 0.0, 0.0117647058823529)
+INS-30001_ITRANSS = ( 0.0, 85.0, 0.0)
+INS-30001_ITRANSL = ( 0.0, 0.0, 85.0)
+
+INS-30002_TRANSX = ( 0.0, 0.0117647058823529, 0.0)
+INS-30002_TRANSY = ( 0.0, 0.0, 0.0117647058823529)
+INS-30002_ITRANSS = ( 0.0, 85.0, 0.0)
+INS-30002_ITRANSL = ( 0.0, 0.0, 85.0)
+
+\begintext
+These are the parameters for writing c-kernels. Isis will create ck
+with the same frame endpoints as the mission ck. For Viking1 the ck
+instrument frame is VO2_PLATFORM (-30000) and the ck reference frame
+is B1950 (2) or J2000 (1), depending on the ck used. The mdim2.0_rand
+ck is in J2000.
+
+\begindata
+INS-30001_CK_FRAME_ID=-30000
+INS-30001_CK_REFERENCE_ID=2
+INS-30002_CK_FRAME_ID=-30000
+INS-30002_CK_REFERENCE_ID=2
diff --git a/tests/pytests/data/f004b65/vo2_fict.tsc b/tests/pytests/data/f004b65/vo2_fict.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..f6c2ed107b663439690e01527eb8125e73642e66
--- /dev/null
+++ b/tests/pytests/data/f004b65/vo2_fict.tsc
@@ -0,0 +1,134 @@
+KPL/SCLK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "VO2_FICT.TSC"
+MISSION_NAME = VIKING
+SPACECRAFT_NAME = "VIKING ORBITER 2"
+DATA_SET_ID = "VO1/VO2-M-SPICE-6-V1.0"
+KERNEL_TYPE_ID = SCLK
+PRODUCT_ID = "VO2_FICT.TSC"
+PRODUCT_CREATION_TIME = 2000-04-21T10:53:21
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = {
+ PRIMARY_MISSION,
+ EXTENDED_MISSION,
+ CONTINUATION_MISSION
+ }
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = MARS
+INSTRUMENT_NAME = "N/A"
+NAIF_INSTRUMENT_ID = "N/A"
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = CLOCK_COEFFICIENTS
+ DESCRIPTION = "SCLK file implementing fictitious clock
+used to tag orientation data in the VO2 CK files. This SCLK file does NOT
+represent real Viking Orbiter 2 on-board clock but rather is a simple
+counter of milliseconds since 1 Jan 1976 00:00:00. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+Viking Orbiter 2 "fictitious" SCLK Kernel
+--------------------------------------------------------
+
+ This file contains the data necessary to convert between the
+ 'fictitious' Viking Orbiter 2 on-board clock times used as tags
+ for pointing instances in Viking Orbiter 2 CK files and ephemeris
+ time.
+
+ NAIF suggests that you do not modify this file. If you do modify
+ it, be sure to indicate this in the `Version' section below.
+
+
+Version
+--------------------------------------------------------
+
+ Version 1.0.1 -- April 20, 2000
+
+ Comments in the file were slightly reformatted and augmented.
+
+ Version 1.0.0 -- July 22, 1996
+
+
+Implementation notes
+--------------------------------------------------------
+
+ This SPICE SCLK file is constructed so that valid SCLK strings
+ are simply the number of seconds that have passed since the UTC
+ epoch 1 Jan 1976 00:00:00. Thus 288929292.827 simply represents
+ the epoch that occurs 288929292.827 seconds past the UTC epoch
+ 1 Jan 1976.
+
+ For all time, the clock runs at the same rate as Terrestrial
+ Dynamical Time (TDT). There is only one partition for this clock.
+
+ You must load this file into the kernel pool before using any
+ of the SPICELIB SCLK routines. The code fragment
+
+ CALL LDPOOL ( < name of this file > )
+
+ performs this task. To convert between ET and UTC, you will also
+ need to load a leapseconds kernel. The additional call to LDPOOL,
+
+ CALL LDPOOL ( < name of your leapsecond file > )
+
+ will accomplish this. Note that you must supply the actual names
+ of the files used on your system as arguments to LDPOOL. Because
+ the file names are system dependent, we do not list them here.
+
+ For more information, consult your SPICELIB required reading
+ files. The following areas are covered:
+
+ SCLK system SCLK required reading
+ Time systems and conversion TIME required reading
+ Kernel pool KERNEL required reading
+
+
+Kernel data
+--------------------------------------------------------
+
+ \begindata
+
+ SCLK_KERNEL_ID = ( @22-JUL-1996 )
+
+ SCLK_DATA_TYPE_30 = ( 1 )
+
+ SCLK01_TIME_SYSTEM_30 = ( 2 )
+ SCLK01_N_FIELDS_30 = ( 2 )
+ SCLK01_MODULI_30 = ( 10000000000 1000 )
+ SCLK01_OFFSETS_30 = ( 0 0 )
+ SCLK01_OUTPUT_DELIM_30 = ( 1 )
+
+ SCLK_PARTITION_START_30 = ( 0.0000000000000E+00 )
+ SCLK_PARTITION_END_30 = ( 1.00000000E+14 )
+ SCLK01_COEFFICIENTS_30 = ( 0.00000000E+00
+ @01-JAN-1976-00:00:47.184
+ 1 )
+
+ \begintext
+
+
+Contact Information
+--------------------------------------------------------
+
+ Contact NAIF node of the Planetary Data System if you have any
+ questions regarding this SCLK file.
+
+ Charles H. Acton, Jr
+ (818)-354-3869
+ chuck.acton@jpl.nasa.gov
+
+ Boris V. Semenov
+ (818)-354-8136
+ boris.semenov@jpl.nasa.gov
diff --git a/tests/pytests/data/f004b65/vo2_fsc.tsc b/tests/pytests/data/f004b65/vo2_fsc.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..d3b30a16469e17ab63230b7fbb1e186e39d68883
--- /dev/null
+++ b/tests/pytests/data/f004b65/vo2_fsc.tsc
@@ -0,0 +1,193 @@
+KPL/SCLK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "VO2_FSC.TSC"
+MISSION_NAME = VIKING
+SPACECRAFT_NAME = "VIKING ORBITER 2"
+DATA_SET_ID = "VO1/VO2-M-SPICE-6-V1.0"
+KERNEL_TYPE_ID = SCLK
+PRODUCT_ID = "VO2_FSC.TSC"
+PRODUCT_CREATION_TIME = 2000-04-21T10:53:21
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = {
+ PRIMARY_MISSION,
+ EXTENDED_MISSION,
+ CONTINUATION_MISSION
+ }
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = MARS
+INSTRUMENT_NAME = "N/A"
+NAIF_INSTRUMENT_ID = "N/A"
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = CLOCK_COEFFICIENTS
+ DESCRIPTION = "SCLK file containing linear piecewise
+function representing VO2 FSC on-board clock. This function was generated as
+the result of VO2 image time tags restoration. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+Viking Orbiter 2 Reconstructed Frame Start Count (FSC) SCLK file
+--------------------------------------------------------
+
+ This file contain data necessary to convert a Viking Orbiter 2
+ FSC count to the ET time corresponding to it. These data are
+ based on the results of VO2 image times reconstruction done at
+ NAIF/JPL. The process of this reconstruction is described in
+ detail in the "VO Image Time Reconstruction" document.
+
+ Note that the main purpose of this file is to store the
+ reconstructed FSC counter; the on-board clock defined by the
+ function in this file was not used to time tag any of the
+ orientation data in CK files.
+
+ To avoid confusion with the other VO2 clock used for time tagging,
+ the FSC on-board clock in this file was assigned the NAIF ID
+ code -30999.
+
+
+Version
+--------------------------------------------------------
+
+ Version 1.0.1 -- April 20, 2000
+
+ Comments in the file were slightly reformatted and augmented.
+
+ Version 1.0.0 -- July 22, 1996
+
+
+Implementation notes
+--------------------------------------------------------
+
+ This SPICE SCLK file is constructed so that valid SCLK strings
+ are the eight digit VO2 FSC count associated with each VO2 image.
+ Note that the actual "image time" (the time of the beginning,
+ middle or the end of exposure) has a significant offset from
+ the FSC tick start time. This offset depends on the exposure
+ duration and is described in the "VO Image Time Reconstruction"
+ document.
+
+ You must load this file into the kernel pool before using any
+ of the SPICELIB SCLK routines. The code fragment
+
+ CALL LDPOOL ( < name of this file > )
+
+ performs this task. To convert between ET and UTC, you will also
+ need to load a leapseconds kernel. The additional call to LDPOOL,
+
+ CALL LDPOOL ( < name of your leapsecond file > )
+
+ will accomplish this. Note that you must supply the actual names
+ of the files used on your system as arguments to LDPOOL. Because
+ the file names are system dependent, we do not list them here.
+
+ For more information, consult your SPICELIB required reading
+ files. The following areas are covered:
+
+ SCLK system SCLK required reading
+ Time systems and conversion TIME required reading
+ Kernel pool KERNEL required reading
+
+
+Kernel data
+--------------------------------------------------------
+
+\begindata
+
+ SCLK_KERNEL_ID = ( @22-JUL-1996 )
+
+ SCLK_DATA_TYPE_30999 = ( 1 )
+ SCLK01_TIME_SYSTEM_30999 = ( 2 )
+ SCLK01_N_FIELDS_30999 = ( 1 )
+ SCLK01_MODULI_30999 = ( 80000000 )
+ SCLK01_OFFSETS_30999 = ( 46442015 )
+ SCLK01_OUTPUT_DELIM_30999 = ( 1 )
+
+ SCLK_PARTITION_START_30999 = (
+ 0
+ 357985
+ 777985
+ 1057985
+ 1268246
+ 1457985
+ 2581493
+ 4701667
+ 5412787
+ 6557985
+ 6810335
+ 7107985
+ 9390838
+ 10007985
+ 10607985
+ 11107985
+ 12557985
+ )
+
+ SCLK_PARTITION_END_30999 = (
+ 357985
+ 777985
+ 1057985
+ 1268246
+ 1457985
+ 2581493
+ 4701667
+ 5412787
+ 6557985
+ 6810335
+ 7107985
+ 9390838
+ 10007985
+ 10607985
+ 11107985
+ 12557985
+ 13843304
+ )
+
+ SCLK01_COEFFICIENTS_30999 = (
+
+ 0 -738643373.631604 4.480001294
+ 357985 -737039600.324536 4.480001238
+ 777985 -735157999.769837 4.480001240
+ 1057985 -733903599.385587 4.480001244
+ 1268246 -732961629.770622 4.480001297
+ 1457985 -732111598.747130 4.480001301
+ 2581493 -727078280.882439 4.480001764
+ 4701667 -717579897.536827 4.480001764
+ 5412787 -714394078.461940 4.480001817
+ 6557985 -709263589.346238 4.480001599
+ 6810335 -708133060.592218 4.480001867
+ 7107985 -706799588.012369 4.480001868
+ 9390838 -696572402.934857 4.480001454
+ 10007985 -693807583.640654 4.480001937
+ 10607985 -691119582.502621 4.480001298
+ 11107985 -688879581.719291 4.480001364
+ 12557985 -682383579.531742 4.480001393
+ )
+
+\begintext
+
+
+Contact Information
+--------------------------------------------------------
+
+ Contact NAIF node of the Planetary Data System if you have any
+ questions regarding this SCLK file.
+
+ Charles H. Acton, Jr
+ (818)-354-3869
+ chuck.acton@jpl.nasa.gov
+
+ Boris V. Semenov
+ (818)-354-8136
+ boris.semenov@jpl.nasa.gov
diff --git a/tests/pytests/data/f004b65/vo2_sedr_ck2_0_sliced_-30000.xc b/tests/pytests/data/f004b65/vo2_sedr_ck2_0_sliced_-30000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..6f2a58bc6dd3db553747578e1ce70de919ccf93e
--- /dev/null
+++ b/tests/pytests/data/f004b65/vo2_sedr_ck2_0_sliced_-30000.xc
@@ -0,0 +1,981 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+'VO2 PLATFORM ATTITUDE; CREATED BY BVS/NAIF; 2006-FEB-09 '
+BEGIN_ARRAY 1 960
+'VO2 ATT. BASED ON GEM AND SEDR FILES '
+'481C5943E^9'
+'481F08AF9^9'
+'-7530'
+'2'
+'2'
+'1'
+960
+'2F5044DC744704^0'
+'-45AEE5FC6BF8A^0'
+'7EE9F2A166BF54^0'
+'CDC0ED4CE8C6E^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'2E66F7CEBF327E^0'
+'-44369B138153D^0'
+'7F3FF2755EDE1C^0'
+'CE3EE31CFDF7F^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'2E31EB7BB55964^0'
+'-43C23CD0A73AD4^0'
+'7FBD44327B68E8^0'
+'CE23ADE56DC088^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'2D9F5E0B6177C8^0'
+'-42D4F1213B80D4^0'
+'7FFB9336C2DF7^0'
+'CE6B167B5811A8^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'2D5F01B7201DDE^0'
+'-424DF1FC862AD4^0'
+'8088D1293D2C^0'
+'CE4D0A0B7D5E8^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'2CD705B0AC0BE4^0'
+'-41721644FDF604^0'
+'80C24D6D5D4A58^0'
+'CE8D16C274292^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'2C99EC8651AA58^0'
+'-40E8E9E20D978C^0'
+'8174A4303ECF8^0'
+'CE5619EC41375^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'2C038D20A2FAA4^0'
+'-3FFAC4D988AB2A^0'
+'81A7FAC0552F48^0'
+'CEA07BE0F0167^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'2BCC2DA443A436^0'
+'-3F85E5C8E6C83E^0'
+'823A23DB1691D^0'
+'CE745FCB19DDE8^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'2B334815E19A7E^0'
+'-3E938B4B46EE14^0'
+'826D443D4586A8^0'
+'CEBE469BD9F7D8^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'2AF9C2D85F32AE^0'
+'-3E1F8C73B4301A^0'
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+'0^0'
+'4189374BC6A7F^-2'
+'4D2389DD1236EC^0'
+'-48BD0F8F90537C^0'
+'C193FCB92D9E68^0'
+'81B358CEEF3E1^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'4C386ADFB9B534^0'
+'-487543034EF37C^0'
+'C14880BB60F9A8^0'
+'82D5D80F5C8D88^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'4BCA759FB06084^0'
+'-47FF60DE3AA094^0'
+'C1CA10092C7A7^0'
+'82971744890AB8^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'4AE09660EA8454^0'
+'-47B53E11184CBC^0'
+'C17BDEBF3A56E8^0'
+'83B97A3EA3839^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'481DB505CFFFFC^9'
+'481DB61D3FFFCC^9'
+'481DB736500034^9'
+'481DB84E4FFFCC^9'
+'481DB96760003^9'
+'481DBA7F5FFFC8^9'
+'481DBB95BFFFC4^9'
+'481DBCAD4FFFF8^9'
+'481DBDC650003^9'
+'481DBEDE4FFFC8^9'
+'481DBFF76FFFE^9'
+'481DC10F6FFFF4^9'
+'481DC225CFFFF^9'
+'481DC33D4FFFF4^9'
+'481DC456500028^9'
+'481DC56E5FFFF^9'
+'481DC687600028^9'
+'481DC79F6FFFF^9'
+'481DC8B5C00038^9'
+'481DC9CD4FFFF^9'
+'481DCAE65FFFD8^9'
+'481DCBFE5FFFEC^9'
+'481DCD17600024^9'
+'481DCE2F6FFFEC^9'
+'481DDC6470000C^9'
+'481DDD7C50003C^9'
+'481DDE94900018^9'
+'481DDFAC6FFFCC^9'
+'481DE0C4BFFFD8^9'
+'481DE1DCB00038^9'
+'481DE2F4800038^9'
+'481DE40C5FFFE8^9'
+'481DE5249FFFC8^9'
+'481DE63C6FFFC8^9'
+'481DE754BFFFD4^9'
+'481DE86CBFFFE8^9'
+'481DE984800034^9'
+'481DEA9C50003^9'
+'481DEBB49FFFC4^9'
+'481DECCC7FFFF^9'
+'481DEDE4B0001C^9'
+'481DEEFCB0003^9'
+'481DF0146FFFFC^9'
+'481DF12C50002C^9'
+'481DF244900008^9'
+'481DF35C7FFFEC^9'
+'481DF474BFFFCC^9'
+'481DF58CB0002C^9'
+'481E03C4BFFFE8^9'
+'481E04DC800034^9'
+'481E05F4FFFFDC^9'
+'481E070CAFFFF4^9'
+'481E08253FFFCC^9'
+'481E093D3FFFE^9'
+'481E0A54B0003^9'
+'481E0B6C8FFFE^9'
+'481E0C85200038^9'
+'481E0D9CC0002^9'
+'481E0EB54FFFF8^9'
+'481E0FCD50000C^9'
+'481E10E4D0001^9'
+'481E11FC800028^9'
+'481E1315200034^9'
+'481E142CC0001C^9'
+'481E15454FFFF4^9'
+'481E165D500008^9'
+'481E1774D0000C^9'
+'481E188C800024^9'
+'481E19A520003^9'
+'481E1ABCCFFFC8^9'
+'481E1BD560002^9'
+'481E1CED500004^9'
+'481E2B2550000C^9'
+'481E2C3CD0001^9'
+'481E2D55CFFFC8^9'
+'481E2E6D5FFFFC^9'
+'481E2F86600034^9'
+'481E309E5FFFC8^9'
+'481E31B5500008^9'
+'481E32CCD0000C^9'
+'481E33E5CFFFC4^9'
+'481E34FD4FFFC8^9'
+'481E36166FFFE^9'
+'481E372E5FFFC4^9'
+'481E3845500004^9'
+'481E395CD00008^9'
+'481E3A75D0003C^9'
+'481E3B8D5FFFF4^9'
+'481E3CA6600028^9'
+'481E3DBE6FFFF^9'
+'481E3ED560003^9'
+'481E3FECD^9'
+'481E4105D00038^9'
+'481E421D500038^9'
+'481E4336600024^9'
+'481E444E600038^9'
+'481DB582CFFFFC^9'
+'481DB69A3FFFCC^9'
+'481DB7B3500034^9'
+'481DB8CB4FFFCC^9'
+'481DB9E460003^9'
+'481DBAFC5FFFC8^9'
+'481DBC12BFFFC4^9'
+'481DBD2A4FFFF8^9'
+'481DBE4350003^9'
+'481DBF5B4FFFC8^9'
+'481DC0746FFFE^9'
+'481DC18C6FFFF4^9'
+'481DC2A2CFFFF^9'
+'481DC3BA4FFFF4^9'
+'481DC4D3500028^9'
+'481DC5EB5FFFF^9'
+'481DC704600028^9'
+'481DC81C6FFFF^9'
+'481DC932C00038^9'
+'481DCA4A4FFFF^9'
+'481DCB635FFFD8^9'
+'481DCC7B5FFFEC^9'
+'481DCD94600024^9'
+'481DCEAC6FFFEC^9'
+'481DDCE170000C^9'
+'481DDDF950003C^9'
+'481DDF11900018^9'
+'481DE0296FFFCC^9'
+'481DE141BFFFD8^9'
+'481DE259B00038^9'
+'481DE371800038^9'
+'481DE4895FFFE8^9'
+'481DE5A19FFFC8^9'
+'481DE6B96FFFC8^9'
+'481DE7D1BFFFD4^9'
+'481DE8E9BFFFE8^9'
+'481DEA01800034^9'
+'481DEB1950003^9'
+'481DEC319FFFC4^9'
+'481DED497FFFF^9'
+'481DEE61B0001C^9'
+'481DEF79B0003^9'
+'481DF0916FFFFC^9'
+'481DF1A950002C^9'
+'481DF2C1900008^9'
+'481DF3D97FFFEC^9'
+'481DF4F1BFFFCC^9'
+'481DF609B0002C^9'
+'481E0441BFFFE8^9'
+'481E0559800034^9'
+'481E0671FFFFDC^9'
+'481E0789AFFFF4^9'
+'481E08A23FFFCC^9'
+'481E09BA3FFFE^9'
+'481E0AD1B0003^9'
+'481E0BE98FFFE^9'
+'481E0D02200038^9'
+'481E0E19C0002^9'
+'481E0F324FFFF8^9'
+'481E104A50000C^9'
+'481E1161D0001^9'
+'481E1279800028^9'
+'481E1392200034^9'
+'481E14A9C0001C^9'
+'481E15C24FFFF4^9'
+'481E16DA500008^9'
+'481E17F1D0000C^9'
+'481E1909800024^9'
+'481E1A2220003^9'
+'481E1B39CFFFC8^9'
+'481E1C5260002^9'
+'481E1D6A500004^9'
+'481E2BA250000C^9'
+'481E2CB9D0001^9'
+'481E2DD2CFFFC8^9'
+'481E2EEA5FFFFC^9'
+'481E3003600034^9'
+'481E311B5FFFC8^9'
+'481E3232500008^9'
+'481E3349D0000C^9'
+'481E3462CFFFC4^9'
+'481E357A4FFFC8^9'
+'481E36936FFFE^9'
+'481E37AB5FFFC4^9'
+'481E38C2500004^9'
+'481E39D9D00008^9'
+'481E3AF2D0003C^9'
+'481E3C0A5FFFF4^9'
+'481E3D23600028^9'
+'481E3E3B6FFFF^9'
+'481E3F5260003^9'
+'481E4069D^9'
+'481E4182D00038^9'
+'481E429A500038^9'
+'481E43B3600024^9'
+'481E44CB600038^9'
+END_ARRAY 1 960
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /home/pgiroux/Desktop/f004b65.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/f004b65/vo2_v10.tf b/tests/pytests/data/f004b65/vo2_v10.tf
new file mode 100644
index 0000000000000000000000000000000000000000..0cff34eed43acbb0aabefa14e3f3bb57cf798ed4
--- /dev/null
+++ b/tests/pytests/data/f004b65/vo2_v10.tf
@@ -0,0 +1,470 @@
+KPL/FK
+
+Viking Orbiter 2 Frames Kernel
+===============================================================================
+
+ This frame kernel contains the complete set of frame definitions for
+ the Viking Orbiter 2 (VO2) spacecraft including definitions for the
+ spacecraft frame, instrument platform frame, and science instrument
+ frames.
+
+
+Version and Date
+-------------------------------------------------------------------------------
+
+ Version 1.0 -- December 1, 2005 -- Boris Semenov, NAIF
+
+ Initial Release.
+
+
+References
+-------------------------------------------------------------------------------
+
+ 1. ``Frames Required Reading''
+
+ 2. ``Kernel Pool Required Reading''
+
+ 3. ``C-Kernel Required Reading''
+
+ 4. VO2 Supplemental Experiment Data Record (SEDR) file, 1976-1980.
+
+ 5. Thomas C. Duxbury/JPL, March-July, 1996
+
+
+Contact Information
+-------------------------------------------------------------------------------
+
+ Boris V. 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/CSPICE/ICY routine FURNSH loads
+ a kernel file into the pool as shown below.
+
+ CALL FURNSH ( 'frame_kernel_name' ) SPICELIB/FORTRAN
+
+ furnsh_c ( "frame_kernel_name" ); CSPICE/C
+
+ cspice_furnsh, "frame_kernel_name" ICY/IDL
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+VO2 Frames
+-------------------------------------------------------------------------------
+
+ The following VO2 frames are defined in this kernel file:
+
+ Name Relative to Type NAIF ID
+ ====================== =================== ============ =======
+
+ Spacecraft frame:
+ -----------------
+ VO2_SPACECRAFT rel.to B1950 CK -30900
+
+ Instrument Platform frame:
+ --------------------------
+ VO2_PLATFORM rel.to B1950 CK -30000
+
+ Science Instrument frames:
+ --------------------------
+ VO2_VISA rel.to PLATFORM FIXED -30001
+ VO2_VISA_TD rel.to PLATFORM FIXED -30011
+ VO2_VISB rel.to PLATFORM FIXED -30002
+ VO2_VISB_TD rel.to PLATFORM FIXED -30012
+ VO2_IRTM rel.to PLATFORM FIXED -30003
+ VO2_MAWD rel.to PLATFORM FIXED -30004
+
+
+VO2 Frames Hierarchy
+-------------------------------------------------------------------------------
+
+ The diagram below shows VO2 frames hierarchy:
+
+
+ "B1950" INERTIAL
+ +-----------------------------------------------------------+
+ | | | |
+ | <--pck | <--ck | <--ck | <--pck
+ | | | |
+ V V | V
+ "IAU_MARS" "V01_SPACECRAFT" | "IAU_EARTH"
+ ----------- ---------------- | ------------
+ |
+ |
+ V
+ "VO2_PLATFORM"
+ +---------------------------------------------------------+
+ | | | | | |
+ | <--fixed | <--fixed fixed--> | | | | <--fixed
+ | | | | | |
+ V V V | | V
+ "VO2_IRTM" "VO2_MAWD" "VO2_VISA" | | "VO2_VISB"
+ ---------- ---------- ---------- | | ----------
+ | |
+ | |
+ fixed--> | | <--fixed
+ | |
+ V V
+ "VO2_VISA_TD" "VO2_VISB_TD"
+ ------------- -------------
+
+
+Spacecraft Bus Frame
+-------------------------------------------------------------------------------
+
+ The spacecraft frame is defined as follows:
+
+ [TBD]
+
+ This diagram illustrates the spacecraft bus frame:
+
+ [TBD]
+
+ Since the S/C bus attitude with respect to an inertial frame is
+ provided by a C kernel (see [3] for more information), this frame is
+ defined as a CK-based frame.
+
+ \begindata
+
+ FRAME_VO2_SPACECRAFT = -30900
+ FRAME_-30900_NAME = 'VO2_SPACECRAFT'
+ FRAME_-30900_CLASS = 3
+ FRAME_-30900_CLASS_ID = -30900
+ FRAME_-30900_CENTER = -30
+ CK_-30900_SCLK = -30
+ CK_-30900_SPK = -30
+
+ \begintext
+
+
+Instrument Platform Frame
+-------------------------------------------------------------------------------
+
+ The instrument platform frame is defined as follows:
+
+ [TBD]
+
+ This diagram illustrates the instrument platform frame:
+
+ [TBD]
+
+ Since the platform attitude with respect to an inertial frame is
+ provided by a C kernel (see [3] for more information), this frame is
+ defined as a CK-based frame.
+
+ \begindata
+
+ FRAME_VO2_PLATFORM = -30000
+ FRAME_-30000_NAME = 'VO2_PLATFORM'
+ FRAME_-30000_CLASS = 3
+ FRAME_-30000_CLASS_ID = -30000
+ FRAME_-30000_CENTER = -30
+ CK_-30000_SCLK = -30
+ CK_-30000_SPK = -30
+
+ \begintext
+
+
+VISA and VISB Frames
+-------------------------------------------------------------------------------
+
+ The frames for the Visual Imaging Subsystem Camera A (VISA) and
+ Camera B (VISB) -- VO2_VISA and VO2_VISB -- are defined as follows:
+
+ - Z axis is along the camera boresight;
+
+ - X axis is along detector lines and points toward the right
+ side of the image;
+
+ - Y axis completes the right hand frame;
+
+ - the origin of this frame is located at the camera focal point.
+
+ This diagram illustrates the camera frames:
+
+ [TBD]
+
+ Since the cameras were rigidly mounted on the instrument platform
+ their frames are defined as fixed offset frames with respect to the
+ platform frame.
+
+ The camera orientation with respect to the platform was specified in
+ [4] as the following three rotation angles:
+
+ T pl-cam = R (RASTER_ORIENTATION) R (CONE) R (-CROSS_CONE)
+ Z Y X
+
+ with the following angle values for each of the two cameras:
+
+ VISA:
+
+ CROSS_CONE = -0.679330, deg
+ CONE = -0.023270, deg
+ RASTER_ORIENTATION = 89.880691, deg
+
+ VISB:
+
+ CROSS_CONE = 0.663000, deg
+ CONE = -0.044000, deg
+ RASTER_ORIENTATION = 89.663790, deg
+
+ These angles are used in the frame definition below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the camera to the platform frame -- see [1].)
+
+ \begindata
+
+ FRAME_VO2_VISA = -30001
+ FRAME_-30001_NAME = 'VO2_VISA'
+ FRAME_-30001_CLASS = 4
+ FRAME_-30001_CLASS_ID = -30001
+ FRAME_-30001_CENTER = -30
+ TKFRAME_-30001_SPEC = 'ANGLES'
+ TKFRAME_-30001_RELATIVE = 'VO2_PLATFORM'
+ TKFRAME_-30001_ANGLES = ( -0.679330, 0.023270, -89.880691 )
+ TKFRAME_-30001_AXES = ( 1, 2, 3 )
+ TKFRAME_-30001_UNITS = 'DEGREES'
+
+ FRAME_VO2_VISB = -30002
+ FRAME_-30002_NAME = 'VO2_VISB'
+ FRAME_-30002_CLASS = 4
+ FRAME_-30002_CLASS_ID = -30002
+ FRAME_-30002_CENTER = -30
+ TKFRAME_-30002_SPEC = 'ANGLES'
+ TKFRAME_-30002_RELATIVE = 'VO2_PLATFORM'
+ TKFRAME_-30002_ANGLES = ( 0.663000, 0.044000, -89.663790 )
+ TKFRAME_-30002_AXES = ( 1, 2, 3 )
+ TKFRAME_-30002_UNITS = 'DEGREES'
+
+ \begintext
+
+ Thomas Duxbury provided a different set of angle values for the cameras
+ (see [5]):
+
+ VISA:
+
+ CROSS_CONE = -0.679300, deg
+ CONE = -0.023300, deg
+ RASTER_ORIENTATION = 89.880700, deg
+
+ VISB:
+
+ CROSS_CONE = 0.663000, deg
+ CONE = -0.044000, deg
+ RASTER_ORIENTATION = 89.663800, deg
+
+ To make this alignment solution available, two more frames parallel
+ to the camera frames and including the ``_TB'' suffix in the name
+ and defined below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the camera to the platform frame -- see [1].)
+
+ \begindata
+
+ FRAME_VO1_VISA_TD = -30011
+ FRAME_-30011_NAME = 'VO1_VISA_TD'
+ FRAME_-30011_CLASS = 4
+ FRAME_-30011_CLASS_ID = -30011
+ FRAME_-30011_CENTER = -30
+ TKFRAME_-30011_SPEC = 'ANGLES'
+ TKFRAME_-30011_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-30011_ANGLES = ( -0.679300, 0.023300, -89.880700 )
+ TKFRAME_-30011_AXES = ( 1, 2, 3 )
+ TKFRAME_-30011_UNITS = 'DEGREES'
+
+ FRAME_VO1_VISB_TD = -30012
+ FRAME_-30012_NAME = 'VO1_VISB_TD'
+ FRAME_-30012_CLASS = 4
+ FRAME_-30012_CLASS_ID = -30012
+ FRAME_-30012_CENTER = -30
+ TKFRAME_-30012_SPEC = 'ANGLES'
+ TKFRAME_-30012_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-30012_ANGLES = ( 0.663000, 0.044000, -89.663800 )
+ TKFRAME_-30012_AXES = ( 1, 2, 3 )
+ TKFRAME_-30012_UNITS = 'DEGREES'
+
+ \begintext
+
+
+IRTM Frame
+-------------------------------------------------------------------------------
+
+ The frame for the Infrared Thermal Mapper -- VO2_IRTM -- is defined
+ as follows:
+
+ [TBD]
+
+ This diagram illustrates the IRTM frame:
+
+ [TBD]
+
+ Since the IRTM instrument was rigidly mounted on the instrument
+ platform its frame is defined as fixed offset frames with respect to
+ the platform frame.
+
+ The instrument orientation with respect to the platform can be
+ specified using the following three rotation angles:
+
+ T pl-cam = R (RASTER_ORIENTATION) R (CONE) R (-CROSS_CONE)
+ Z Y X
+
+ with the nominal angle values:
+
+ CROSS_CONE = 0.0, deg
+ CONE = 0.0, deg
+ RASTER_ORIENTATION = 90.0, deg
+
+ These angles are used in the frame definition below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the instrument to the platform frame -- see
+ [1].)
+
+ \begindata
+
+ FRAME_VO2_IRTM = -30003
+ FRAME_-30003_NAME = 'VO2_IRTM'
+ FRAME_-30003_CLASS = 4
+ FRAME_-30003_CLASS_ID = -30003
+ FRAME_-30003_CENTER = -30
+ TKFRAME_-30003_SPEC = 'ANGLES'
+ TKFRAME_-30003_RELATIVE = 'VO2_PLATFORM'
+ TKFRAME_-30003_ANGLES = ( 0.0, 0.0, -90.0 )
+ TKFRAME_-30003_AXES = ( 1, 2, 3 )
+ TKFRAME_-30003_UNITS = 'DEGREES'
+
+ \begintext
+
+
+MAWD Frame
+-------------------------------------------------------------------------------
+
+ The frame for the Mars Atmosphere Water Detector (MAWD) -- VO2_MAWD
+ -- is defined as follows:
+
+ [TBD]
+
+ This diagram illustrates the MAWD frame:
+
+ [TBD]
+
+ Since the MAWD instrument was rigidly mounted on the instrument
+ platform its frame is defined as fixed offset frames with respect to
+ the platform frame.
+
+ The instrument orientation with respect to the platform can be
+ specified using the following three rotation angles:
+
+ T pl-cam = R (RASTER_ORIENTATION) R (CONE) R (-CROSS_CONE)
+ Z Y X
+
+ with the nominal angle values:
+
+ CROSS_CONE = 0.0, deg
+ CONE = 0.0, deg
+ RASTER_ORIENTATION = 90.0, deg
+
+ These angles are used in the frame definition below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the instrument to the platform frame -- see
+ [1].)
+
+ \begindata
+
+ FRAME_VO2_MAWD = -30004
+ FRAME_-30004_NAME = 'VO2_MAWD'
+ FRAME_-30004_CLASS = 4
+ FRAME_-30004_CLASS_ID = -30004
+ FRAME_-30004_CENTER = -30
+ TKFRAME_-30004_SPEC = 'ANGLES'
+ TKFRAME_-30004_RELATIVE = 'VO2_PLATFORM'
+ TKFRAME_-30004_ANGLES = ( 0.0, 0.0, -90.0 )
+ TKFRAME_-30004_AXES = ( 1, 2, 3 )
+ TKFRAME_-30004_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Viking Orbiter 2 NAIF ID Codes -- Definition Section
+========================================================================
+
+ This section contains name to NAIF ID mappings for the VO2. Once the
+ contents of this file is loaded into the KERNEL POOL, these mappings
+ become available within SPICE, making it possible to use names
+ instead of ID code in the high level SPICE routine calls.
+
+ Spacecraft and its structures:
+ ------------------------------
+
+ VIKING ORBITER 2 -30
+ VO2 -30
+
+ VO2_SPACECRAFT_BUS -30900
+ VO2_SC_BUS -30900
+ VO2_SPACECRAFT -30900
+
+ VO2_INSTRUMENT_PLATFORM -30000
+ VO2_PLATFORM -30000
+
+ Science Instruments:
+ --------------------
+
+ VO2_VISA -30001
+ VO2_VISB -30002
+
+ VO2_IRTM -30003
+
+ VO2_MAWD -30004
+
+ The mappings summarized in this table are implemented by the keywords
+ below.
+
+ \begindata
+
+ NAIF_BODY_NAME += ( 'VIKING ORBITER 2' )
+ NAIF_BODY_CODE += ( -30 )
+
+ NAIF_BODY_NAME += ( 'VO2' )
+ NAIF_BODY_CODE += ( -30 )
+
+ NAIF_BODY_NAME += ( 'VO2_SPACECRAFT_BUS' )
+ NAIF_BODY_CODE += ( -30900 )
+
+ NAIF_BODY_NAME += ( 'VO2_SC_BUS' )
+ NAIF_BODY_CODE += ( -30900 )
+
+ NAIF_BODY_NAME += ( 'VO2_SPACECRAFT' )
+ NAIF_BODY_CODE += ( -30900 )
+
+ NAIF_BODY_NAME += ( 'VO2_INSTRUMENT_PLATFORM' )
+ NAIF_BODY_CODE += ( -30000 )
+
+ NAIF_BODY_NAME += ( 'VO2_PLATFORM' )
+ NAIF_BODY_CODE += ( -30000 )
+
+ NAIF_BODY_NAME += ( 'VO2_VISA' )
+ NAIF_BODY_CODE += ( -30001 )
+
+ NAIF_BODY_NAME += ( 'VO2_VISB' )
+ NAIF_BODY_CODE += ( -30002 )
+
+ NAIF_BODY_NAME += ( 'VO2_IRTM' )
+ NAIF_BODY_CODE += ( -30003 )
+
+ NAIF_BODY_NAME += ( 'VO2_MAWD' )
+ NAIF_BODY_CODE += ( -30004 )
+
+ \begintext
diff --git a/tests/pytests/data/f704b28/f704b28_0.xsp b/tests/pytests/data/f704b28/f704b28_0.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..c34e3bb2fbd52ff79bc35fbeee66a32c32a6f722
--- /dev/null
+++ b/tests/pytests/data/f704b28/f704b28_0.xsp
@@ -0,0 +1,418 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
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+'MAR097 '
+'-2855CCF9643998^8'
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+'1F3'
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+'0^0'
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+'0^0'
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+'546^4'
+'32^2'
+'1^1'
+END_ARRAY 4 54
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /home/pgiroux/Desktop/vo2_sliced/f704b28_0.bsp LOG FILE
+
+; Created 2019-09-27/11:28:08.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /home/pgiroux/Desktop/vo2_sliced/f704b28_0.bsp
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/viking2/kernels/spk/vo2_rcon.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -30
+ BEGIN_TIME = 1978 JUL 23 04:31:17.425
+ END_TIME = 1978 JUL 23 05:18:02.556
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/spk/mar097.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 4, 10, 499
+ BEGIN_TIME = 1978 JUL 23 04:31:17.425
+ END_TIME = 1978 JUL 23 05:18:02.556
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/f704b28/f704b28_isis3.lbl b/tests/pytests/data/f704b28/f704b28_isis3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..01b91f03bc5d1e539a69f34ce75e0a5acc92a867
--- /dev/null
+++ b/tests/pytests/data/f704b28/f704b28_isis3.lbl
@@ -0,0 +1,103 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 1204
+ TileLines = 1056
+
+ Group = Dimensions
+ Samples = 1204
+ Lines = 1056
+ Bands = 1
+ End_Group
+
+ Group = Pixels
+ Type = UnsignedByte
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftName = VIKING_ORBITER_2
+ InstrumentId = VISUAL_IMAGING_SUBSYSTEM_CAMERA_B
+ TargetName = MARS
+ StartTime = 1978-07-23T05:01:26
+ ExposureDuration = 0.067880 <seconds>
+ SpacecraftClockCount = 60266453
+ FloodModeId = ON
+ GainModeId = LOW
+ OffsetModeId = ON
+ End_Group
+
+ Group = Archive
+ DataSetId = VO1/VO2-M-VIS-2-EDR-V2.0
+ ProductId = 704B28
+ MissonPhaseName = CONTINUATION_MISSION
+ ImageNumber = 60266453
+ OrbitNumber = 704
+ End_Group
+
+ Group = BandBin
+ FilterName = MINUS_BLUE
+ FilterId = 2
+ Center = 0.55 <micrometers>
+ Width = 0.22 <micrometers>
+ End_Group
+
+ Group = Kernels
+ NaifFrameCode = -30002
+ CameraVersion = 1
+ End_Group
+
+ Group = Reseaus
+ Line = (5, 7, 9, 10, 11, 12, 14, 15, 17, 19, 20, 135, 136, 137, 138,
+ 139, 140, 142, 143, 144, 146, 148, 149, 265, 266, 267, 268,
+ 269, 270, 271, 272, 274, 276, 278, 395, 395, 397, 398, 398,
+ 399, 400, 401, 402, 404, 406, 407, 525, 526, 526, 527, 528,
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+ 916, 917, 918, 920, 922, 1043, 1043, 1043, 1043, 1044, 1044,
+ 1045, 1045, 1046, 1048, 1051)
+ Sample = (23, 141, 257, 373, 489, 605, 720, 836, 952, 1068, 1185, 23,
+ 82, 199, 315, 431, 546, 662, 778, 894, 1010, 1126, 1184, 24,
+ 141, 257, 373, 489, 605, 720, 836, 952, 1068, 1184, 24, 82,
+ 199, 315, 432, 547, 663, 779, 895, 1011, 1127, 1184, 24, 141,
+ 258, 374, 490, 605, 721, 837, 953, 1070, 1185, 24, 83, 200,
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+ 432, 548, 664, 780, 896, 1013, 1129, 1186, 22, 140, 257, 374,
+ 489, 606, 722, 838, 954, 1071, 1187)
+ Type = (1, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6)
+ Valid = (0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
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+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0)
+ Template = $viking2/reseaus/vo2.visb.template.cub
+ Status = Nominal
+ End_Group
+End_Object
+
+Object = Label
+ Bytes = 65536
+End_Object
+
+Object = History
+ Name = IsisCube
+ StartByte = 1336961
+ Bytes = 428
+End_Object
+
+Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 1337389
+ Bytes = 2042
+End_Object
+End
diff --git a/tests/pytests/data/f704b28/f704b28_pds3.lbl b/tests/pytests/data/f704b28/f704b28_pds3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..154343c271bfe87e213abaaddc47a551e913112d
--- /dev/null
+++ b/tests/pytests/data/f704b28/f704b28_pds3.lbl
@@ -0,0 +1,1632 @@
+CCSD3ZF0000100000001NJPL3IF0PDS200000001 = SFDU_LABEL
+/* FILE FORMAT AND LENGTH */
+RECORD_TYPE = VARIABLE_LENGTH
+RECORD_BYTES = 1204
+FILE_RECORDS = 2176
+LABEL_RECORDS = 60
+/* POINTERS TO START RECORDS OF MAJOR OBJECTS IN FILE */
+^IMAGE_HISTOGRAM = 61
+^ENCODING_HISTOGRAM = 62
+^ENGINEERING_TABLE = 64
+^LINE_HEADER_TABLE = 65
+^IMAGE = 1121
+/* IMAGE DESCRIPTION */
+DATA_SET_ID = 'VO1/VO2-M-VIS-2-EDR-V2.0'
+SPACECRAFT_NAME = VIKING_ORBITER_2
+MISSION_PHASE_NAME = CONTINUATION_MISSION
+TARGET_NAME = MARS
+IMAGE_ID = '704B28'
+IMAGE_NUMBER = 60266453
+IMAGE_TIME = 1978-07-23T05:01:26Z
+EARTH_RECEIVED_TIME = 1978-07-23T06:18:16Z
+ORBIT_NUMBER = 704
+INSTRUMENT_NAME = VISUAL_IMAGING_SUBSYSTEM_CAMERA_B
+GAIN_MODE_ID = LOW
+FLOOD_MODE_ID = ON
+OFFSET_MODE_ID = ON
+FILTER_NAME = MINUS_BLUE
+EXPOSURE_DURATION = 0.067880 <SECONDS>
+NOTE = "MEDIUM RESOLUTION MAPPING SEQUENCE"
+/* DESCRIPTION OF THE OBJECTS CONTAINED IN FILE */
+OBJECT = IMAGE_HISTOGRAM
+ ITEMS = 256
+ ITEM_TYPE = VAX_INTEGER
+ ITEM_BITS = 32
+END_OBJECT
+OBJECT = ENCODING_HISTOGRAM
+ ITEMS = 511
+ ITEM_TYPE = VAX_INTEGER
+ ITEM_BITS = 32
+END_OBJECT
+OBJECT = ENGINEERING_TABLE
+ ROWS = 1
+ ROW_BYTES = 152
+CCSD3ZF0000100000001NJPL3IF0PDS200000001 = SFDU_LABEL
+
+OBJECT = ENGINEERING_TABLE_STRUCTURE
+ INTERCHANGE_FORMAT = BINARY
+ BYTES = 152
+ NOTE = "This structure describes the format of
+ the engineering record that is included in each image file.
+ This record contains the first 152 bytes of data extracted from
+ the Mission and Test Imaging System (MTIS) header record on each
+ file of an imaging EDR tape."
+
+ OBJECT = COLUMN
+ NAME = MTIS_RECORD_ID
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 1
+ BYTES = 2
+ DESCRIPTION = "Mission and Test Imaging System record
+ ID."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PHYSICAL_SEQUENCE_NUMBER
+ DATA_TYPE = VAX_UNSIGNED_INTEGER
+ START_BYTE = 3
+ BYTES = 2
+ DESCRIPTION = "Physical sequence number on Experiment
+ Data Record tape. Not used."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LOGICAL_SEQUENCE_NUMBER
+ DATA_TYPE = VAX_UNSIGNED_INTEGER
+ START_BYTE = 5
+ BYTES = 2
+ DESCRIPTION = "Logical sequence number on Experiment
+ Data Record tape. Not used."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_ERT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 7
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time year and day
+ value. Time of first line segment in the file containing valid
+ data. This field is NOT stored in VAX least significant byte
+ first format."
+
+ OBJECT = BIT_COLUMN
+ NAME = FIRST_ERT_YEAR
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 1
+ BITS = 7
+ DESCRIPTION = "Earth Received Time year of century
+ (1900). Time of first line record in the file containing valid
+ data. This field is often incorrect."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FIRST_ERT_DAY
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 7
+ BITS = 9
+ DESCRIPTION = "Earth Received Time day of year."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_ERT_MINUTE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 9
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time minute of day."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_ERT_MILLISECOND
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 11
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time millisecond of
+ minute."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_ERT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 13
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time year and day
+ value. Time of last line segment of the file containing valid
+ data."
+
+ OBJECT = BIT_COLUMN
+ NAME = LAST_ERT_YEAR
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 1
+ BITS = 7
+ DESCRIPTION = "Earth Received Time year of century
+ (1900). This field is often incorrect."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = LAST_ERT_DAY
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 8
+ BITS = 9
+ DESCRIPTION = "Earth Received Time day of year."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_ERT_MINUTE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 15
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time minute of day."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_ERT_MILLISECOND
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 17
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time millisecond of
+ minute."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_FDS_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 19
+ BYTES = 4
+ DESCRIPTION = "Flight Data Subsystem count for the
+ first line segment of the file containing valid data. Note that
+ this may not correspond to the FDS count for line 1, segment 1."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_FDS_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 23
+ BYTES = 4
+ DESCRIPTION = "Flight Data Subsystem count for the
+ last line segment of the file containing valid data. Note that
+ this may not correspond to the FDS count for segment 7 of line
+ 1056."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = EDR_ID
+ DATA_TYPE = CHARACTER
+ START_BYTE = 27
+ BYTES = 6
+ DESCRIPTION = "Tape reel identifier of the original
+ EDR tape for this image."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = EDR_FILE_NUMBER
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 33
+ BYTES = 2
+ DESCRIPTION = "File number of image on original EDR
+ tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FILL_IN
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 34
+ BYTES = 1
+ DESCRIPTION = "Value used to fill in missing samples
+ (always zero)."
+ END_OBJECT = COLUMN
+ OBJECT = COLUMN
+ NAME = TRACK_PRESENCE_MASK
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 36
+ BYTES = 1
+ DESCRIPTION = "Mask indicating which tracks are
+ present in the image. The nominal value is HEX 7F, indicating
+ that all seven tracks are present."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = AVERAGE_PIXEL
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 37
+ BYTES = 2
+ DESCRIPTION = "Average pixel value for image."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_1
+ DATA_TYPE = CHARACTER
+ START_BYTE = 39
+ BYTES = 4
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MINIMUM_SNR
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 43
+ BYTES = 2
+ FACTOR = 0.03125
+ DESCRIPTION = "Minimum signal to noise ratio. The
+ minimum noise level found for the scan lines. Divide by 32 to
+ get the actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MAXIMUM_SNR
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 45
+ BYTES = 2
+ FACTOR = 0.03125
+ DESCRIPTION = "Maximum signal to noise ratio. The
+ maximum noise level found for the scan lines. Divide by 32 to
+ get the actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_2
+ DATA_TYPE = CHARACTER
+ START_BYTE = 47
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MINIMUM_AGC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 49
+ BYTES = 2
+ FACTOR = 0.0625
+ DESCRIPTION = "Automatic gain control minimum.
+ Divide by 16 to get actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MAXIMUM_AGC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 51
+ BYTES = 2
+ FACTOR = 0.0625
+ DESCRIPTION = "Automatic gain control maximum.
+ Divide by 16 to get actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_3
+ DATA_TYPE = CHARACTER
+ START_BYTE = 53
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 55
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that contain some valid data (maximum is 7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FULLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 57
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that were fully synchronized (maximum is 7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PARTLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 59
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that were partly synchronized (maximum is 7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI0_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 61
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 0 (maximum is 7 x 1056).
+ DQI0 indicates bad data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI1_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 63
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 1 (maximum is 7 x 1056).
+ DQI1 means SNR low, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI2_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 65
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 2 (maximum is 7 x 1056).
+ DQI2 means SNR good, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI3_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 67
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 3 (maximum is 7 x 1056).
+ DQI3 means SNR low, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI4_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 69
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 4 (maximum is 7 x 1056).
+ DQI4 means SNR good, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FDS_CORRECTIONS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 71
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with corrected FDS counts."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PNERROR_CORRECTIONS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 73
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with corrected pseudonoise codes."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = ADJUSTED_PNERROR_CORRECTIONS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 75
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with corrected pseudonoise codes adjusted based on the
+ number of line segments processed versus the total in a full
+ image (7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNREADABLE_RECORDS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 77
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that could not be read from the Master Data Record tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LOGICAL_SEQUENCE_BREAKS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 79
+ BYTES = 2
+ DESCRIPTION = "Total number of breaks in logical
+ sequence number in reading the System/Master Data Record tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DATA_BREAKS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 81
+ BYTES = 2
+ DESCRIPTION = "Total number of breaks in data
+ sequence in reading the System/Master Data Record tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_4
+ DATA_TYPE = CHARACTER
+ START_BYTE = 83
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINES
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 85
+ BYTES = 2
+ DESCRIPTION = "Total number of lines in the file that
+ contain some valid data (nominal is 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FULL_LINES
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 87
+ BYTES = 2
+ DESCRIPTION = "Number of lines in the file that are
+ composed of seven line segments."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PARTIAL_LINES
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 89
+ BYTES = 2
+ DESCRIPTION = "Total number of line records in the
+ file that contain some valid data but are not composed of seven
+ line segments."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_LINE_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 91
+ BYTES = 2
+ DESCRIPTION = "First line in image containing valid
+ data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_LINE_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 93
+ BYTES = 2
+ DESCRIPTION = "Last line in image containing valid
+ data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_5
+ DATA_TYPE = CHARACTER
+ START_BYTE = 95
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = IMAGE_ID
+ DATA_TYPE = CHARACTER
+ START_BYTE = 97
+ BYTES = 6
+ DESCRIPTION = "Image identifier (PICNO) for this
+ image, formatted OOOSNN, where OOO is orbit number, S is
+ spacecraft identifier (A for Viking Orbiter 1 prime and extended
+ missions; B for Viking Orbiter 2; and S for Viking Orbiter 1
+ Survey mission)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VRP_RUN_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 103
+ BYTES = 2
+ DESCRIPTION = "Viking Reconstruction Processing run
+ number."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DISK_ID
+ DATA_TYPE = CHARACTER
+ START_BYTE = 105
+ BYTES = 6
+ DESCRIPTION = "MTIS disk identifier of the original
+ EDR file for this image."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_6
+ DATA_TYPE = CHARACTER
+ START_BYTE = 111
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = TRANSMITTED_CODE_WORD1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 113
+ BYTES = 2
+ DESCRIPTION = "Transmitted command code word for the
+ image."
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ START_BIT = 1
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Set to 1 if data not present for the
+ following measurements."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ START_BIT = 3
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Data quality indicator associated with
+ code word values. Where: 0 is bad data; 1 is SNR low, GCF block
+ error; 2 is SNR good, GCF block bad; 3 is SNR low, GCF block
+ good; 4 is SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = CATHODE_CURRENT_FLAG
+ START_BIT = 7
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Cathode current off (0) or on (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = GAIN_FLAG
+ START_BIT = 8
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Gain mode low (0) or high (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = LIGHT_FLOOD_FLAG
+ START_BIT = 9
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Light flood off (0) or on (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FILTER_STEP
+ START_BIT = 10
+ BITS = 2
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Filter step indicator."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = EXPOSURE_CODE
+ START_BIT = 12
+ BITS = 5
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Exposure interval code."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = TRANSMITTED_CODE_WORD2
+ DATA_TYPE = INTEGER
+ START_BYTE = 115
+ BYTES = 2
+ DESCRIPTION = "Transmitted command code word 2 for
+ this image."
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ START_BIT = 1
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Set to 1 if data not present for the
+ following measurements."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ START_BIT = 3
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Data quality indicator associated with
+ code word values. where: 0 is bad data; 1 is SNR low, GCF block
+ error; 2 is SNR good, GCF block bad; 3 is SNR low, GCF block
+ good; 4 is SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FILTER_NUMBER
+ START_BIT = 10
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Filter number: where 1 is blue; 2 is
+ minus blue; 3 is violet; 4 is clear; 5 is green; and 6 is red."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = CAMERA_SERIAL_NUMBER
+ START_BIT = 13
+ BITS = 4
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Visual Imaging Subsystem camera serial
+ number."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = RECEIVED_CODE_WORD1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 117
+ BYTES = 2
+ DESCRIPTION = "Received command code word for the
+ image."
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ START_BIT = 1
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Set to 1 if data not present for the
+ following measurements."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ START_BIT = 3
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Data quality indicator associated with
+ code word values. where: 0 is bad data; 1 is SNR low, GCF block
+ error; 2 is SNR good, GCF block bad; 3 is SNR low, GCF block
+ good; 4 is SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = CATHODE_CURRENT_FLAG
+ START_BIT = 7
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Cathode current (beam) off (0) or on
+ (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = GAIN_FLAG
+ START_BIT = 8
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Gain mode low (0) or high (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = LIGHT_FLOOD_FLAG
+ START_BIT = 9
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Light flood off (0) or on (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FILTER_STEP
+ START_BIT = 10
+ BITS = 2
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Filter step."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = EXPOSURE_CODE
+ START_BIT = 12
+ BITS = 5
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Exposure interval code."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS50_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 121
+ BYTES = 2
+ DESCRIPTION = "Plus 50 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS15_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 123
+ BYTES = 2
+ DESCRIPTION = "Plus 15 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS12_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 125
+ BYTES = 2
+ DESCRIPTION = "Plus 12 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS5_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 127
+ BYTES = 2
+ DESCRIPTION = "Plus 5 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_MINUS15_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 129
+ BYTES = 2
+ DESCRIPTION = "Minus 15 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_MINUS23_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 131
+ BYTES = 2
+ DESCRIPTION = "Minus 23 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_AVERAGE_VIDEO
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 133
+ BYTES = 2
+ DESCRIPTION = "Average video."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = POWER_CONVERTER_INPUT_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 135
+ BYTES = 2
+ DESCRIPTION = "Power converter input current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = CATHODE_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 137
+ BYTES = 2
+ DESCRIPTION = "Cathode current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = CATHODE_VOLTAGE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 139
+ BYTES = 2
+ DESCRIPTION = "Cathode voltage."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FILAMENT_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 141
+ BYTES = 2
+ DESCRIPTION = "Filament current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FRAME_SWEEP_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 143
+ BYTES = 2
+ DESCRIPTION = "Frame sweep current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_SWEEP_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 145
+ BYTES = 2
+ DESCRIPTION = "Line sweep current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = GRID3_VOLTAGE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 147
+ BYTES = 2
+ DESCRIPTION = "Grid 3 voltage."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FOCUS_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 149
+ BYTES = 2
+ DESCRIPTION = "Focus current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DIGITAL_LADDER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 151
+ BYTES = 2
+ DESCRIPTION = "Digital ladder."
+ END_OBJECT = COLUMN
+
+END_OBJECT = ENGINEERING_TABLE_STRUCTURE
+
+END
+END_OBJECT
+OBJECT = LINE_HEADER_TABLE
+ ROWS = 1056
+ ROW_BYTES = 62
+CCSD3ZF0000100000001NJPL3IF0PDS200000001 = SFDU_LABEL
+
+OBJECT = LINE_HEADER_TABLE_STRUCTURE
+ INTERCHANGE_FORMAT = BINARY
+ BYTES = 62
+ NOTE = "Viking Orbiter Image Line-header
+ Structure. This label describes the structure of the 62-bytes
+ extracted from the end of each image line."
+
+ OBJECT = COLUMN
+ NAME = FDS_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 1
+ BYTES = 4
+ DESCRIPTION = "Flight Data Subsystem (FDS) clock
+ count."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 5
+ BYTES = 2
+ DESCRIPTION = "Flight Data Subsystem line number,
+ extracted from the telemetry record header information."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FILL_IN
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 7
+ BYTES = 1
+ DESCRIPTION = "Value used to fill in missing samples
+ (always zero)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = TRACK_PRESENCE_MASK
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 8
+ BYTES = 1
+ DESCRIPTION = "Mask indicating which tracks are
+ present in this line. The nominal value is HEX 7F, indicating
+ that all seven tracks are present."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = AVERAGE_PIXEL
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 9
+ BYTES = 2
+ DESCRIPTION = "Average pixel value for this line."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 11
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ line that contain some valid data (maximum is 7)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FULLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 13
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ that were fully synchronized (maximum is 7)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PARTLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 15
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ that were partly synchronized (maximum is 7)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI0_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 17
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 0 (maximum is 7), indicating
+ bad data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI1_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 19
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 1 (maximum is 7), indicating
+ SNR low, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI2_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 21
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 2 (maximum is 7), indicating
+ SNR good, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI3_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 23
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 3 (maximum is 7), indicating
+ SNR low, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI4_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 25
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 4 (maximum is 7), indicating
+ SNR good, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 27
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 29
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT2
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 31
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK2
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 33
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT3
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 35
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK3
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 37
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT4
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 39
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK4
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 41
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT5
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 43
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK5
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 45
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT6
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 47
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK6
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 49
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT7
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 51
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK7
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 53
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = EMBEDDED_SCIENCE_DATA
+ ITEMS = 7
+ DATA_TYPE = INTEGER
+ START_BYTE = 55
+ ITEM_BYTES = 1
+ DESCRIPTION = "Embedded low rate science data from
+ seven segments."
+ END_OBJECT = COLUMN
+
+END_OBJECT = LINE_HEADER_TABLE_STRUCTURE
+
+END
+END_OBJECT
+OBJECT = IMAGE
+ ENCODING_TYPE = HUFFMAN_FIRST_DIFFERENCE
+ LINES = 1056
+ LINE_SAMPLES = 1204
+ SAMPLE_TYPE = UNSIGNED_INTEGER
+ SAMPLE_BITS = 8
+ SAMPLE_BIT_MASK = 2#11111110#
+ CHECKSUM = 157067616
+END_OBJECT
+END
diff --git a/tests/pytests/data/f704b28/naif0012.tls b/tests/pytests/data/f704b28/naif0012.tls
new file mode 100644
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/f704b28/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/f704b28/pck00009.tpc b/tests/pytests/data/f704b28/pck00009.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..bfadaab2b26817327189ff3173e9609f49dedc9d
--- /dev/null
+++ b/tests/pytests/data/f704b28/pck00009.tpc
@@ -0,0 +1,3639 @@
+KPL/PCK
+
+
+P_constants (PcK) SPICE kernel file
+===========================================================================
+
+ By: Nat Bachman (NAIF) 2010 March 3
+
+
+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/IAG
+ 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
+
+
+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 and planets.
+ Additional items included in this section:
+
+ - Earth north geomagnetic centered dipole values
+ for epochs 1945-2000
+
+ - Mars prime meridian offset "lambda_a"
+
+ -- Orientation constants for satellites
+
+ -- Orientation constants for asteroids Eros, Gaspra, Ida,
+ Itokawa, and Vesta
+
+ -- Orientation constants for comets 19P/Borrelly
+ and 9P/Tempel 1
+
+
+ Radii of Bodies
+ ---------------
+
+ -- Radii of Sun and planets
+
+ -- Radii of satellites, where available
+
+ -- Radii of asteroids Ceres, Eros, Gaspra, Ida, Itokawa,
+ Mathilde, Toutatis, and Vesta.
+
+ -- Radii of comets 19P/Borrelly, Halley, 9P/Tempel 1,
+ and 81P/Wild 2
+
+
+
+Version Description
+--------------------------------------------------------
+
+ This file was created on March 3, 2010. This version
+ incorporates data from reference [1].
+
+ This file contains size, shape, and orientation data for all
+ objects described by the previous version of the file, except
+ for Kleopatra: a shape model for this body is not provided in [1]
+ because, according to this source, it had been "modeled from
+ low resolution radar data, and cannot be mapped from those
+ data."
+
+ New objects covered by this file but not the previous
+ version are:
+
+ 19P/Borrelly
+ Halley
+ 9P/Tempel 1
+ 81P/Wild 2
+ Ceres
+ Itokawa
+ Mathilde
+ Toutatis
+
+
+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, and version description section if you modify
+ this file.
+
+Known Limitations and Caveats
+
+ Accuracy
+ --------
+
+ In general, the orientation models given here are claimed by the
+ IAU/IAG 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]) 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. 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 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. A more
+ accurate approximation can be obtained by using both the NAIF
+ lunar frame kernel and the binary lunar orientation PCK file,
+ which 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
+ J2000 epoch 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].
+
+
+ Mars prime meridian offset
+ --------------------------
+
+ The Mars prime meridian offset given by [5] is not used by
+ SPICE geometry software for computations involving the shape
+ of Mars (for example, in sub-observer point or surface intercept
+ computations). The value 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 only planets for which such terms are used are
+ Jupiter and Neptune. Use of trigonometric polynomial terms for
+ natural satellites is and has been supported for all SPICE Toolkit
+ versions.
+
+ 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
+--------------------------------------------------------
+
+ The sources for the constants listed in this file are:
+
+
+ [1] 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."
+
+ [2] Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F.,
+ Cruikshank, D.P., Hilton, J.L., Keller, H.U., Oberst, J.,
+ Simon, J.L., Stooke, P., Tholen, D.J., and Thomas, P.C.
+ "Report of the IAU/IAG Working Group on Cartographic
+ Coordinates and Rotational Elements of the Planets and
+ Satellites: 2003."
+
+ [3] 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.
+
+ [4] Nautical Almanac Office, United States Naval Observatory,
+ H.M. Nautical Almanac Office, Royal Greenwich
+ Observatory, Jet Propulsion Laboratory, Bureau des
+ Longitudes, and The Time Service and Astronomy
+ Departments, United States Naval Observatory (1992).
+ "Explanatory Supplement to the Astronomical Almanac," P.
+ Kenneth Seidelmann, ed. University Science Books, 20
+ Edgehill Road, Mill Valley, CA 9494.
+
+ [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.
+
+
+ Most values are from [1]. All exceptions are
+ commented where they occur in this file. The exceptions are:
+
+
+ -- Radii for the Sun are from [3].
+
+ -- 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
+ [8]. The article [6] was used to check most of
+ these values, and the values were also re-computed from
+ the 9th generation IGRF [9] by Nat Bachman.
+
+ -- The Mars prime meridian offset angle is from [5].
+
+
+ "Old values" listed are from the SPICE P_constants file
+ pck00008.tpc dated September 21, 2004. Most of these values came
+ from the 2003 IAU report [2].
+
+
+
+
+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 = ( 6378.14 6378.14 6356.75 )
+
+ Any blanks preceding or following keyword names, values and equal
+ signs are ignored.
+
+ Assignments may be spread over multiple lines, for example:
+
+ BODY399_RADII = ( 6378.14
+ 6378.14
+ 6356.75 )
+
+ 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 2006 IAU/IAG 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 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 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, 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: 2006 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 = ( 284.95 870.5366420 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 term is zero for all bodies except Mars. It represents the
+ angular offset between the meridian containing the longest axis of
+ the triaxial ellipsoid used to model a body's surface and the
+ prime meridian of the body.
+
+ 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 2006 IAU report does
+ not use any other models, except in the case of Mars, where
+ separate values are given for the north and south polar radii.
+
+ 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 = ( 6378.14 6378.14 6356.75 )
+
+
+Body Numbers 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
+
+
+ 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
+ 2000004 Asteroid Vesta
+ 2000216 Asteroid Kleopatra
+ 2000253 Asteroid Mathilde
+ 2000433 Asteroid Eros
+ 2004179 Asteroid Toutatis
+ 2025143 Asteroid Itokawa
+ 2431010 Asteroid Ida
+ 9511010 Asteroid Gaspra
+
+
+Orientation Constants for the Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+
+ 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. )
+
+ 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 unchanged in the 2006 IAU report.
+
+
+ Current values:
+
+ \begindata
+
+ BODY199_POLE_RA = ( 281.01 -0.033 0. )
+ BODY199_POLE_DEC = ( 61.45 -0.005 0. )
+ BODY199_PM = ( 329.548 6.1385025 0. )
+
+ BODY199_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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:
+
+ Old 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 )
+
+
+ Current values:
+
+ 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
+
+
+ Values are given for the epoch 2000 and are from the final row
+ of the above table, which is from [8]. As shown by the table
+ these values constitute a low-accuracy approximation for epochs
+ not close to 2000.
+
+ \begindata
+
+ BODY399_N_GEOMAG_CTR_DIPOLE_LON = ( 288.43 )
+ BODY399_N_GEOMAG_CTR_DIPOLE_LAT = ( 79.54 )
+
+ \begintext
+
+
+Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 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:
+
+ Values are from the 2003 IAU report.
+
+
+ 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 )
+
+
+
+ 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 = ( 284.95 870.5366420 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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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 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.
+
+
+ \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
+ 29.80 -52.1
+ 706.64 151413.4
+ 57.44 151413.4 )
+ \begintext
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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
+
+
+
+Pluto
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ BODY999_POLE_RA = ( 313.02 0. 0. )
+ BODY999_POLE_DEC = ( 9.09 0. 0. )
+ BODY999_PM = ( 236.77 -56.3623195 0. )
+ BODY999_LONG_AXIS = ( 0. )
+
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+
+Orientation constants for the satellites
+--------------------------------------------------------
+
+
+Satellites of Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 from the 2003 IAU report.
+
+
+ body502_pole_ra = ( 268.08 -0.009 0. )
+ body502_pole_dec = ( 64.51 0.003 0. )
+ body502_pm = ( 35.67 101.3747235 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 )
+
+
+ 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+ Enceladus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Tethys
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+ Dione
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Rhea
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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. 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
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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 )
+
+ \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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Phoebe
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body609_pole_ra = ( 355.00 0. 0. )
+ body609_pole_dec = ( 68.70 0. 0. )
+ body609_pm = ( 304.70 930.8338720 0. )
+ body609_long_axis = ( 0. )
+
+ 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 2006 IAU report.
+
+ Current values:
+
+ \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. 0.023 )
+ BODY610_NUT_PREC_DEC = ( 0. -0.183 0. 0. 0. 0. 0. 0. 0.001 )
+ BODY610_NUT_PREC_PM = ( 0. 1.613 0. 0. 0. 0. 0. 0. -0.023 )
+
+ \begintext
+
+
+
+ Epimetheus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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. 0.086 0. )
+ BODY611_NUT_PREC_DEC = ( -0.356 0. 0. 0. 0. 0. 0. 0.005 0. )
+ BODY611_NUT_PREC_PM = ( 3.133 0. 0. 0. 0. 0. 0. -0.086 0. )
+
+ \begintext
+
+
+
+ Helene
+
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 report [1] states that values for Nereid are not
+ given because Nereid is not in synchronous rotation with Neptune
+ (p. 167).
+
+
+
+ Naiad
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2003 IAU report.
+
+ body901_pole_ra = ( 313.02 0. 0. )
+ body901_pole_dec = ( 9.09 0. 0. )
+ body901_pm = ( 56.77 -56.3623195 0. )
+ body901_long_axis = ( 0. )
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+Orientation constants for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+19P/Borrelly
+
+
+ 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
+
+
+
+9P/Tempel 1
+
+
+ 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
+
+
+Vesta
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2000004_POLE_RA = ( 301. 0. 0. )
+ BODY2000004_POLE_DEC = ( 41. 0. 0. )
+ BODY2000004_PM = ( 292. 1617.332776 0. )
+ BODY2000004_LONG_AXIS = ( 0. )
+
+ \begintext
+
+Eros
+
+ Old values:
+
+ Values are unchanged in the 2006 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
+
+
+Itokawa
+
+
+ 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
+
+
+
+Ida
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+Gaspra
+
+ Old values:
+
+ Values are unchanged in the 2006 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
+
+
+
+
+
+
+
+
+
+
+Radii of Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Value for the Sun is from the [3], page K7.
+
+ \begindata
+
+ BODY10_RADII = ( 696000. 696000. 696000. )
+
+ \begintext
+
+
+Mercury
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY199_RADII = ( 2439.7 2439.7 2439.7 )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY299_RADII = ( 6051.8 6051.8 6051.8 )
+
+ \begintext
+
+
+Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY399_RADII = ( 6378.14 6378.14 6356.75 )
+
+ \begintext
+
+
+Mars
+
+
+ Old values:
+
+ body499_radii = ( 3397. 3397. 3375. )
+
+ Current values:
+
+
+ The IAU report gives separate values for the north and south
+ polar radii:
+
+ north: 3373.19
+ south: 3379.21
+
+ We use the average of these values 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 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY599_RADII = ( 71492 71492 66854 )
+
+ \begintext
+
+
+
+Saturn
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY699_RADII = ( 60268 60268 54364 )
+
+ \begintext
+
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY799_RADII = ( 25559 25559 24973 )
+
+ \begintext
+
+
+
+Neptune
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ (Values are for the 1 bar pressure level.)
+
+ \begindata
+
+ BODY899_RADII = ( 24764 24764 24341 )
+
+ \begintext
+
+
+
+Pluto
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY999_RADII = ( 1195 1195 1195 )
+
+ \begintext
+
+
+
+
+Radii of Satellites
+--------------------------------------------------------
+
+
+Moon
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY301_RADII = ( 1737.4 1737.4 1737.4 )
+
+ \begintext
+
+
+
+Satellites of Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY401_RADII = ( 13.4 11.2 9.2 )
+ BODY402_RADII = ( 7.5 6.1 5.2 )
+
+ \begintext
+
+
+
+Satellites of Jupiter
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY501_RADII = ( 1829.4 1819.3 1815.7 )
+ BODY502_RADII = ( 1564.13 1561.23 1560.93 )
+ BODY503_RADII = ( 2632.4 2632.29 2632.35 )
+ BODY504_RADII = ( 2409.4 2409.2 2409.3 )
+ 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 )
+
+ \begintext
+
+ 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.
+ \begindata
+
+ BODY516_RADII = ( 21.5 21.5 21.5 )
+
+ \begintext
+
+
+
+Satellites of Saturn
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body601_radii = ( 209.1 196.2 191.4 )
+ body602_radii = ( 256.3 247.3 244.6 )
+ body603_radii = ( 535.6 528.2 525.8 )
+ body604_radii = ( 560 560 560 )
+ body605_radii = ( 764 764 764 )
+ body606_radii = ( 2575 2575 2575 )
+ body607_radii = ( 164 130 107 )
+ body608_radii = ( 718 718 718 )
+ body609_radii = ( 115 110 105 )
+ 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) was given in the
+ 2003 IAU report:
+
+ body612_radii = ( 17.5 --- --- )
+
+ The mean radius was 16km; we used this radius for all three axes, as
+ we do for the satellites for which only the mean radius is available.
+
+
+ body612_radii = ( 16 16 16 )
+ 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 )
+
+
+
+ Current values:
+
+ \begindata
+
+ 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 )
+
+ \begintext
+
+ 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.
+
+
+ \begindata
+
+ 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 )
+
+ \begintext
+
+
+ For Pan, only a mean radius is given in the 2006 report.
+
+ \begindata
+
+ BODY618_RADII = ( 10 10 10 )
+
+ \begintext
+
+
+
+Satellites of Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 IAU report.
+
+ Current values:
+
+ The 2000 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 2000
+ 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 from the 2003 IAU report.
+
+ BODY901_RADII = ( 593 593 593 )
+
+ Current values:
+
+ \begindata
+
+ BODY901_RADII = ( 605 605 605 )
+
+ \begintext
+
+
+
+Radii for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+19P/Borrelly
+
+
+ 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
+
+
+
+Halley
+
+
+ Current values:
+
+ \begindata
+
+ BODY1000036_RADII = ( 8.0 4.0 4.0 )
+
+ \begintext
+
+
+
+9P/Tempel 1
+
+
+ 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
+
+
+81P/Wild 2
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY1000107_RADII = ( 2.7 1.9 1.5 )
+
+ \begintext
+
+
+Ceres
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000001_RADII = ( 487.3 487.3 454.7 )
+
+ \begintext
+
+
+Vesta
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000004_RADII = ( 289. 280. 229. )
+
+ \begintext
+
+
+Toutatis
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2004179_RADII = ( 2.13 1.015 0.85 )
+
+ \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 2006 report.
+
+
+Mathilde
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000253_RADII = ( 33. 24. 23. )
+
+ \begintext
+
+Eros
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000433_RADII = ( 17.0 5.5 5.5 )
+
+ \begintext
+
+
+Itokawa
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2025143_RADII = ( 0.535 0.294 0.209 )
+
+ \begintext
+
+
+
+Gaspra
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY9511010_RADII = ( 9.1 5.2 4.4 )
+
+ \begintext
+
+
+
+
+Ida
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2431010_RADII = ( 26.8 12.0 7.6 )
+
+ \begintext
+
+
+
+===========================================================================
+End of file pck00009.tpc
+===========================================================================
+
+
+
diff --git a/tests/pytests/data/f704b28/vikingAddendum003.ti b/tests/pytests/data/f704b28/vikingAddendum003.ti
new file mode 100644
index 0000000000000000000000000000000000000000..b84e8a81eddcfdd2ab1919dab123bf5f08d5399a
--- /dev/null
+++ b/tests/pytests/data/f704b28/vikingAddendum003.ti
@@ -0,0 +1,23 @@
+\begindata
+INS-30001_TRANSX = ( 0.0, 0.0117647058823529, 0.0)
+INS-30001_TRANSY = ( 0.0, 0.0, 0.0117647058823529)
+INS-30001_ITRANSS = ( 0.0, 85.0, 0.0)
+INS-30001_ITRANSL = ( 0.0, 0.0, 85.0)
+
+INS-30002_TRANSX = ( 0.0, 0.0117647058823529, 0.0)
+INS-30002_TRANSY = ( 0.0, 0.0, 0.0117647058823529)
+INS-30002_ITRANSS = ( 0.0, 85.0, 0.0)
+INS-30002_ITRANSL = ( 0.0, 0.0, 85.0)
+
+\begintext
+These are the parameters for writing c-kernels. Isis will create ck
+with the same frame endpoints as the mission ck. For Viking1 the ck
+instrument frame is VO2_PLATFORM (-30000) and the ck reference frame
+is B1950 (2) or J2000 (1), depending on the ck used. The mdim2.0_rand
+ck is in J2000.
+
+\begindata
+INS-30001_CK_FRAME_ID=-30000
+INS-30001_CK_REFERENCE_ID=2
+INS-30002_CK_FRAME_ID=-30000
+INS-30002_CK_REFERENCE_ID=2
diff --git a/tests/pytests/data/f704b28/vo2_fict.tsc b/tests/pytests/data/f704b28/vo2_fict.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..f6c2ed107b663439690e01527eb8125e73642e66
--- /dev/null
+++ b/tests/pytests/data/f704b28/vo2_fict.tsc
@@ -0,0 +1,134 @@
+KPL/SCLK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "VO2_FICT.TSC"
+MISSION_NAME = VIKING
+SPACECRAFT_NAME = "VIKING ORBITER 2"
+DATA_SET_ID = "VO1/VO2-M-SPICE-6-V1.0"
+KERNEL_TYPE_ID = SCLK
+PRODUCT_ID = "VO2_FICT.TSC"
+PRODUCT_CREATION_TIME = 2000-04-21T10:53:21
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = {
+ PRIMARY_MISSION,
+ EXTENDED_MISSION,
+ CONTINUATION_MISSION
+ }
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = MARS
+INSTRUMENT_NAME = "N/A"
+NAIF_INSTRUMENT_ID = "N/A"
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = CLOCK_COEFFICIENTS
+ DESCRIPTION = "SCLK file implementing fictitious clock
+used to tag orientation data in the VO2 CK files. This SCLK file does NOT
+represent real Viking Orbiter 2 on-board clock but rather is a simple
+counter of milliseconds since 1 Jan 1976 00:00:00. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+Viking Orbiter 2 "fictitious" SCLK Kernel
+--------------------------------------------------------
+
+ This file contains the data necessary to convert between the
+ 'fictitious' Viking Orbiter 2 on-board clock times used as tags
+ for pointing instances in Viking Orbiter 2 CK files and ephemeris
+ time.
+
+ NAIF suggests that you do not modify this file. If you do modify
+ it, be sure to indicate this in the `Version' section below.
+
+
+Version
+--------------------------------------------------------
+
+ Version 1.0.1 -- April 20, 2000
+
+ Comments in the file were slightly reformatted and augmented.
+
+ Version 1.0.0 -- July 22, 1996
+
+
+Implementation notes
+--------------------------------------------------------
+
+ This SPICE SCLK file is constructed so that valid SCLK strings
+ are simply the number of seconds that have passed since the UTC
+ epoch 1 Jan 1976 00:00:00. Thus 288929292.827 simply represents
+ the epoch that occurs 288929292.827 seconds past the UTC epoch
+ 1 Jan 1976.
+
+ For all time, the clock runs at the same rate as Terrestrial
+ Dynamical Time (TDT). There is only one partition for this clock.
+
+ You must load this file into the kernel pool before using any
+ of the SPICELIB SCLK routines. The code fragment
+
+ CALL LDPOOL ( < name of this file > )
+
+ performs this task. To convert between ET and UTC, you will also
+ need to load a leapseconds kernel. The additional call to LDPOOL,
+
+ CALL LDPOOL ( < name of your leapsecond file > )
+
+ will accomplish this. Note that you must supply the actual names
+ of the files used on your system as arguments to LDPOOL. Because
+ the file names are system dependent, we do not list them here.
+
+ For more information, consult your SPICELIB required reading
+ files. The following areas are covered:
+
+ SCLK system SCLK required reading
+ Time systems and conversion TIME required reading
+ Kernel pool KERNEL required reading
+
+
+Kernel data
+--------------------------------------------------------
+
+ \begindata
+
+ SCLK_KERNEL_ID = ( @22-JUL-1996 )
+
+ SCLK_DATA_TYPE_30 = ( 1 )
+
+ SCLK01_TIME_SYSTEM_30 = ( 2 )
+ SCLK01_N_FIELDS_30 = ( 2 )
+ SCLK01_MODULI_30 = ( 10000000000 1000 )
+ SCLK01_OFFSETS_30 = ( 0 0 )
+ SCLK01_OUTPUT_DELIM_30 = ( 1 )
+
+ SCLK_PARTITION_START_30 = ( 0.0000000000000E+00 )
+ SCLK_PARTITION_END_30 = ( 1.00000000E+14 )
+ SCLK01_COEFFICIENTS_30 = ( 0.00000000E+00
+ @01-JAN-1976-00:00:47.184
+ 1 )
+
+ \begintext
+
+
+Contact Information
+--------------------------------------------------------
+
+ Contact NAIF node of the Planetary Data System if you have any
+ questions regarding this SCLK file.
+
+ Charles H. Acton, Jr
+ (818)-354-3869
+ chuck.acton@jpl.nasa.gov
+
+ Boris V. Semenov
+ (818)-354-8136
+ boris.semenov@jpl.nasa.gov
diff --git a/tests/pytests/data/f704b28/vo2_fsc.tsc b/tests/pytests/data/f704b28/vo2_fsc.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..d3b30a16469e17ab63230b7fbb1e186e39d68883
--- /dev/null
+++ b/tests/pytests/data/f704b28/vo2_fsc.tsc
@@ -0,0 +1,193 @@
+KPL/SCLK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "VO2_FSC.TSC"
+MISSION_NAME = VIKING
+SPACECRAFT_NAME = "VIKING ORBITER 2"
+DATA_SET_ID = "VO1/VO2-M-SPICE-6-V1.0"
+KERNEL_TYPE_ID = SCLK
+PRODUCT_ID = "VO2_FSC.TSC"
+PRODUCT_CREATION_TIME = 2000-04-21T10:53:21
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = {
+ PRIMARY_MISSION,
+ EXTENDED_MISSION,
+ CONTINUATION_MISSION
+ }
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = MARS
+INSTRUMENT_NAME = "N/A"
+NAIF_INSTRUMENT_ID = "N/A"
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = CLOCK_COEFFICIENTS
+ DESCRIPTION = "SCLK file containing linear piecewise
+function representing VO2 FSC on-board clock. This function was generated as
+the result of VO2 image time tags restoration. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+Viking Orbiter 2 Reconstructed Frame Start Count (FSC) SCLK file
+--------------------------------------------------------
+
+ This file contain data necessary to convert a Viking Orbiter 2
+ FSC count to the ET time corresponding to it. These data are
+ based on the results of VO2 image times reconstruction done at
+ NAIF/JPL. The process of this reconstruction is described in
+ detail in the "VO Image Time Reconstruction" document.
+
+ Note that the main purpose of this file is to store the
+ reconstructed FSC counter; the on-board clock defined by the
+ function in this file was not used to time tag any of the
+ orientation data in CK files.
+
+ To avoid confusion with the other VO2 clock used for time tagging,
+ the FSC on-board clock in this file was assigned the NAIF ID
+ code -30999.
+
+
+Version
+--------------------------------------------------------
+
+ Version 1.0.1 -- April 20, 2000
+
+ Comments in the file were slightly reformatted and augmented.
+
+ Version 1.0.0 -- July 22, 1996
+
+
+Implementation notes
+--------------------------------------------------------
+
+ This SPICE SCLK file is constructed so that valid SCLK strings
+ are the eight digit VO2 FSC count associated with each VO2 image.
+ Note that the actual "image time" (the time of the beginning,
+ middle or the end of exposure) has a significant offset from
+ the FSC tick start time. This offset depends on the exposure
+ duration and is described in the "VO Image Time Reconstruction"
+ document.
+
+ You must load this file into the kernel pool before using any
+ of the SPICELIB SCLK routines. The code fragment
+
+ CALL LDPOOL ( < name of this file > )
+
+ performs this task. To convert between ET and UTC, you will also
+ need to load a leapseconds kernel. The additional call to LDPOOL,
+
+ CALL LDPOOL ( < name of your leapsecond file > )
+
+ will accomplish this. Note that you must supply the actual names
+ of the files used on your system as arguments to LDPOOL. Because
+ the file names are system dependent, we do not list them here.
+
+ For more information, consult your SPICELIB required reading
+ files. The following areas are covered:
+
+ SCLK system SCLK required reading
+ Time systems and conversion TIME required reading
+ Kernel pool KERNEL required reading
+
+
+Kernel data
+--------------------------------------------------------
+
+\begindata
+
+ SCLK_KERNEL_ID = ( @22-JUL-1996 )
+
+ SCLK_DATA_TYPE_30999 = ( 1 )
+ SCLK01_TIME_SYSTEM_30999 = ( 2 )
+ SCLK01_N_FIELDS_30999 = ( 1 )
+ SCLK01_MODULI_30999 = ( 80000000 )
+ SCLK01_OFFSETS_30999 = ( 46442015 )
+ SCLK01_OUTPUT_DELIM_30999 = ( 1 )
+
+ SCLK_PARTITION_START_30999 = (
+ 0
+ 357985
+ 777985
+ 1057985
+ 1268246
+ 1457985
+ 2581493
+ 4701667
+ 5412787
+ 6557985
+ 6810335
+ 7107985
+ 9390838
+ 10007985
+ 10607985
+ 11107985
+ 12557985
+ )
+
+ SCLK_PARTITION_END_30999 = (
+ 357985
+ 777985
+ 1057985
+ 1268246
+ 1457985
+ 2581493
+ 4701667
+ 5412787
+ 6557985
+ 6810335
+ 7107985
+ 9390838
+ 10007985
+ 10607985
+ 11107985
+ 12557985
+ 13843304
+ )
+
+ SCLK01_COEFFICIENTS_30999 = (
+
+ 0 -738643373.631604 4.480001294
+ 357985 -737039600.324536 4.480001238
+ 777985 -735157999.769837 4.480001240
+ 1057985 -733903599.385587 4.480001244
+ 1268246 -732961629.770622 4.480001297
+ 1457985 -732111598.747130 4.480001301
+ 2581493 -727078280.882439 4.480001764
+ 4701667 -717579897.536827 4.480001764
+ 5412787 -714394078.461940 4.480001817
+ 6557985 -709263589.346238 4.480001599
+ 6810335 -708133060.592218 4.480001867
+ 7107985 -706799588.012369 4.480001868
+ 9390838 -696572402.934857 4.480001454
+ 10007985 -693807583.640654 4.480001937
+ 10607985 -691119582.502621 4.480001298
+ 11107985 -688879581.719291 4.480001364
+ 12557985 -682383579.531742 4.480001393
+ )
+
+\begintext
+
+
+Contact Information
+--------------------------------------------------------
+
+ Contact NAIF node of the Planetary Data System if you have any
+ questions regarding this SCLK file.
+
+ Charles H. Acton, Jr
+ (818)-354-3869
+ chuck.acton@jpl.nasa.gov
+
+ Boris V. Semenov
+ (818)-354-8136
+ boris.semenov@jpl.nasa.gov
diff --git a/tests/pytests/data/f704b28/vo2_sedr_ck2_0_sliced_-30000.xc b/tests/pytests/data/f704b28/vo2_sedr_ck2_0_sliced_-30000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..33400df90b7602d3ea7a86303ab395a1d0edba26
--- /dev/null
+++ b/tests/pytests/data/f704b28/vo2_sedr_ck2_0_sliced_-30000.xc
@@ -0,0 +1,691 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+'VO2 PLATFORM ATTITUDE; CREATED BY BVS/NAIF; 2006-FEB-09 '
+BEGIN_ARRAY 1 670
+'VO2 ATT. BASED ON GEM AND SEDR FILES '
+'12CAEC0F81^A'
+'12CB16DD0C^A'
+'-7530'
+'2'
+'2'
+'1'
+670
+'605119A622EED4^-1'
+'-2FEA9A6DF74D3^0'
+'FB2C40430DD82^0'
+'AC4E997ABF6BA^-1'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'255A22C8133C18^0'
+'-3261BEC01642EA^0'
+'F802BA3ECE62C^0'
+'9A78BF8F157808^-1'
+'0^0'
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+'12CB0B8218FFFE^A'
+'12CB0B93880002^A'
+'12CB0BA5190001^A'
+'12CB0BB687FFFD^A'
+'12CB0BC819FFFF^A'
+'12CB0BD9890002^A'
+'12CB0BEB2C0002^A'
+'12CB0BFC220002^A'
+'12CB0C0DAF0004^A'
+'12CB0C1F3BFFFE^A'
+'12CB0C30C7FFFD^A'
+'12CB0C4254FFFF^A'
+'12CB0C53E20001^A'
+'12CB0C656F0003^A'
+'12CB0C76FBFFFD^A'
+END_ARRAY 1 670
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /home/pgiroux/Desktop/f704b28.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/f704b28/vo2_v10.tf b/tests/pytests/data/f704b28/vo2_v10.tf
new file mode 100644
index 0000000000000000000000000000000000000000..0cff34eed43acbb0aabefa14e3f3bb57cf798ed4
--- /dev/null
+++ b/tests/pytests/data/f704b28/vo2_v10.tf
@@ -0,0 +1,470 @@
+KPL/FK
+
+Viking Orbiter 2 Frames Kernel
+===============================================================================
+
+ This frame kernel contains the complete set of frame definitions for
+ the Viking Orbiter 2 (VO2) spacecraft including definitions for the
+ spacecraft frame, instrument platform frame, and science instrument
+ frames.
+
+
+Version and Date
+-------------------------------------------------------------------------------
+
+ Version 1.0 -- December 1, 2005 -- Boris Semenov, NAIF
+
+ Initial Release.
+
+
+References
+-------------------------------------------------------------------------------
+
+ 1. ``Frames Required Reading''
+
+ 2. ``Kernel Pool Required Reading''
+
+ 3. ``C-Kernel Required Reading''
+
+ 4. VO2 Supplemental Experiment Data Record (SEDR) file, 1976-1980.
+
+ 5. Thomas C. Duxbury/JPL, March-July, 1996
+
+
+Contact Information
+-------------------------------------------------------------------------------
+
+ Boris V. 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/CSPICE/ICY routine FURNSH loads
+ a kernel file into the pool as shown below.
+
+ CALL FURNSH ( 'frame_kernel_name' ) SPICELIB/FORTRAN
+
+ furnsh_c ( "frame_kernel_name" ); CSPICE/C
+
+ cspice_furnsh, "frame_kernel_name" ICY/IDL
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+VO2 Frames
+-------------------------------------------------------------------------------
+
+ The following VO2 frames are defined in this kernel file:
+
+ Name Relative to Type NAIF ID
+ ====================== =================== ============ =======
+
+ Spacecraft frame:
+ -----------------
+ VO2_SPACECRAFT rel.to B1950 CK -30900
+
+ Instrument Platform frame:
+ --------------------------
+ VO2_PLATFORM rel.to B1950 CK -30000
+
+ Science Instrument frames:
+ --------------------------
+ VO2_VISA rel.to PLATFORM FIXED -30001
+ VO2_VISA_TD rel.to PLATFORM FIXED -30011
+ VO2_VISB rel.to PLATFORM FIXED -30002
+ VO2_VISB_TD rel.to PLATFORM FIXED -30012
+ VO2_IRTM rel.to PLATFORM FIXED -30003
+ VO2_MAWD rel.to PLATFORM FIXED -30004
+
+
+VO2 Frames Hierarchy
+-------------------------------------------------------------------------------
+
+ The diagram below shows VO2 frames hierarchy:
+
+
+ "B1950" INERTIAL
+ +-----------------------------------------------------------+
+ | | | |
+ | <--pck | <--ck | <--ck | <--pck
+ | | | |
+ V V | V
+ "IAU_MARS" "V01_SPACECRAFT" | "IAU_EARTH"
+ ----------- ---------------- | ------------
+ |
+ |
+ V
+ "VO2_PLATFORM"
+ +---------------------------------------------------------+
+ | | | | | |
+ | <--fixed | <--fixed fixed--> | | | | <--fixed
+ | | | | | |
+ V V V | | V
+ "VO2_IRTM" "VO2_MAWD" "VO2_VISA" | | "VO2_VISB"
+ ---------- ---------- ---------- | | ----------
+ | |
+ | |
+ fixed--> | | <--fixed
+ | |
+ V V
+ "VO2_VISA_TD" "VO2_VISB_TD"
+ ------------- -------------
+
+
+Spacecraft Bus Frame
+-------------------------------------------------------------------------------
+
+ The spacecraft frame is defined as follows:
+
+ [TBD]
+
+ This diagram illustrates the spacecraft bus frame:
+
+ [TBD]
+
+ Since the S/C bus attitude with respect to an inertial frame is
+ provided by a C kernel (see [3] for more information), this frame is
+ defined as a CK-based frame.
+
+ \begindata
+
+ FRAME_VO2_SPACECRAFT = -30900
+ FRAME_-30900_NAME = 'VO2_SPACECRAFT'
+ FRAME_-30900_CLASS = 3
+ FRAME_-30900_CLASS_ID = -30900
+ FRAME_-30900_CENTER = -30
+ CK_-30900_SCLK = -30
+ CK_-30900_SPK = -30
+
+ \begintext
+
+
+Instrument Platform Frame
+-------------------------------------------------------------------------------
+
+ The instrument platform frame is defined as follows:
+
+ [TBD]
+
+ This diagram illustrates the instrument platform frame:
+
+ [TBD]
+
+ Since the platform attitude with respect to an inertial frame is
+ provided by a C kernel (see [3] for more information), this frame is
+ defined as a CK-based frame.
+
+ \begindata
+
+ FRAME_VO2_PLATFORM = -30000
+ FRAME_-30000_NAME = 'VO2_PLATFORM'
+ FRAME_-30000_CLASS = 3
+ FRAME_-30000_CLASS_ID = -30000
+ FRAME_-30000_CENTER = -30
+ CK_-30000_SCLK = -30
+ CK_-30000_SPK = -30
+
+ \begintext
+
+
+VISA and VISB Frames
+-------------------------------------------------------------------------------
+
+ The frames for the Visual Imaging Subsystem Camera A (VISA) and
+ Camera B (VISB) -- VO2_VISA and VO2_VISB -- are defined as follows:
+
+ - Z axis is along the camera boresight;
+
+ - X axis is along detector lines and points toward the right
+ side of the image;
+
+ - Y axis completes the right hand frame;
+
+ - the origin of this frame is located at the camera focal point.
+
+ This diagram illustrates the camera frames:
+
+ [TBD]
+
+ Since the cameras were rigidly mounted on the instrument platform
+ their frames are defined as fixed offset frames with respect to the
+ platform frame.
+
+ The camera orientation with respect to the platform was specified in
+ [4] as the following three rotation angles:
+
+ T pl-cam = R (RASTER_ORIENTATION) R (CONE) R (-CROSS_CONE)
+ Z Y X
+
+ with the following angle values for each of the two cameras:
+
+ VISA:
+
+ CROSS_CONE = -0.679330, deg
+ CONE = -0.023270, deg
+ RASTER_ORIENTATION = 89.880691, deg
+
+ VISB:
+
+ CROSS_CONE = 0.663000, deg
+ CONE = -0.044000, deg
+ RASTER_ORIENTATION = 89.663790, deg
+
+ These angles are used in the frame definition below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the camera to the platform frame -- see [1].)
+
+ \begindata
+
+ FRAME_VO2_VISA = -30001
+ FRAME_-30001_NAME = 'VO2_VISA'
+ FRAME_-30001_CLASS = 4
+ FRAME_-30001_CLASS_ID = -30001
+ FRAME_-30001_CENTER = -30
+ TKFRAME_-30001_SPEC = 'ANGLES'
+ TKFRAME_-30001_RELATIVE = 'VO2_PLATFORM'
+ TKFRAME_-30001_ANGLES = ( -0.679330, 0.023270, -89.880691 )
+ TKFRAME_-30001_AXES = ( 1, 2, 3 )
+ TKFRAME_-30001_UNITS = 'DEGREES'
+
+ FRAME_VO2_VISB = -30002
+ FRAME_-30002_NAME = 'VO2_VISB'
+ FRAME_-30002_CLASS = 4
+ FRAME_-30002_CLASS_ID = -30002
+ FRAME_-30002_CENTER = -30
+ TKFRAME_-30002_SPEC = 'ANGLES'
+ TKFRAME_-30002_RELATIVE = 'VO2_PLATFORM'
+ TKFRAME_-30002_ANGLES = ( 0.663000, 0.044000, -89.663790 )
+ TKFRAME_-30002_AXES = ( 1, 2, 3 )
+ TKFRAME_-30002_UNITS = 'DEGREES'
+
+ \begintext
+
+ Thomas Duxbury provided a different set of angle values for the cameras
+ (see [5]):
+
+ VISA:
+
+ CROSS_CONE = -0.679300, deg
+ CONE = -0.023300, deg
+ RASTER_ORIENTATION = 89.880700, deg
+
+ VISB:
+
+ CROSS_CONE = 0.663000, deg
+ CONE = -0.044000, deg
+ RASTER_ORIENTATION = 89.663800, deg
+
+ To make this alignment solution available, two more frames parallel
+ to the camera frames and including the ``_TB'' suffix in the name
+ and defined below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the camera to the platform frame -- see [1].)
+
+ \begindata
+
+ FRAME_VO1_VISA_TD = -30011
+ FRAME_-30011_NAME = 'VO1_VISA_TD'
+ FRAME_-30011_CLASS = 4
+ FRAME_-30011_CLASS_ID = -30011
+ FRAME_-30011_CENTER = -30
+ TKFRAME_-30011_SPEC = 'ANGLES'
+ TKFRAME_-30011_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-30011_ANGLES = ( -0.679300, 0.023300, -89.880700 )
+ TKFRAME_-30011_AXES = ( 1, 2, 3 )
+ TKFRAME_-30011_UNITS = 'DEGREES'
+
+ FRAME_VO1_VISB_TD = -30012
+ FRAME_-30012_NAME = 'VO1_VISB_TD'
+ FRAME_-30012_CLASS = 4
+ FRAME_-30012_CLASS_ID = -30012
+ FRAME_-30012_CENTER = -30
+ TKFRAME_-30012_SPEC = 'ANGLES'
+ TKFRAME_-30012_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-30012_ANGLES = ( 0.663000, 0.044000, -89.663800 )
+ TKFRAME_-30012_AXES = ( 1, 2, 3 )
+ TKFRAME_-30012_UNITS = 'DEGREES'
+
+ \begintext
+
+
+IRTM Frame
+-------------------------------------------------------------------------------
+
+ The frame for the Infrared Thermal Mapper -- VO2_IRTM -- is defined
+ as follows:
+
+ [TBD]
+
+ This diagram illustrates the IRTM frame:
+
+ [TBD]
+
+ Since the IRTM instrument was rigidly mounted on the instrument
+ platform its frame is defined as fixed offset frames with respect to
+ the platform frame.
+
+ The instrument orientation with respect to the platform can be
+ specified using the following three rotation angles:
+
+ T pl-cam = R (RASTER_ORIENTATION) R (CONE) R (-CROSS_CONE)
+ Z Y X
+
+ with the nominal angle values:
+
+ CROSS_CONE = 0.0, deg
+ CONE = 0.0, deg
+ RASTER_ORIENTATION = 90.0, deg
+
+ These angles are used in the frame definition below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the instrument to the platform frame -- see
+ [1].)
+
+ \begindata
+
+ FRAME_VO2_IRTM = -30003
+ FRAME_-30003_NAME = 'VO2_IRTM'
+ FRAME_-30003_CLASS = 4
+ FRAME_-30003_CLASS_ID = -30003
+ FRAME_-30003_CENTER = -30
+ TKFRAME_-30003_SPEC = 'ANGLES'
+ TKFRAME_-30003_RELATIVE = 'VO2_PLATFORM'
+ TKFRAME_-30003_ANGLES = ( 0.0, 0.0, -90.0 )
+ TKFRAME_-30003_AXES = ( 1, 2, 3 )
+ TKFRAME_-30003_UNITS = 'DEGREES'
+
+ \begintext
+
+
+MAWD Frame
+-------------------------------------------------------------------------------
+
+ The frame for the Mars Atmosphere Water Detector (MAWD) -- VO2_MAWD
+ -- is defined as follows:
+
+ [TBD]
+
+ This diagram illustrates the MAWD frame:
+
+ [TBD]
+
+ Since the MAWD instrument was rigidly mounted on the instrument
+ platform its frame is defined as fixed offset frames with respect to
+ the platform frame.
+
+ The instrument orientation with respect to the platform can be
+ specified using the following three rotation angles:
+
+ T pl-cam = R (RASTER_ORIENTATION) R (CONE) R (-CROSS_CONE)
+ Z Y X
+
+ with the nominal angle values:
+
+ CROSS_CONE = 0.0, deg
+ CONE = 0.0, deg
+ RASTER_ORIENTATION = 90.0, deg
+
+ These angles are used in the frame definition below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the instrument to the platform frame -- see
+ [1].)
+
+ \begindata
+
+ FRAME_VO2_MAWD = -30004
+ FRAME_-30004_NAME = 'VO2_MAWD'
+ FRAME_-30004_CLASS = 4
+ FRAME_-30004_CLASS_ID = -30004
+ FRAME_-30004_CENTER = -30
+ TKFRAME_-30004_SPEC = 'ANGLES'
+ TKFRAME_-30004_RELATIVE = 'VO2_PLATFORM'
+ TKFRAME_-30004_ANGLES = ( 0.0, 0.0, -90.0 )
+ TKFRAME_-30004_AXES = ( 1, 2, 3 )
+ TKFRAME_-30004_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Viking Orbiter 2 NAIF ID Codes -- Definition Section
+========================================================================
+
+ This section contains name to NAIF ID mappings for the VO2. Once the
+ contents of this file is loaded into the KERNEL POOL, these mappings
+ become available within SPICE, making it possible to use names
+ instead of ID code in the high level SPICE routine calls.
+
+ Spacecraft and its structures:
+ ------------------------------
+
+ VIKING ORBITER 2 -30
+ VO2 -30
+
+ VO2_SPACECRAFT_BUS -30900
+ VO2_SC_BUS -30900
+ VO2_SPACECRAFT -30900
+
+ VO2_INSTRUMENT_PLATFORM -30000
+ VO2_PLATFORM -30000
+
+ Science Instruments:
+ --------------------
+
+ VO2_VISA -30001
+ VO2_VISB -30002
+
+ VO2_IRTM -30003
+
+ VO2_MAWD -30004
+
+ The mappings summarized in this table are implemented by the keywords
+ below.
+
+ \begindata
+
+ NAIF_BODY_NAME += ( 'VIKING ORBITER 2' )
+ NAIF_BODY_CODE += ( -30 )
+
+ NAIF_BODY_NAME += ( 'VO2' )
+ NAIF_BODY_CODE += ( -30 )
+
+ NAIF_BODY_NAME += ( 'VO2_SPACECRAFT_BUS' )
+ NAIF_BODY_CODE += ( -30900 )
+
+ NAIF_BODY_NAME += ( 'VO2_SC_BUS' )
+ NAIF_BODY_CODE += ( -30900 )
+
+ NAIF_BODY_NAME += ( 'VO2_SPACECRAFT' )
+ NAIF_BODY_CODE += ( -30900 )
+
+ NAIF_BODY_NAME += ( 'VO2_INSTRUMENT_PLATFORM' )
+ NAIF_BODY_CODE += ( -30000 )
+
+ NAIF_BODY_NAME += ( 'VO2_PLATFORM' )
+ NAIF_BODY_CODE += ( -30000 )
+
+ NAIF_BODY_NAME += ( 'VO2_VISA' )
+ NAIF_BODY_CODE += ( -30001 )
+
+ NAIF_BODY_NAME += ( 'VO2_VISB' )
+ NAIF_BODY_CODE += ( -30002 )
+
+ NAIF_BODY_NAME += ( 'VO2_IRTM' )
+ NAIF_BODY_CODE += ( -30003 )
+
+ NAIF_BODY_NAME += ( 'VO2_MAWD' )
+ NAIF_BODY_CODE += ( -30004 )
+
+ \begintext
diff --git a/tests/pytests/data/f735a00/f735a00_0.xsp b/tests/pytests/data/f735a00/f735a00_0.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..7832281a0faf5fc3b8773192b01a57c0b830873b
--- /dev/null
+++ b/tests/pytests/data/f735a00/f735a00_0.xsp
@@ -0,0 +1,634 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 433
+'22jun78 '
+'-287DFD03CFC8F^8'
+'-287DF201F2585C^8'
+'-1B'
+'4'
+'E'
+'1'
+433
+'-287DFC3051C54E^8'
+'227C5A4E882^3'
+'44F8B49D104^3'
+'67750EEB986^3'
+'89F1693A208^3'
+'AC6DC388A8A^3'
+'CEEA1DD730C^3'
+'F1667825B8E^3'
+'113E2D27441^4'
+'1365F2CC2C92^4'
+'158DB8711514^4'
+'17B57E15FD96^4'
+'18C960E871D7^4'
+'19DD43BAE618^4'
+'1AF1268D5A59^4'
+'1C05095FCE9A^4'
+'AF15B76B3F26F^3'
+'A09FCC652453^0'
+'-6DB934FFDF948^4'
+'-9F5FB8B76B97E^0'
+'-1F8C429AF67E63^4'
+'-EF9F0DA9BA977^-1'
+'-4F882770621108^-4'
+'-71915DAA94B2A4^-5'
+'9C62E3E87AF6E8^-6'
+'-152E78F23E325E^-6'
+'35C1C68853D784^-7'
+'-A7A10E4EF6A59^-8'
+'26CBE61FC5A628^-8'
+'-A8708A28BB733^-9'
+'34DB3B7FC73014^-9'
+'-12FC1DD002F78C^-9'
+'7BD314D266AB58^-A'
+'-38E6FA4A36DEE8^-A'
+'1B766CAE0F4F8F^-A'
+'-E0EA7622BE0EF^-B'
+'740F49^-B'
+'31D6BA6FA756DC^-3'
+'-151F19C1110412^-4'
+'172239BEB281AA^-5'
+'-22529228556F68^-6'
+'454EB2A84958D4^-7'
+'-AEE4693F89F85^-8'
+'216ECDD616841^-8'
+'-78615E000913F8^-9'
+'1F3844767B583A^-9'
+'-920B2728E9AD6^-A'
+'30569E239BA3AC^-A'
+'-E93C1FB3D9744^-B'
+'A233CE^-B'
+'0^0'
+'0^0'
+'E54338B725CDC8^-4'
+'-808C542A378EE8^-5'
+'939E2DFEE5C7B8^-6'
+'-F1CE2CE465209^-7'
+'20DC3CCBAC69D4^-7'
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+'1298A6D4CF7C82^-8'
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+'14EA565DE27BE4^-9'
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+'-1089E572CAB1C9^-A'
+'93B32B21C5D35^-B'
+'77D1535F50231^-B'
+'0^0'
+'F^1'
+'E^1'
+'C^1'
+'D^1'
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+'-4E07B^-B'
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+'B11328890E058^-B'
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+'-728EFC093B8D7^4'
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+'-148FCE5CF5C^-7'
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+'0^0'
+'-66B022E077AD84^-4'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'2D686366A67D4A^-3'
+'-40009C8962^-7'
+'-40009C8962^-7'
+'0^0'
+'2D686366A67D4A^-3'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'CA6FFDC88975D8^-4'
+'-1824C23449^-7'
+'-1824C23449^-7'
+'0^0'
+'CA6FFDC88975D8^-4'
+'0^0'
+'0^0'
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+'-287DF3BDD476C6^8'
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+'CEEA1DD730C^3'
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+'1365F2CC2C92^4'
+'158DB8711514^4'
+'17B57E15FD96^4'
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+'1C05095FCE9A^4'
+'1E2CCF04B71C^4'
+'205494A99F9E^4'
+'1031F2C3A20E24^4'
+'9D997F62CF02C^0'
+'-728FD71743C508^4'
+'-864798F9C545C^0'
+'-1FEC24BE01BE31^4'
+'-7DF70D7E1268BC^-1'
+'-66B406B08A4FE8^-4'
+'-29AD88ADFA100E^-7'
+'1077BC0623CB82^-A'
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+'0^0'
+'2D67A1ABA18B44^-3'
+'-81BB5FF47F5BB8^-7'
+'2F78AD25225A6E^-A'
+'-1358^-D'
+'2D686366A67D4A^-3'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'CA6B6C7DCAC56^-4'
+'-30F0487326F6AE^-7'
+'122AC6CD23B6D6^-A'
+'-83D^-E'
+'CA6FFDC88975D8^-4'
+'0^0'
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+'1E2CCF04B71C^4'
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+'127B64DD6400EB^4'
+'9C0A16692E599^0'
+'-74719420CC8564^4'
+'-7BE1A022F9296^0'
+'-20041DA53F0C46^4'
+'-4FEA6672E27F9C^-1'
+'-6F224AB0130978^-4'
+'-25A116D1CE927E^-5'
+'10AFA56FEA6237^-6'
+'-C9D83F7B0A92D8^-8'
+'898B8413DBF848^-9'
+'-653BDA4827DA3C^-A'
+'4B453F688466C^-B'
+'-395C54^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'2BC28C0270B40C^-3'
+'-75A2B4E1017E04^-5'
+'32CBE7AF3D3068^-6'
+'-17F1CD1E2137C3^-7'
+'D8346CE9FF623^-9'
+'-81E775DA784DE^-A'
+'525E10448FDE3^-B'
+'-32BF6^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'C07F38589AD1F^-4'
+'-2C5741E439D146^-5'
+'133D7FF797DEDF^-6'
+'-A150B2F0B09738^-8'
+'6013B67A6B749^-9'
+'-3DB0E73289FE48^-A'
+'297C805EE5CA7A^-B'
+'-1C898^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'9^1'
+'8^1'
+'7^1'
+'8^1'
+'-287DFC3051C582^8'
+'-287DF3C^8'
+'-287DF3BF760E94^8'
+'-287DF3BDD476F2^8'
+'-287DF378ED27E6^8'
+'-287DF0022E762^8'
+'6^1'
+END_ARRAY 1 433
+BEGIN_ARRAY 2 39
+'DE-0721LE-0721 '
+'-287DFD03CFC8F^8'
+'-287DF201F2585C^8'
+'A'
+'0'
+'1'
+'2'
+39
+'-2875B0C^8'
+'A8C^5'
+'AC3D7CB77DDCD^5'
+'22DD35A9AFDBDE^4'
+'-D5CA2734F1FCE^1'
+'A0B502418872A8^-1'
+'2EF71655C6B0F6^-1'
+'-4D33BAD60F483^-2'
+'3F4064180DB726^-3'
+'97FCA03D617BF^-4'
+'-2CA793D85A09C^-4'
+'4DC3E7CA6EF588^-5'
+'4644C189321A34^-7'
+'-7FD7ABE4C4DFDC^5'
+'F108D2E4E03F9^3'
+'142C70A32BAD5B^2'
+'-354CFA25CFA2CE^0'
+'1DCFF0D39314F5^-1'
+'12E36A6B063B73^-2'
+'-7E5D32363242DC^-3'
+'10FA3F9B71DCD3^-3'
+'-A6718EFD7C574^-5'
+'-3718DF13579132^-5'
+'CF066909006E58^-6'
+'-3C91F8173D173E^5'
+'570193D309EE9^3'
+'92F3652F409B08^1'
+'-1A1CCC41A5E191^0'
+'AF616C630E437^-2'
+'119850853207CE^-2'
+'-4A0D67DE16AD8^-3'
+'815BE67E5FDA98^-4'
+'-EC36E1960368^-6'
+'-257FEBA6229DD4^-5'
+'6E20CF9FCB9EE4^-6'
+'-28803CC^8'
+'1518^6'
+'23^2'
+'1^1'
+END_ARRAY 2 39
+BEGIN_ARRAY 3 39
+'DE-0721LE-0721 '
+'-287DFD03CFC8F^8'
+'-287DF201F2585C^8'
+'4'
+'0'
+'1'
+'2'
+39
+'-28803CC^8'
+'1518^6'
+'-E5EAE27440F3C^7'
+'5BD189B93FB1E^6'
+'FE3618F9424968^5'
+'-2FD48EC5E5BD1^3'
+'-12683B83E8210F^3'
+'-2AF2CE9D9DF1F6^1'
+'-B8A1D5CF80ACF^-1'
+'13A36CE79CB407^-2'
+'F46015645D4AD^-4'
+'-13D806CF4E54B^-4'
+'1A8D2CBFB41BAB^-6'
+'-20BEAEA7FDFB94^7'
+'-1A264A82B9749F^7'
+'23ABBF14364814^5'
+'4EBB77339BFF78^4'
+'3DE85EB8B1A3C8^2'
+'-135F9C8CF78BB3^1'
+'-B182A4D6BB98E8^-1'
+'-51EE302A7898E^-2'
+'-136A2C396F1108^-3'
+'39BE63F95C7B1^-5'
+'2CBCEE46FAD5FE^-5'
+'-8C7F8646FA5268^6'
+'-C263F2A08DDD88^6'
+'979B5833C3625^4'
+'2431430C6D00FE^4'
+'245E1E50540A98^2'
+'-7BA06A115F13A8^0'
+'-4C4C4B3077CDC4^-1'
+'-25A29AC98720BC^-2'
+'-96ED02723DE9B8^-4'
+'-9EC540801679C^-6'
+'12571425850D1F^-5'
+'-289554C^8'
+'2A3^6'
+'23^2'
+'1^1'
+END_ARRAY 3 39
+BEGIN_ARRAY 4 54
+'MAR097 '
+'-287DFD03CFC8F^8'
+'-287DF201F2585C^8'
+'1F3'
+'4'
+'1'
+'3'
+54
+'-287E185^8'
+'2A3^4'
+'2BCAF6A6A13A4A^-3'
+'8EFE351F45F4C^-3'
+'-796AD624F8BA1^-4'
+'-3BE638DB8AEF12^-3'
+'1807051B01932^-5'
+'4CB6C184A9A3D8^-4'
+'14A0193B4053A8^-5'
+'-1D7CE27DFCEAD^-5'
+'FCFCD4DA1E2598^-4'
+'437252F138D22^-3'
+'7C3CA80D357EA8^-3'
+'-FE257D5B1D00F8^-4'
+'-1367670D565C38^-3'
+'103DF03129F098^-4'
+'E69F539069FBA^-5'
+'2E29B7045B518^-6'
+'-DF2A547DE173D^-4'
+'-30D438E13C719A^-3'
+'45F424B25863D8^-3'
+'1A57BCB9195BE9^-3'
+'-A571269E59C258^-4'
+'-23E0E57AE0294C^-4'
+'6E51E84DF7106^-5'
+'12A0F0B824FC^-5'
+'-5226C27319672^-7'
+'-ADC580FC90D458^-7'
+'-76BB54CBC00F7C^-6'
+'A6C4F7222866^-8'
+'11928B05B2B45C^-6'
+'5DDE50B2A30D3C^-8'
+'-9C91C83508489^-8'
+'0^0'
+'976454F1A5192^-7'
+'85B2F66842C64^-6'
+'-203C48F702FA58^-6'
+'-36C5E1171BA73C^-6'
+'3E8E79560B86C8^-7'
+'4199688D33C398^-7'
+'F51BB072279DC^-9'
+'0^0'
+'764ECB7D37907^-7'
+'4CB5FB968352AC^-6'
+'33D37FD6FD5FBC^-6'
+'-1D69557E1C8EC1^-6'
+'-81E3FD07D2F6B^-7'
+'1F6140F0A14C56^-7'
+'62E94E888AB9D4^-8'
+'0^0'
+'-287E428^8'
+'546^4'
+'32^2'
+'1^1'
+END_ARRAY 4 54
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /home/pgiroux/Desktop/f735a00/f735a00_0.bsp LOG FILE
+
+; Created 2019-09-11/12:19:02.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /home/pgiroux/Desktop/f735a00/f735a00_0.bsp
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/viking1/kernels/spk/viking1b.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -27
+ BEGIN_TIME = 1978 JUN 22 16:55:39.004
+ END_TIME = 1978 JUN 22 17:42:36.869
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/spk/mar097.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 4, 10, 499
+ BEGIN_TIME = 1978 JUN 22 16:55:39.004
+ END_TIME = 1978 JUN 22 17:42:36.869
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/f735a00/f735a00_isis3.lbl b/tests/pytests/data/f735a00/f735a00_isis3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..9ba2057d888f944e4d5c8a3412df187dc3a4853b
--- /dev/null
+++ b/tests/pytests/data/f735a00/f735a00_isis3.lbl
@@ -0,0 +1,103 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 1204
+ TileLines = 1056
+
+ Group = Dimensions
+ Samples = 1204
+ Lines = 1056
+ Bands = 1
+ End_Group
+
+ Group = Pixels
+ Type = UnsignedByte
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftName = VIKING_ORBITER_1
+ InstrumentId = VISUAL_IMAGING_SUBSYSTEM_CAMERA_B
+ TargetName = MARS
+ StartTime = 1978-06-22T17:26:00
+ ExposureDuration = 0.067880 <seconds>
+ SpacecraftClockCount = 40031801
+ FloodModeId = ON
+ GainModeId = HIGH
+ OffsetModeId = ON
+ End_Group
+
+ Group = Archive
+ DataSetId = VO1/VO2-M-VIS-2-EDR-V2.0
+ ProductId = 735A00
+ MissonPhaseName = CONTINUATION_MISSION
+ ImageNumber = 40031801
+ OrbitNumber = 735
+ End_Group
+
+ Group = BandBin
+ FilterName = RED
+ FilterId = 6
+ Center = 0.59 <micrometers>
+ Width = 0.15 <micrometers>
+ End_Group
+
+ Group = Kernels
+ NaifFrameCode = -27002
+ CameraVersion = 1
+ End_Group
+
+ Group = Reseaus
+ Line = (5, 6, 8, 9, 10, 11, 12, 13, 14, 14, 15, 133, 134, 135, 137,
+ 138, 139, 140, 141, 141, 142, 143, 144, 263, 264, 266, 267,
+ 268, 269, 269, 270, 271, 272, 273, 393, 393, 395, 396, 397,
+ 398, 399, 399, 400, 401, 402, 403, 523, 524, 525, 526, 527,
+ 527, 528, 529, 530, 530, 532, 652, 652, 654, 655, 656, 657,
+ 657, 658, 659, 660, 661, 662, 781, 783, 784, 785, 786, 787,
+ 788, 788, 789, 790, 791, 911, 912, 913, 914, 915, 916, 917,
+ 918, 918, 919, 920, 921, 1040, 1041, 1043, 1044, 1045, 1045,
+ 1046, 1047, 1047, 1048, 1050)
+ Sample = (24, 142, 259, 375, 491, 607, 723, 839, 954, 1070, 1185, 24,
+ 84, 201, 317, 433, 549, 665, 780, 896, 1011, 1127, 1183, 25,
+ 142, 259, 375, 492, 607, 722, 838, 953, 1068, 1183, 25, 84,
+ 201, 317, 433, 549, 665, 779, 895, 1010, 1125, 1182, 25, 143,
+ 259, 375, 491, 607, 722, 837, 952, 1067, 1182, 25, 84, 201,
+ 317, 433, 548, 664, 779, 894, 1009, 1124, 1181, 25, 142, 258,
+ 374, 490, 605, 720, 835, 951, 1066, 1180, 24, 83, 200, 316,
+ 431, 547, 662, 776, 892, 1007, 1122, 1179, 23, 140, 257, 373,
+ 488, 603, 718, 833, 948, 1063, 1179)
+ Type = (1, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 6, 4, 5, 5, 5, 5, 5, 5, 5, 5, 5, 6)
+ Valid = (0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0)
+ Template = $viking1/reseaus/vo1.visb.template.cub
+ Status = Nominal
+ End_Group
+ End_Object
+
+ Object = Label
+ Bytes = 65536
+ End_Object
+
+ Object = History
+ Name = IsisCube
+ StartByte = 1336961
+ Bytes = 444
+ End_Object
+
+ Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 1337405
+ Bytes = 1988
+ End_Object
+ End
diff --git a/tests/pytests/data/f735a00/f735a00_pds3.lbl b/tests/pytests/data/f735a00/f735a00_pds3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..4591dc7f780fc402d08151fb531bbdb7e9ccd4b3
--- /dev/null
+++ b/tests/pytests/data/f735a00/f735a00_pds3.lbl
@@ -0,0 +1,1632 @@
+CCSD3ZF0000100000001NJPL3IF0PDS200000001 = SFDU_LABEL
+/* FILE FORMAT AND LENGTH */
+RECORD_TYPE = VARIABLE_LENGTH
+RECORD_BYTES = 1204
+FILE_RECORDS = 2176
+LABEL_RECORDS = 60
+/* POINTERS TO START RECORDS OF MAJOR OBJECTS IN FILE */
+^IMAGE_HISTOGRAM = 61
+^ENCODING_HISTOGRAM = 62
+^ENGINEERING_TABLE = 64
+^LINE_HEADER_TABLE = 65
+^IMAGE = 1121
+/* IMAGE DESCRIPTION */
+DATA_SET_ID = 'VO1/VO2-M-VIS-2-EDR-V2.0'
+SPACECRAFT_NAME = VIKING_ORBITER_1
+MISSION_PHASE_NAME = CONTINUATION_MISSION
+TARGET_NAME = MARS
+IMAGE_ID = '735A00'
+IMAGE_NUMBER = 40031801
+IMAGE_TIME = 1978-06-22T17:26:00Z
+EARTH_RECEIVED_TIME = 1978-06-24T06:19:00Z
+ORBIT_NUMBER = 735
+INSTRUMENT_NAME = VISUAL_IMAGING_SUBSYSTEM_CAMERA_B
+GAIN_MODE_ID = HIGH
+FLOOD_MODE_ID = ON
+OFFSET_MODE_ID = ON
+FILTER_NAME = RED
+EXPOSURE_DURATION = 0.067880 <SECONDS>
+NOTE = "LOW RESOLUTION STEREO SEQUENCE"
+/* DESCRIPTION OF THE OBJECTS CONTAINED IN FILE */
+OBJECT = IMAGE_HISTOGRAM
+ ITEMS = 256
+ ITEM_TYPE = VAX_INTEGER
+ ITEM_BITS = 32
+END_OBJECT
+OBJECT = ENCODING_HISTOGRAM
+ ITEMS = 511
+ ITEM_TYPE = VAX_INTEGER
+ ITEM_BITS = 32
+END_OBJECT
+OBJECT = ENGINEERING_TABLE
+ ROWS = 1
+ ROW_BYTES = 152
+CCSD3ZF0000100000001NJPL3IF0PDS200000001 = SFDU_LABEL
+
+OBJECT = ENGINEERING_TABLE_STRUCTURE
+ INTERCHANGE_FORMAT = BINARY
+ BYTES = 152
+ NOTE = "This structure describes the format of
+ the engineering record that is included in each image file.
+ This record contains the first 152 bytes of data extracted from
+ the Mission and Test Imaging System (MTIS) header record on each
+ file of an imaging EDR tape."
+
+ OBJECT = COLUMN
+ NAME = MTIS_RECORD_ID
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 1
+ BYTES = 2
+ DESCRIPTION = "Mission and Test Imaging System record
+ ID."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PHYSICAL_SEQUENCE_NUMBER
+ DATA_TYPE = VAX_UNSIGNED_INTEGER
+ START_BYTE = 3
+ BYTES = 2
+ DESCRIPTION = "Physical sequence number on Experiment
+ Data Record tape. Not used."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LOGICAL_SEQUENCE_NUMBER
+ DATA_TYPE = VAX_UNSIGNED_INTEGER
+ START_BYTE = 5
+ BYTES = 2
+ DESCRIPTION = "Logical sequence number on Experiment
+ Data Record tape. Not used."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_ERT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 7
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time year and day
+ value. Time of first line segment in the file containing valid
+ data. This field is NOT stored in VAX least significant byte
+ first format."
+
+ OBJECT = BIT_COLUMN
+ NAME = FIRST_ERT_YEAR
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 1
+ BITS = 7
+ DESCRIPTION = "Earth Received Time year of century
+ (1900). Time of first line record in the file containing valid
+ data. This field is often incorrect."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FIRST_ERT_DAY
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 7
+ BITS = 9
+ DESCRIPTION = "Earth Received Time day of year."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_ERT_MINUTE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 9
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time minute of day."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_ERT_MILLISECOND
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 11
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time millisecond of
+ minute."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_ERT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 13
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time year and day
+ value. Time of last line segment of the file containing valid
+ data."
+
+ OBJECT = BIT_COLUMN
+ NAME = LAST_ERT_YEAR
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 1
+ BITS = 7
+ DESCRIPTION = "Earth Received Time year of century
+ (1900). This field is often incorrect."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = LAST_ERT_DAY
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BIT = 8
+ BITS = 9
+ DESCRIPTION = "Earth Received Time day of year."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_ERT_MINUTE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 15
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time minute of day."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_ERT_MILLISECOND
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 17
+ BYTES = 2
+ DESCRIPTION = "Earth Received Time millisecond of
+ minute."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_FDS_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 19
+ BYTES = 4
+ DESCRIPTION = "Flight Data Subsystem count for the
+ first line segment of the file containing valid data. Note that
+ this may not correspond to the FDS count for line 1, segment 1."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_FDS_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 23
+ BYTES = 4
+ DESCRIPTION = "Flight Data Subsystem count for the
+ last line segment of the file containing valid data. Note that
+ this may not correspond to the FDS count for segment 7 of line
+ 1056."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = EDR_ID
+ DATA_TYPE = CHARACTER
+ START_BYTE = 27
+ BYTES = 6
+ DESCRIPTION = "Tape reel identifier of the original
+ EDR tape for this image."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = EDR_FILE_NUMBER
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 33
+ BYTES = 2
+ DESCRIPTION = "File number of image on original EDR
+ tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FILL_IN
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 34
+ BYTES = 1
+ DESCRIPTION = "Value used to fill in missing samples
+ (always zero)."
+ END_OBJECT = COLUMN
+ OBJECT = COLUMN
+ NAME = TRACK_PRESENCE_MASK
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 36
+ BYTES = 1
+ DESCRIPTION = "Mask indicating which tracks are
+ present in the image. The nominal value is HEX 7F, indicating
+ that all seven tracks are present."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = AVERAGE_PIXEL
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 37
+ BYTES = 2
+ DESCRIPTION = "Average pixel value for image."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_1
+ DATA_TYPE = CHARACTER
+ START_BYTE = 39
+ BYTES = 4
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MINIMUM_SNR
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 43
+ BYTES = 2
+ FACTOR = 0.03125
+ DESCRIPTION = "Minimum signal to noise ratio. The
+ minimum noise level found for the scan lines. Divide by 32 to
+ get the actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MAXIMUM_SNR
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 45
+ BYTES = 2
+ FACTOR = 0.03125
+ DESCRIPTION = "Maximum signal to noise ratio. The
+ maximum noise level found for the scan lines. Divide by 32 to
+ get the actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_2
+ DATA_TYPE = CHARACTER
+ START_BYTE = 47
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MINIMUM_AGC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 49
+ BYTES = 2
+ FACTOR = 0.0625
+ DESCRIPTION = "Automatic gain control minimum.
+ Divide by 16 to get actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = MAXIMUM_AGC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 51
+ BYTES = 2
+ FACTOR = 0.0625
+ DESCRIPTION = "Automatic gain control maximum.
+ Divide by 16 to get actual value."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_3
+ DATA_TYPE = CHARACTER
+ START_BYTE = 53
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 55
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that contain some valid data (maximum is 7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FULLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 57
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that were fully synchronized (maximum is 7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PARTLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 59
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that were partly synchronized (maximum is 7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI0_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 61
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 0 (maximum is 7 x 1056).
+ DQI0 indicates bad data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI1_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 63
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 1 (maximum is 7 x 1056).
+ DQI1 means SNR low, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI2_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 65
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 2 (maximum is 7 x 1056).
+ DQI2 means SNR good, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI3_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 67
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 3 (maximum is 7 x 1056).
+ DQI3 means SNR low, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI4_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 69
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with a data quality indicator of 4 (maximum is 7 x 1056).
+ DQI4 means SNR good, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FDS_CORRECTIONS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 71
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with corrected FDS counts."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PNERROR_CORRECTIONS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 73
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with corrected pseudonoise codes."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = ADJUSTED_PNERROR_CORRECTIONS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 75
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file with corrected pseudonoise codes adjusted based on the
+ number of line segments processed versus the total in a full
+ image (7 x 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNREADABLE_RECORDS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 77
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ file that could not be read from the Master Data Record tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LOGICAL_SEQUENCE_BREAKS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 79
+ BYTES = 2
+ DESCRIPTION = "Total number of breaks in logical
+ sequence number in reading the System/Master Data Record tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DATA_BREAKS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 81
+ BYTES = 2
+ DESCRIPTION = "Total number of breaks in data
+ sequence in reading the System/Master Data Record tape."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_4
+ DATA_TYPE = CHARACTER
+ START_BYTE = 83
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINES
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 85
+ BYTES = 2
+ DESCRIPTION = "Total number of lines in the file that
+ contain some valid data (nominal is 1056)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FULL_LINES
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 87
+ BYTES = 2
+ DESCRIPTION = "Number of lines in the file that are
+ composed of seven line segments."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PARTIAL_LINES
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 89
+ BYTES = 2
+ DESCRIPTION = "Total number of line records in the
+ file that contain some valid data but are not composed of seven
+ line segments."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FIRST_LINE_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 91
+ BYTES = 2
+ DESCRIPTION = "First line in image containing valid
+ data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LAST_LINE_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 93
+ BYTES = 2
+ DESCRIPTION = "Last line in image containing valid
+ data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_5
+ DATA_TYPE = CHARACTER
+ START_BYTE = 95
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = IMAGE_ID
+ DATA_TYPE = CHARACTER
+ START_BYTE = 97
+ BYTES = 6
+ DESCRIPTION = "Image identifier (PICNO) for this
+ image, formatted OOOSNN, where OOO is orbit number, S is
+ spacecraft identifier (A for Viking Orbiter 1 prime and extended
+ missions; B for Viking Orbiter 2; and S for Viking Orbiter 1
+ Survey mission)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VRP_RUN_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 103
+ BYTES = 2
+ DESCRIPTION = "Viking Reconstruction Processing run
+ number."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DISK_ID
+ DATA_TYPE = CHARACTER
+ START_BYTE = 105
+ BYTES = 6
+ DESCRIPTION = "MTIS disk identifier of the original
+ EDR file for this image."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = UNUSED_6
+ DATA_TYPE = CHARACTER
+ START_BYTE = 111
+ BYTES = 2
+ DESCRIPTION = "Unused."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = TRANSMITTED_CODE_WORD1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 113
+ BYTES = 2
+ DESCRIPTION = "Transmitted command code word for the
+ image."
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ START_BIT = 1
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Set to 1 if data not present for the
+ following measurements."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ START_BIT = 3
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Data quality indicator associated with
+ code word values. Where: 0 is bad data; 1 is SNR low, GCF block
+ error; 2 is SNR good, GCF block bad; 3 is SNR low, GCF block
+ good; 4 is SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = CATHODE_CURRENT_FLAG
+ START_BIT = 7
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Cathode current off (0) or on (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = GAIN_FLAG
+ START_BIT = 8
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Gain mode low (0) or high (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = LIGHT_FLOOD_FLAG
+ START_BIT = 9
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Light flood off (0) or on (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FILTER_STEP
+ START_BIT = 10
+ BITS = 2
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Filter step indicator."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = EXPOSURE_CODE
+ START_BIT = 12
+ BITS = 5
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Exposure interval code."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = TRANSMITTED_CODE_WORD2
+ DATA_TYPE = INTEGER
+ START_BYTE = 115
+ BYTES = 2
+ DESCRIPTION = "Transmitted command code word 2 for
+ this image."
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ START_BIT = 1
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Set to 1 if data not present for the
+ following measurements."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ START_BIT = 3
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Data quality indicator associated with
+ code word values. where: 0 is bad data; 1 is SNR low, GCF block
+ error; 2 is SNR good, GCF block bad; 3 is SNR low, GCF block
+ good; 4 is SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FILTER_NUMBER
+ START_BIT = 10
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Filter number: where 1 is blue; 2 is
+ minus blue; 3 is violet; 4 is clear; 5 is green; and 6 is red."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = CAMERA_SERIAL_NUMBER
+ START_BIT = 13
+ BITS = 4
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Visual Imaging Subsystem camera serial
+ number."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = RECEIVED_CODE_WORD1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 117
+ BYTES = 2
+ DESCRIPTION = "Received command code word for the
+ image."
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ START_BIT = 1
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Set to 1 if data not present for the
+ following measurements."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ START_BIT = 3
+ BITS = 3
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Data quality indicator associated with
+ code word values. where: 0 is bad data; 1 is SNR low, GCF block
+ error; 2 is SNR good, GCF block bad; 3 is SNR low, GCF block
+ good; 4 is SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = CATHODE_CURRENT_FLAG
+ START_BIT = 7
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Cathode current (beam) off (0) or on
+ (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = GAIN_FLAG
+ START_BIT = 8
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Gain mode low (0) or high (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = LIGHT_FLOOD_FLAG
+ START_BIT = 9
+ BITS = 1
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Light flood off (0) or on (1)."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = FILTER_STEP
+ START_BIT = 10
+ BITS = 2
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Filter step."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = EXPOSURE_CODE
+ START_BIT = 12
+ BITS = 5
+ DATA_TYPE = UNSIGNED_INTEGER
+ DESCRIPTION = "Exposure interval code."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS50_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 121
+ BYTES = 2
+ DESCRIPTION = "Plus 50 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS15_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 123
+ BYTES = 2
+ DESCRIPTION = "Plus 15 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS12_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 125
+ BYTES = 2
+ DESCRIPTION = "Plus 12 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_PLUS5_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 127
+ BYTES = 2
+ DESCRIPTION = "Plus 5 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_MINUS15_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 129
+ BYTES = 2
+ DESCRIPTION = "Minus 15 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_MINUS23_VDC
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 131
+ BYTES = 2
+ DESCRIPTION = "Minus 23 volts dc."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = VIS_AVERAGE_VIDEO
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 133
+ BYTES = 2
+ DESCRIPTION = "Average video."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = POWER_CONVERTER_INPUT_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 135
+ BYTES = 2
+ DESCRIPTION = "Power converter input current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = CATHODE_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 137
+ BYTES = 2
+ DESCRIPTION = "Cathode current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = CATHODE_VOLTAGE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 139
+ BYTES = 2
+ DESCRIPTION = "Cathode voltage."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FILAMENT_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 141
+ BYTES = 2
+ DESCRIPTION = "Filament current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FRAME_SWEEP_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 143
+ BYTES = 2
+ DESCRIPTION = "Frame sweep current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_SWEEP_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 145
+ BYTES = 2
+ DESCRIPTION = "Line sweep current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = GRID3_VOLTAGE
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 147
+ BYTES = 2
+ DESCRIPTION = "Grid 3 voltage."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FOCUS_CURRENT
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 149
+ BYTES = 2
+ DESCRIPTION = "Focus current."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DIGITAL_LADDER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 151
+ BYTES = 2
+ DESCRIPTION = "Digital ladder."
+ END_OBJECT = COLUMN
+
+END_OBJECT = ENGINEERING_TABLE_STRUCTURE
+
+END
+END_OBJECT
+OBJECT = LINE_HEADER_TABLE
+ ROWS = 1056
+ ROW_BYTES = 62
+CCSD3ZF0000100000001NJPL3IF0PDS200000001 = SFDU_LABEL
+
+OBJECT = LINE_HEADER_TABLE_STRUCTURE
+ INTERCHANGE_FORMAT = BINARY
+ BYTES = 62
+ NOTE = "Viking Orbiter Image Line-header
+ Structure. This label describes the structure of the 62-bytes
+ extracted from the end of each image line."
+
+ OBJECT = COLUMN
+ NAME = FDS_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 1
+ BYTES = 4
+ DESCRIPTION = "Flight Data Subsystem (FDS) clock
+ count."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_NUMBER
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 5
+ BYTES = 2
+ DESCRIPTION = "Flight Data Subsystem line number,
+ extracted from the telemetry record header information."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FILL_IN
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 7
+ BYTES = 1
+ DESCRIPTION = "Value used to fill in missing samples
+ (always zero)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = TRACK_PRESENCE_MASK
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 8
+ BYTES = 1
+ DESCRIPTION = "Mask indicating which tracks are
+ present in this line. The nominal value is HEX 7F, indicating
+ that all seven tracks are present."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = AVERAGE_PIXEL
+ DATA_TYPE = UNSIGNED_INTEGER
+ START_BYTE = 9
+ BYTES = 2
+ DESCRIPTION = "Average pixel value for this line."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 11
+ BYTES = 2
+ DESCRIPTION = "Total number of line segments in the
+ line that contain some valid data (maximum is 7)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = FULLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 13
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ that were fully synchronized (maximum is 7)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = PARTLY_SYNCHED_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 15
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ that were partly synchronized (maximum is 7)."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI0_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 17
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 0 (maximum is 7), indicating
+ bad data."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI1_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 19
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 1 (maximum is 7), indicating
+ SNR low, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI2_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 21
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 2 (maximum is 7), indicating
+ SNR good, GCF block bad."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI3_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 23
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 3 (maximum is 7), indicating
+ SNR low, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI4_SEGMENTS
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 25
+ BYTES = 2
+ DESCRIPTION = "Total number of segments in the line
+ with a data quality indicator of 4 (maximum is 7), indicating
+ SNR good, GCF block good."
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 27
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK1
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 29
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT2
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 31
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK2
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 33
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT3
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 35
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK3
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 37
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT4
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 39
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK4
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 41
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT5
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 43
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK5
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 45
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT6
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 47
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK6
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 49
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = DQI_RATE_ORBIT7
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 51
+ BYTES = 2
+ DESCRIPTION = "Bit string containing data quality
+ indicator, telemetry rate code and orbit number."
+
+ OBJECT = BIT_COLUMN
+ NAME = DQI
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 3
+ DESCRIPTION = "Data quality indicator for this line
+ segment, where: 0 is bad data; 1 is SNR low, GCF block error; 2
+ is SNR good, GCF block bad; 3 is SNR low, GCF block good; 4 is
+ SNR good, GCF block good."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TELEMETRY_RATE_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 4
+ BITS = 3
+ DESCRIPTION = "Telemetry rate code, where: 1 for
+ 16K; 2 for 8K; 3 for 4K; 4 for 2K; 5 for 1K."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = ORBIT_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 7
+ BITS = 10
+ DESCRIPTION = "Orbit number taken from expected
+ picture list. For Viking Orbiter 1 Survey mission images this
+ is ORBIT_NUMBER - 1000."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = LINE_TRACK7
+ DATA_TYPE = VAX_INTEGER
+ START_BYTE = 53
+ BYTES = 2
+ DESCRIPTION = "Bit string containing track and line
+ number."
+
+ OBJECT = BIT_COLUMN
+ NAME = PLAYBACK_REVERSED_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 1
+ BITS = 1
+ DESCRIPTION = "Set to 1 if playback is in reverse
+ order for this segment. Track 1, 3, 5 and 7 are played-back
+ forward, 2, 4 and 6 are played-back reversed."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = DATA_ABSENCE_FLAG
+ DATA_TYPE = INTEGER
+ START_BIT = 2
+ BITS = 1
+ DESCRIPTION = "Set to 1 if data is not present for
+ this segment."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = TRACK_CODE
+ DATA_TYPE = INTEGER
+ START_BIT = 3
+ BITS = 3
+ DESCRIPTION = "Track code, where: 0 is Track 7; 1 is
+ Track 3; 2 is Track 2; 3 is error; 4 is Track 6; 5 is Track 1; 6
+ is Track 5; 7 is Track 4."
+ END_OBJECT = BIT_COLUMN
+
+ OBJECT = BIT_COLUMN
+ NAME = SEGMENT_LINE_NUMBER
+ DATA_TYPE = INTEGER
+ START_BIT = 6
+ BITS = 11
+ DESCRIPTION = "Line number extracted from segment
+ header."
+ END_OBJECT = BIT_COLUMN
+
+ END_OBJECT = COLUMN
+
+ OBJECT = COLUMN
+ NAME = EMBEDDED_SCIENCE_DATA
+ ITEMS = 7
+ DATA_TYPE = INTEGER
+ START_BYTE = 55
+ ITEM_BYTES = 1
+ DESCRIPTION = "Embedded low rate science data from
+ seven segments."
+ END_OBJECT = COLUMN
+
+END_OBJECT = LINE_HEADER_TABLE_STRUCTURE
+
+END
+END_OBJECT
+OBJECT = IMAGE
+ ENCODING_TYPE = HUFFMAN_FIRST_DIFFERENCE
+ LINES = 1056
+ LINE_SAMPLES = 1204
+ SAMPLE_TYPE = UNSIGNED_INTEGER
+ SAMPLE_BITS = 8
+ SAMPLE_BIT_MASK = 2#11111110#
+ CHECKSUM = 44303556
+END_OBJECT
+END
diff --git a/tests/pytests/data/f735a00/naif0012.tls b/tests/pytests/data/f735a00/naif0012.tls
new file mode 100644
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/f735a00/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/f735a00/pck00009.tpc b/tests/pytests/data/f735a00/pck00009.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..bfadaab2b26817327189ff3173e9609f49dedc9d
--- /dev/null
+++ b/tests/pytests/data/f735a00/pck00009.tpc
@@ -0,0 +1,3639 @@
+KPL/PCK
+
+
+P_constants (PcK) SPICE kernel file
+===========================================================================
+
+ By: Nat Bachman (NAIF) 2010 March 3
+
+
+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/IAG
+ 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
+
+
+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 and planets.
+ Additional items included in this section:
+
+ - Earth north geomagnetic centered dipole values
+ for epochs 1945-2000
+
+ - Mars prime meridian offset "lambda_a"
+
+ -- Orientation constants for satellites
+
+ -- Orientation constants for asteroids Eros, Gaspra, Ida,
+ Itokawa, and Vesta
+
+ -- Orientation constants for comets 19P/Borrelly
+ and 9P/Tempel 1
+
+
+ Radii of Bodies
+ ---------------
+
+ -- Radii of Sun and planets
+
+ -- Radii of satellites, where available
+
+ -- Radii of asteroids Ceres, Eros, Gaspra, Ida, Itokawa,
+ Mathilde, Toutatis, and Vesta.
+
+ -- Radii of comets 19P/Borrelly, Halley, 9P/Tempel 1,
+ and 81P/Wild 2
+
+
+
+Version Description
+--------------------------------------------------------
+
+ This file was created on March 3, 2010. This version
+ incorporates data from reference [1].
+
+ This file contains size, shape, and orientation data for all
+ objects described by the previous version of the file, except
+ for Kleopatra: a shape model for this body is not provided in [1]
+ because, according to this source, it had been "modeled from
+ low resolution radar data, and cannot be mapped from those
+ data."
+
+ New objects covered by this file but not the previous
+ version are:
+
+ 19P/Borrelly
+ Halley
+ 9P/Tempel 1
+ 81P/Wild 2
+ Ceres
+ Itokawa
+ Mathilde
+ Toutatis
+
+
+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, and version description section if you modify
+ this file.
+
+Known Limitations and Caveats
+
+ Accuracy
+ --------
+
+ In general, the orientation models given here are claimed by the
+ IAU/IAG 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]) 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. 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 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. A more
+ accurate approximation can be obtained by using both the NAIF
+ lunar frame kernel and the binary lunar orientation PCK file,
+ which 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
+ J2000 epoch 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].
+
+
+ Mars prime meridian offset
+ --------------------------
+
+ The Mars prime meridian offset given by [5] is not used by
+ SPICE geometry software for computations involving the shape
+ of Mars (for example, in sub-observer point or surface intercept
+ computations). The value 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 only planets for which such terms are used are
+ Jupiter and Neptune. Use of trigonometric polynomial terms for
+ natural satellites is and has been supported for all SPICE Toolkit
+ versions.
+
+ 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
+--------------------------------------------------------
+
+ The sources for the constants listed in this file are:
+
+
+ [1] 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."
+
+ [2] Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F.,
+ Cruikshank, D.P., Hilton, J.L., Keller, H.U., Oberst, J.,
+ Simon, J.L., Stooke, P., Tholen, D.J., and Thomas, P.C.
+ "Report of the IAU/IAG Working Group on Cartographic
+ Coordinates and Rotational Elements of the Planets and
+ Satellites: 2003."
+
+ [3] 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.
+
+ [4] Nautical Almanac Office, United States Naval Observatory,
+ H.M. Nautical Almanac Office, Royal Greenwich
+ Observatory, Jet Propulsion Laboratory, Bureau des
+ Longitudes, and The Time Service and Astronomy
+ Departments, United States Naval Observatory (1992).
+ "Explanatory Supplement to the Astronomical Almanac," P.
+ Kenneth Seidelmann, ed. University Science Books, 20
+ Edgehill Road, Mill Valley, CA 9494.
+
+ [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.
+
+
+ Most values are from [1]. All exceptions are
+ commented where they occur in this file. The exceptions are:
+
+
+ -- Radii for the Sun are from [3].
+
+ -- 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
+ [8]. The article [6] was used to check most of
+ these values, and the values were also re-computed from
+ the 9th generation IGRF [9] by Nat Bachman.
+
+ -- The Mars prime meridian offset angle is from [5].
+
+
+ "Old values" listed are from the SPICE P_constants file
+ pck00008.tpc dated September 21, 2004. Most of these values came
+ from the 2003 IAU report [2].
+
+
+
+
+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 = ( 6378.14 6378.14 6356.75 )
+
+ Any blanks preceding or following keyword names, values and equal
+ signs are ignored.
+
+ Assignments may be spread over multiple lines, for example:
+
+ BODY399_RADII = ( 6378.14
+ 6378.14
+ 6356.75 )
+
+ 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 2006 IAU/IAG 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 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 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, 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: 2006 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 = ( 284.95 870.5366420 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 term is zero for all bodies except Mars. It represents the
+ angular offset between the meridian containing the longest axis of
+ the triaxial ellipsoid used to model a body's surface and the
+ prime meridian of the body.
+
+ 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 2006 IAU report does
+ not use any other models, except in the case of Mars, where
+ separate values are given for the north and south polar radii.
+
+ 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 = ( 6378.14 6378.14 6356.75 )
+
+
+Body Numbers 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
+
+
+ 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
+ 2000004 Asteroid Vesta
+ 2000216 Asteroid Kleopatra
+ 2000253 Asteroid Mathilde
+ 2000433 Asteroid Eros
+ 2004179 Asteroid Toutatis
+ 2025143 Asteroid Itokawa
+ 2431010 Asteroid Ida
+ 9511010 Asteroid Gaspra
+
+
+Orientation Constants for the Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+
+ 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. )
+
+ 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 unchanged in the 2006 IAU report.
+
+
+ Current values:
+
+ \begindata
+
+ BODY199_POLE_RA = ( 281.01 -0.033 0. )
+ BODY199_POLE_DEC = ( 61.45 -0.005 0. )
+ BODY199_PM = ( 329.548 6.1385025 0. )
+
+ BODY199_LONG_AXIS = ( 0. )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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:
+
+ Old 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 )
+
+
+ Current values:
+
+ 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
+
+
+ Values are given for the epoch 2000 and are from the final row
+ of the above table, which is from [8]. As shown by the table
+ these values constitute a low-accuracy approximation for epochs
+ not close to 2000.
+
+ \begindata
+
+ BODY399_N_GEOMAG_CTR_DIPOLE_LON = ( 288.43 )
+ BODY399_N_GEOMAG_CTR_DIPOLE_LAT = ( 79.54 )
+
+ \begintext
+
+
+Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 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:
+
+ Values are from the 2003 IAU report.
+
+
+ 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 )
+
+
+
+ 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 = ( 284.95 870.5366420 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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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 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.
+
+
+ \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
+ 29.80 -52.1
+ 706.64 151413.4
+ 57.44 151413.4 )
+ \begintext
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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
+
+
+
+Pluto
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ BODY999_POLE_RA = ( 313.02 0. 0. )
+ BODY999_POLE_DEC = ( 9.09 0. 0. )
+ BODY999_PM = ( 236.77 -56.3623195 0. )
+ BODY999_LONG_AXIS = ( 0. )
+
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+
+Orientation constants for the satellites
+--------------------------------------------------------
+
+
+Satellites of Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 from the 2003 IAU report.
+
+
+ body502_pole_ra = ( 268.08 -0.009 0. )
+ body502_pole_dec = ( 64.51 0.003 0. )
+ body502_pm = ( 35.67 101.3747235 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 )
+
+
+ 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+ Enceladus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Tethys
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+ Dione
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Rhea
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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. 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
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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 )
+
+ \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 unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+ Phoebe
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body609_pole_ra = ( 355.00 0. 0. )
+ body609_pole_dec = ( 68.70 0. 0. )
+ body609_pm = ( 304.70 930.8338720 0. )
+ body609_long_axis = ( 0. )
+
+ 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 2006 IAU report.
+
+ Current values:
+
+ \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. 0.023 )
+ BODY610_NUT_PREC_DEC = ( 0. -0.183 0. 0. 0. 0. 0. 0. 0.001 )
+ BODY610_NUT_PREC_PM = ( 0. 1.613 0. 0. 0. 0. 0. 0. -0.023 )
+
+ \begintext
+
+
+
+ Epimetheus
+
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \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. 0.086 0. )
+ BODY611_NUT_PREC_DEC = ( -0.356 0. 0. 0. 0. 0. 0. 0.005 0. )
+ BODY611_NUT_PREC_PM = ( 3.133 0. 0. 0. 0. 0. 0. -0.086 0. )
+
+ \begintext
+
+
+
+ Helene
+
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2006 report [1] states that values for Nereid are not
+ given because Nereid is not in synchronous rotation with Neptune
+ (p. 167).
+
+
+
+ Naiad
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 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 2006 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 2006 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 2006 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 2006 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 2003 IAU report.
+
+ body901_pole_ra = ( 313.02 0. 0. )
+ body901_pole_dec = ( 9.09 0. 0. )
+ body901_pm = ( 56.77 -56.3623195 0. )
+ body901_long_axis = ( 0. )
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+
+
+Orientation constants for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+19P/Borrelly
+
+
+ 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
+
+
+
+9P/Tempel 1
+
+
+ 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
+
+
+Vesta
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY2000004_POLE_RA = ( 301. 0. 0. )
+ BODY2000004_POLE_DEC = ( 41. 0. 0. )
+ BODY2000004_PM = ( 292. 1617.332776 0. )
+ BODY2000004_LONG_AXIS = ( 0. )
+
+ \begintext
+
+Eros
+
+ Old values:
+
+ Values are unchanged in the 2006 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
+
+
+Itokawa
+
+
+ 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
+
+
+
+Ida
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ 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. )
+
+ \begintext
+
+Gaspra
+
+ Old values:
+
+ Values are unchanged in the 2006 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
+
+
+
+
+
+
+
+
+
+
+Radii of Sun and Planets
+--------------------------------------------------------
+
+
+Sun
+
+ Value for the Sun is from the [3], page K7.
+
+ \begindata
+
+ BODY10_RADII = ( 696000. 696000. 696000. )
+
+ \begintext
+
+
+Mercury
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY199_RADII = ( 2439.7 2439.7 2439.7 )
+
+ \begintext
+
+
+Venus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY299_RADII = ( 6051.8 6051.8 6051.8 )
+
+ \begintext
+
+
+Earth
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+
+ \begindata
+
+ BODY399_RADII = ( 6378.14 6378.14 6356.75 )
+
+ \begintext
+
+
+Mars
+
+
+ Old values:
+
+ body499_radii = ( 3397. 3397. 3375. )
+
+ Current values:
+
+
+ The IAU report gives separate values for the north and south
+ polar radii:
+
+ north: 3373.19
+ south: 3379.21
+
+ We use the average of these values 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 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY599_RADII = ( 71492 71492 66854 )
+
+ \begintext
+
+
+
+Saturn
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY699_RADII = ( 60268 60268 54364 )
+
+ \begintext
+
+
+
+Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY799_RADII = ( 25559 25559 24973 )
+
+ \begintext
+
+
+
+Neptune
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ (Values are for the 1 bar pressure level.)
+
+ \begindata
+
+ BODY899_RADII = ( 24764 24764 24341 )
+
+ \begintext
+
+
+
+Pluto
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY999_RADII = ( 1195 1195 1195 )
+
+ \begintext
+
+
+
+
+Radii of Satellites
+--------------------------------------------------------
+
+
+Moon
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY301_RADII = ( 1737.4 1737.4 1737.4 )
+
+ \begintext
+
+
+
+Satellites of Mars
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY401_RADII = ( 13.4 11.2 9.2 )
+ BODY402_RADII = ( 7.5 6.1 5.2 )
+
+ \begintext
+
+
+
+Satellites of Jupiter
+
+ Old values:
+
+ Values are unchanged in the 2006 IAU report.
+
+ Current values:
+
+ \begindata
+
+ BODY501_RADII = ( 1829.4 1819.3 1815.7 )
+ BODY502_RADII = ( 1564.13 1561.23 1560.93 )
+ BODY503_RADII = ( 2632.4 2632.29 2632.35 )
+ BODY504_RADII = ( 2409.4 2409.2 2409.3 )
+ 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 )
+
+ \begintext
+
+ 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.
+ \begindata
+
+ BODY516_RADII = ( 21.5 21.5 21.5 )
+
+ \begintext
+
+
+
+Satellites of Saturn
+
+
+ Old values:
+
+ Values are from the 2003 IAU report.
+
+ body601_radii = ( 209.1 196.2 191.4 )
+ body602_radii = ( 256.3 247.3 244.6 )
+ body603_radii = ( 535.6 528.2 525.8 )
+ body604_radii = ( 560 560 560 )
+ body605_radii = ( 764 764 764 )
+ body606_radii = ( 2575 2575 2575 )
+ body607_radii = ( 164 130 107 )
+ body608_radii = ( 718 718 718 )
+ body609_radii = ( 115 110 105 )
+ 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) was given in the
+ 2003 IAU report:
+
+ body612_radii = ( 17.5 --- --- )
+
+ The mean radius was 16km; we used this radius for all three axes, as
+ we do for the satellites for which only the mean radius is available.
+
+
+ body612_radii = ( 16 16 16 )
+ 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 )
+
+
+
+ Current values:
+
+ \begindata
+
+ 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 )
+
+ \begintext
+
+ 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.
+
+
+ \begindata
+
+ 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 )
+
+ \begintext
+
+
+ For Pan, only a mean radius is given in the 2006 report.
+
+ \begindata
+
+ BODY618_RADII = ( 10 10 10 )
+
+ \begintext
+
+
+
+Satellites of Uranus
+
+ Old values:
+
+ Values are unchanged in the 2006 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 2006 IAU report.
+
+ Current values:
+
+ The 2000 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 2000
+ 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 from the 2003 IAU report.
+
+ BODY901_RADII = ( 593 593 593 )
+
+ Current values:
+
+ \begindata
+
+ BODY901_RADII = ( 605 605 605 )
+
+ \begintext
+
+
+
+Radii for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+19P/Borrelly
+
+
+ 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
+
+
+
+Halley
+
+
+ Current values:
+
+ \begindata
+
+ BODY1000036_RADII = ( 8.0 4.0 4.0 )
+
+ \begintext
+
+
+
+9P/Tempel 1
+
+
+ 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
+
+
+81P/Wild 2
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY1000107_RADII = ( 2.7 1.9 1.5 )
+
+ \begintext
+
+
+Ceres
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000001_RADII = ( 487.3 487.3 454.7 )
+
+ \begintext
+
+
+Vesta
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000004_RADII = ( 289. 280. 229. )
+
+ \begintext
+
+
+Toutatis
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2004179_RADII = ( 2.13 1.015 0.85 )
+
+ \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 2006 report.
+
+
+Mathilde
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000253_RADII = ( 33. 24. 23. )
+
+ \begintext
+
+Eros
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2000433_RADII = ( 17.0 5.5 5.5 )
+
+ \begintext
+
+
+Itokawa
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2025143_RADII = ( 0.535 0.294 0.209 )
+
+ \begintext
+
+
+
+Gaspra
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY9511010_RADII = ( 9.1 5.2 4.4 )
+
+ \begintext
+
+
+
+
+Ida
+
+
+ Current values:
+
+
+ \begindata
+
+ BODY2431010_RADII = ( 26.8 12.0 7.6 )
+
+ \begintext
+
+
+
+===========================================================================
+End of file pck00009.tpc
+===========================================================================
+
+
+
diff --git a/tests/pytests/data/f735a00/vikingAddendum003.ti b/tests/pytests/data/f735a00/vikingAddendum003.ti
new file mode 100644
index 0000000000000000000000000000000000000000..98d77dabf0b8c75725cc56d8e0d7e8f530da5fa2
--- /dev/null
+++ b/tests/pytests/data/f735a00/vikingAddendum003.ti
@@ -0,0 +1,23 @@
+\begindata
+INS-27001_TRANSX = ( 0.0, 0.0117647058823529, 0.0)
+INS-27001_TRANSY = ( 0.0, 0.0, 0.0117647058823529)
+INS-27001_ITRANSS = ( 0.0, 85.0, 0.0)
+INS-27001_ITRANSL = ( 0.0, 0.0, 85.0)
+
+INS-27002_TRANSX = ( 0.0, 0.0117647058823529, 0.0)
+INS-27002_TRANSY = ( 0.0, 0.0, 0.0117647058823529)
+INS-27002_ITRANSS = ( 0.0, 85.0, 0.0)
+INS-27002_ITRANSL = ( 0.0, 0.0, 85.0)
+
+\begintext
+These are the parameters for writing c-kernels. Isis will create ck
+with the same frame endpoints as the mission ck. For Viking1 the ck
+instrument frame is VO1_PLATFORM (-27000) and the ck reference frame
+is B1950 (2) or J2000 (1), depending on the ck used. The mdim2.0_rand
+ck is in J2000.
+
+\begindata
+INS-27001_CK_FRAME_ID=-27000
+INS-27001_CK_REFERENCE_ID=2
+INS-27002_CK_FRAME_ID=-27000
+INS-27002_CK_REFERENCE_ID=2
diff --git a/tests/pytests/data/f735a00/vo1_fict.tsc b/tests/pytests/data/f735a00/vo1_fict.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..ca6eab8889dbe1ae002356ae175ce3da73dc318f
--- /dev/null
+++ b/tests/pytests/data/f735a00/vo1_fict.tsc
@@ -0,0 +1,136 @@
+KPL/SCLK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "VO1_FICT.TSC"
+MISSION_NAME = VIKING
+SPACECRAFT_NAME = "VIKING ORBITER 1"
+DATA_SET_ID = "VO1/VO2-M-SPICE-6-V1.0"
+KERNEL_TYPE_ID = SCLK
+PRODUCT_ID = "VO1_FICT.TSC"
+PRODUCT_CREATION_TIME = 2000-04-21T10:53:20
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = {
+ PRIMARY_MISSION,
+ EXTENDED_MISSION,
+ CONTINUATION_MISSION,
+ SURVEY_MISSION
+ }
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = MARS
+INSTRUMENT_NAME = "N/A"
+NAIF_INSTRUMENT_ID = "N/A"
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = CLOCK_COEFFICIENTS
+ DESCRIPTION = "SCLK file implementing fictitious clock
+used to tag orientation data in the VO1 CK files. This SCLK file does NOT
+represent real Viking Orbiter 1 on-board clock but rather is a simple
+counter of milliseconds since 1 Jan 1976 00:00:00. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+Viking Orbiter 1 "fictitious" SCLK Kernel
+--------------------------------------------------------
+
+ This file contains the data necessary to convert between the
+ 'fictitious' Viking Orbiter 1 on-board clock times used as tags
+ for pointing instances in Viking Orbiter 1 CK files and ephemeris
+ time.
+
+ NAIF suggests that you do not modify this file. If you do modify
+ it, be sure to indicate this in the `Version' section below.
+
+
+Version
+--------------------------------------------------------
+
+ Version 1.0.1 -- April 20, 2000
+
+ Comments in the file were slightly reformatted and augmented.
+
+ Version 1.0.0 -- July 22, 1996
+
+
+Implementation notes
+--------------------------------------------------------
+
+ This SPICE SCLK file is constructed so that valid SCLK strings
+ are simply the number of seconds that have passed since the UTC
+ epoch 1 Jan 1976 00:00:00. Thus 288929292.827 simply represents
+ the epoch that occurs 288929292.827 seconds past the UTC epoch
+ 1 Jan 1976.
+
+ For all time, the clock runs at the same rate as Terrestrial
+ Dynamical Time (TDT). There is only one partition for this clock.
+
+ You must load this file into the kernel pool before using any
+ of the SPICELIB SCLK routines. The code fragment
+
+ CALL LDPOOL ( < name of this file > )
+
+ performs this task. To convert between ET and UTC, you will
+ also need to load a leapseconds kernel. The additional call
+ to LDPOOL,
+
+ CALL LDPOOL ( < name of your leapsecond file > )
+
+ will accomplish this. Note that you must supply the actual names
+ of the files used on your system as arguments to LDPOOL. Because
+ the file names are system dependent, we do not list them here.
+
+ For more information, consult your SPICELIB required reading
+ files. The following areas are covered:
+
+ SCLK system SCLK required reading
+ Time systems and conversion TIME required reading
+ Kernel pool KERNEL required reading
+
+
+Kernel data
+--------------------------------------------------------
+
+ \begindata
+
+ SCLK_KERNEL_ID = ( @22-JUL-1996 )
+
+ SCLK_DATA_TYPE_27 = ( 1 )
+
+ SCLK01_TIME_SYSTEM_27 = ( 2 )
+ SCLK01_N_FIELDS_27 = ( 2 )
+ SCLK01_MODULI_27 = ( 10000000000 1000 )
+ SCLK01_OFFSETS_27 = ( 0 0 )
+ SCLK01_OUTPUT_DELIM_27 = ( 1 )
+
+ SCLK_PARTITION_START_27 = ( 0.0000000000000E+00 )
+ SCLK_PARTITION_END_27 = ( 1.00000000E+14 )
+ SCLK01_COEFFICIENTS_27 = ( 0.00000000E+00
+ @01-JAN-1976-00:00:47.184
+ 1 )
+
+ \begintext
+
+
+Contact Information
+--------------------------------------------------------
+
+ Contact NAIF node of the Planetary Data System if you have any
+ questions regarding this SCLK file.
+
+ Charles H. Acton, Jr
+ (818)-354-3869
+ chuck.acton@jpl.nasa.gov
+
+ Boris V. Semenov
+ (818)-354-8136
+ boris.semenov@jpl.nasa.gov
diff --git a/tests/pytests/data/f735a00/vo1_fsc.tsc b/tests/pytests/data/f735a00/vo1_fsc.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..aa5d9a7c0ea464b9eb1da461c207a2de2c1927e2
--- /dev/null
+++ b/tests/pytests/data/f735a00/vo1_fsc.tsc
@@ -0,0 +1,237 @@
+KPL/SCLK
+
+\beginlabel
+PDS_VERSION_ID = PDS3
+RECORD_TYPE = STREAM
+RECORD_BYTES = "N/A"
+^SPICE_KERNEL = "VO1_FSC.TSC"
+MISSION_NAME = VIKING
+SPACECRAFT_NAME = "VIKING ORBITER 1"
+DATA_SET_ID = "VO1/VO2-M-SPICE-6-V1.0"
+KERNEL_TYPE_ID = SCLK
+PRODUCT_ID = "VO1_FSC.TSC"
+PRODUCT_CREATION_TIME = 2000-04-21T10:53:21
+PRODUCER_ID = "NAIF/JPL"
+MISSION_PHASE_NAME = {
+ PRIMARY_MISSION,
+ EXTENDED_MISSION,
+ CONTINUATION_MISSION,
+ SURVEY_MISSION
+ }
+PRODUCT_VERSION_TYPE = ACTUAL
+PLATFORM_OR_MOUNTING_NAME = "N/A"
+START_TIME = "N/A"
+STOP_TIME = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT = "N/A"
+TARGET_NAME = MARS
+INSTRUMENT_NAME = "N/A"
+NAIF_INSTRUMENT_ID = "N/A"
+SOURCE_PRODUCT_ID = "N/A"
+NOTE = "See comments in the file for details"
+OBJECT = SPICE_KERNEL
+ INTERCHANGE_FORMAT = ASCII
+ KERNEL_TYPE = CLOCK_COEFFICIENTS
+ DESCRIPTION = "SCLK file containing linear piecewise
+function representing VO1 FSC on-board clock. This function was generated as
+the result of VO1 image time tags restoration. "
+END_OBJECT = SPICE_KERNEL
+\endlabel
+
+
+Viking Orbiter 1 Reconstructed Frame Start Count (FSC) SCLK file
+--------------------------------------------------------
+
+ This file contain data necessary to convert a Viking Orbiter 1
+ FSC count to the ET time corresponding to it. These data are
+ based on the results of VO1 image times reconstruction done at
+ NAIF/JPL. The process of this reconstruction is described in
+ detail in the "VO Image Time Reconstruction" document.
+
+ Note that the main purpose of this file is to store the
+ reconstructed FSC counter; the on-board clock defined by the
+ function in this file was not used to time tag any of the
+ orientation data in CK files.
+
+ To avoid confusion with the other VO1 clock used for time tagging,
+ the FSC on-board clock in this file was assigned the NAIF ID
+ code -27999.
+
+
+Version
+--------------------------------------------------------
+
+ Version 1.0.1 -- April 20, 2000
+
+ Comments in the file were slightly reformatted and augmented.
+
+ Version 1.0.0 -- July 22, 1996
+
+
+Implementation notes
+--------------------------------------------------------
+
+ This SPICE SCLK file is constructed so that valid SCLK strings
+ are the eight digit VO1 FSC count associated with each VO1 image.
+ Note that the actual "image time" (the time of the beginning,
+ middle or the end of exposure) has a significant offset from
+ the FSC tick start time. This offset depends on the exposure
+ duration and is described in the "VO Image Time Reconstruction"
+ document.
+
+ You must load this file into the kernel pool before using any
+ of the SPICELIB SCLK routines. The code fragment
+
+ CALL LDPOOL ( < name of this file > )
+
+ performs this task. To convert between ET and UTC, you will also
+ need to load a leapseconds kernel. The additional call to LDPOOL,
+
+ CALL LDPOOL ( < name of your leapsecond file > )
+
+ will accomplish this. Note that you must supply the actual names
+ of the files used on your system as arguments to LDPOOL. Because
+ the file names are system dependent, we do not list them here.
+
+ For more information, consult your SPICELIB required reading
+ files. The following areas are covered:
+
+ SCLK system SCLK required reading
+ Time systems and conversion TIME required reading
+ Kernel pool KERNEL required reading
+
+
+Kernel data
+--------------------------------------------------------
+
+\begindata
+
+ SCLK_KERNEL_ID = ( @22-JUL-1996 )
+
+ SCLK_DATA_TYPE_27999 = ( 1 )
+ SCLK01_TIME_SYSTEM_27999 = ( 2 )
+ SCLK01_N_FIELDS_27999 = ( 1 )
+ SCLK01_MODULI_27999 = ( 60000000 )
+ SCLK01_OFFSETS_27999 = ( 25837050 )
+ SCLK01_OUTPUT_DELIM_27999 = ( 1 )
+
+ SCLK_PARTITION_START_27999 = (
+ 0
+ 231791
+ 644942
+ 1569121
+ 3367553
+ 5555717
+ 6396566
+ 7572950
+ 8087730
+ 9835672
+ 10866610
+ 11503583
+ 12217716
+ 13159619
+ 13679685
+ 14664700
+ 15449939
+ 16432925
+ 17479492
+ 17896518
+ 18344818
+ 20321730
+ 23280832
+ 24166658
+ 24262845
+ 24359029
+ 24609280
+ 25992950
+ 26522392
+ 27368930
+ 27915783
+ )
+
+ SCLK_PARTITION_END_27999 = (
+ 231791
+ 644942
+ 1569121
+ 3367553
+ 5555717
+ 6396566
+ 7572950
+ 8087730
+ 9835672
+ 10866610
+ 11503583
+ 12217716
+ 13159619
+ 13679685
+ 14664700
+ 15449939
+ 16432925
+ 17479492
+ 17896518
+ 18344818
+ 20321730
+ 23280832
+ 24166658
+ 24262845
+ 24359029
+ 24609280
+ 25992950
+ 26522392
+ 27368930
+ 27915783
+ 59999999
+ )
+
+ SCLK01_COEFFICIENTS_27999 = (
+
+ 0 -742936101.084011 4.480002320
+ 231791 -741897676.845143 4.480001506
+ 644942 -740046759.578601 4.480001685
+ 1569121 -735906436.111559 4.480001416
+ 3367553 -727849458.210550 4.480001972
+ 5555717 -718046479.059529 4.480002284
+ 6396566 -714279473.752967 4.480001816
+ 7572950 -709009271.245943 4.480001816
+ 8087730 -706703055.797485 4.480001869
+ 9835672 -698872272.708142 4.480001557
+ 10866610 -694253669.451953 4.480001151
+ 11503583 -691400029.539901 4.480000884
+ 12217716 -688200712.915836 4.480000934
+ 13159619 -683980986.490315 4.480000934
+ 13679685 -681651090.175512 4.480000934
+ 14664700 -677238222.129167 4.480000778
+ 15449939 -673720350.640383 4.480000830
+ 16432925 -669316572.195161 4.480000882
+ 17479492 -664627950.891482 4.480000922
+ 17896518 -662759673.743136 4.480000929
+ 18344818 -660751289.419364 4.480000581
+ 20321730 -651894716.843243 4.480001297
+ 23280832 -638637935.825957 4.480001191
+ 24166658 -634669434.296886 4.480000989
+ 24262845 -634238516.448398 4.480001715
+ 24359029 -633807611.943517 4.480001275
+ 24609280 -632686487.136533 4.480001142
+ 25992950 -626487643.963656 4.480001192
+ 26522392 -624115743.164982 4.480000986
+ 27368930 -620323251.820923 4.480001408
+ 27915783 -617873349.601991 4.480001089
+
+ )
+
+\begintext
+
+
+Contact Information
+--------------------------------------------------------
+
+ Contact NAIF node of the Planetary Data System if you have any
+ questions regarding this SCLK file.
+
+ Charles H. Acton, Jr
+ (818)-354-3869
+ chuck.acton@jpl.nasa.gov
+
+ Boris V. Semenov
+ (818)-354-8136
+ boris.semenov@jpl.nasa.gov
diff --git a/tests/pytests/data/f735a00/vo1_sedr_ck2_0_sliced_-27000.xc b/tests/pytests/data/f735a00/vo1_sedr_ck2_0_sliced_-27000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..f535e7d21e931f8b722e255545ce6e75a103d3de
--- /dev/null
+++ b/tests/pytests/data/f735a00/vo1_sedr_ck2_0_sliced_-27000.xc
@@ -0,0 +1,101 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+'VO1 PLATFORM ATTITUDE; CREATED BY BVS/NAIF; 2006-FEB-09 '
+BEGIN_ARRAY 1 80
+'VO1 ATT. BASED ON GEM AND SEDR FILES '
+'122DF066CC^A'
+'122E1B6615^A'
+'-6978'
+'2'
+'2'
+'1'
+80
+'60BAE2FF9377E4^-1'
+'-7297AF3F99C068^-1'
+'9A26C09802033^0'
+'CC2B9860BF7C4^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'723F9FE60E38F^-1'
+'-8E5BA3434CB3F8^-1'
+'9ADE330545D3F8^0'
+'CB85FBA8AFD88^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'59FF5C2BD5AF64^-1'
+'-74D68FC13A594C^-1'
+'9C38243F49C918^0'
+'CA997A2B9A801^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'6DA317049D4BD4^-1'
+'-958CAA3AE81058^-1'
+'9D8E8E3B7A0898^0'
+'C9704999CD23A^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'55AFAEB074CF6C^-1'
+'-7CC6C97CB2A1EC^-1'
+'9EE327F5ECD82^0'
+'C880AECAFC645^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'6A086A75B4E6A8^-1'
+'-98B71F7ED22CE^-1'
+'A0133940960F78^0'
+'C7710BA98B8078^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'51DC30B3206E44^-1'
+'-7D73B8FC526EA4^-1'
+'A174F3CE64BEB^0'
+'C671AC0CF2E9D8^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'65DC3F1AF382F^-1'
+'-9945A0B47BF2^-1'
+'A2BABA2E6EF008^0'
+'C549EA8DCCED18^0'
+'0^0'
+'0^0'
+'0^0'
+'4189374BC6A7F^-2'
+'122E0BB4E10002^A'
+'122E0BC6720001^A'
+'122E0BD7E0FFFD^A'
+'122E0BE972FFFF^A'
+'122E0BFAE0FFFF^A'
+'122E0C0C730001^A'
+'122E0C1DD90001^A'
+'122E0C2F610003^A'
+'122E0BBCB10002^A'
+'122E0BCE420001^A'
+'122E0BDFB0FFFD^A'
+'122E0BF142FFFF^A'
+'122E0C02B0FFFF^A'
+'122E0C14430001^A'
+'122E0C25A90001^A'
+'122E0C37310003^A'
+END_ARRAY 1 80
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /home/pgiroux/Desktop/f735a00.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/f735a00/vo1_v10.tf b/tests/pytests/data/f735a00/vo1_v10.tf
new file mode 100644
index 0000000000000000000000000000000000000000..0ce54d5df53a7c50b1257e28f7d0ac9fb7ad9ffb
--- /dev/null
+++ b/tests/pytests/data/f735a00/vo1_v10.tf
@@ -0,0 +1,470 @@
+KPL/FK
+
+Viking Orbiter 1 Frames Kernel
+===============================================================================
+
+ This frame kernel contains the complete set of frame definitions for
+ the Viking Orbiter 1 (VO1) spacecraft including definitions for the
+ spacecraft frame, instrument platform frame, and science instrument
+ frames.
+
+
+Version and Date
+-------------------------------------------------------------------------------
+
+ Version 1.0 -- December 1, 2005 -- Boris Semenov, NAIF
+
+ Initial Release.
+
+
+References
+-------------------------------------------------------------------------------
+
+ 1. ``Frames Required Reading''
+
+ 2. ``Kernel Pool Required Reading''
+
+ 3. ``C-Kernel Required Reading''
+
+ 4. VO1 Supplemental Experiment Data Record (SEDR) file, 1976-1980.
+
+ 5. Thomas C. Duxbury/JPL, March-July, 1996
+
+
+Contact Information
+-------------------------------------------------------------------------------
+
+ Boris V. 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/CSPICE/ICY routine FURNSH loads
+ a kernel file into the pool as shown below.
+
+ CALL FURNSH ( 'frame_kernel_name' ) SPICELIB/FORTRAN
+
+ furnsh_c ( "frame_kernel_name" ); CSPICE/C
+
+ cspice_furnsh, "frame_kernel_name" ICY/IDL
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+VO1 Frames
+-------------------------------------------------------------------------------
+
+ The following VO1 frames are defined in this kernel file:
+
+ Name Relative to Type NAIF ID
+ ====================== =================== ============ =======
+
+ Spacecraft frame:
+ -----------------
+ VO1_SPACECRAFT rel.to B1950 CK -27900
+
+ Instrument Platform frame:
+ --------------------------
+ VO1_PLATFORM rel.to B1950 CK -27000
+
+ Science Instrument frames:
+ --------------------------
+ VO1_VISA rel.to PLATFORM FIXED -27001
+ VO1_VISA_TD rel.to PLATFORM FIXED -27011
+ VO1_VISB rel.to PLATFORM FIXED -27002
+ VO1_VISB_TD rel.to PLATFORM FIXED -27012
+ VO1_IRTM rel.to PLATFORM FIXED -27003
+ VO1_MAWD rel.to PLATFORM FIXED -27004
+
+
+VO1 Frames Hierarchy
+-------------------------------------------------------------------------------
+
+ The diagram below shows VO1 frames hierarchy:
+
+
+ "B1950" INERTIAL
+ +-----------------------------------------------------------+
+ | | | |
+ | <--pck | <--ck | <--ck | <--pck
+ | | | |
+ V V | V
+ "IAU_MARS" "V01_SPACECRAFT" | "IAU_EARTH"
+ ----------- ---------------- | ------------
+ |
+ |
+ V
+ "VO1_PLATFORM"
+ +---------------------------------------------------------+
+ | | | | | |
+ | <--fixed | <--fixed fixed--> | | | | <--fixed
+ | | | | | |
+ V V V | | V
+ "VO1_IRTM" "VO1_MAWD" "VO1_VISA" | | "VO1_VISB"
+ ---------- ---------- ---------- | | ----------
+ | |
+ | |
+ fixed--> | | <--fixed
+ | |
+ V V
+ "VO1_VISA_TD" "VO1_VISB_TD"
+ ------------- -------------
+
+
+Spacecraft Bus Frame
+-------------------------------------------------------------------------------
+
+ The spacecraft frame is defined as follows:
+
+ [TBD]
+
+ This diagram illustrates the spacecraft bus frame:
+
+ [TBD]
+
+ Since the S/C bus attitude with respect to an inertial frame is
+ provided by a C kernel (see [3] for more information), this frame is
+ defined as a CK-based frame.
+
+ \begindata
+
+ FRAME_VO1_SPACECRAFT = -27900
+ FRAME_-27900_NAME = 'VO1_SPACECRAFT'
+ FRAME_-27900_CLASS = 3
+ FRAME_-27900_CLASS_ID = -27900
+ FRAME_-27900_CENTER = -27
+ CK_-27900_SCLK = -27
+ CK_-27900_SPK = -27
+
+ \begintext
+
+
+Instrument Platform Frame
+-------------------------------------------------------------------------------
+
+ The instrument platform frame is defined as follows:
+
+ [TBD]
+
+ This diagram illustrates the instrument platform frame:
+
+ [TBD]
+
+ Since the platform attitude with respect to an inertial frame is
+ provided by a C kernel (see [3] for more information), this frame is
+ defined as a CK-based frame.
+
+ \begindata
+
+ FRAME_VO1_PLATFORM = -27000
+ FRAME_-27000_NAME = 'VO1_PLATFORM'
+ FRAME_-27000_CLASS = 3
+ FRAME_-27000_CLASS_ID = -27000
+ FRAME_-27000_CENTER = -27
+ CK_-27000_SCLK = -27
+ CK_-27000_SPK = -27
+
+ \begintext
+
+
+VISA and VISB Frames
+-------------------------------------------------------------------------------
+
+ The frames for the Visual Imaging Subsystem Camera A (VISA) and
+ Camera B (VISB) -- VO1_VISA and VO1_VISB -- are defined as follows:
+
+ - Z axis is along the camera boresight;
+
+ - X axis is along detector lines and points toward the right
+ side of the image;
+
+ - Y axis completes the right hand frame;
+
+ - the origin of this frame is located at the camera focal point.
+
+ This diagram illustrates the camera frames:
+
+ [TBD]
+
+ Since the cameras were rigidly mounted on the instrument platform
+ their frames are defined as fixed offset frames with respect to the
+ platform frame.
+
+ The camera orientation with respect to the platform was specified in
+ [4] as the following three rotation angles:
+
+ T pl-cam = R (RASTER_ORIENTATION) R (CONE) R (-CROSS_CONE)
+ Z Y X
+
+ with the following angle values for each of the two cameras:
+
+ VISA:
+
+ CROSS_CONE = -0.707350, deg
+ CONE = -0.007580, deg
+ RASTER_ORIENTATION = 89.735690, deg
+
+ VISB:
+
+ CROSS_CONE = 0.681000, deg
+ CONE = -0.032000, deg
+ RASTER_ORIENTATION = 90.022800, deg
+
+ These angles are used in the frame definition below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the camera to the platform frame -- see [1].)
+
+ \begindata
+
+ FRAME_VO1_VISA = -27001
+ FRAME_-27001_NAME = 'VO1_VISA'
+ FRAME_-27001_CLASS = 4
+ FRAME_-27001_CLASS_ID = -27001
+ FRAME_-27001_CENTER = -27
+ TKFRAME_-27001_SPEC = 'ANGLES'
+ TKFRAME_-27001_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-27001_ANGLES = ( -0.707350, 0.007580, -89.735690 )
+ TKFRAME_-27001_AXES = ( 1, 2, 3 )
+ TKFRAME_-27001_UNITS = 'DEGREES'
+
+ FRAME_VO1_VISB = -27002
+ FRAME_-27002_NAME = 'VO1_VISB'
+ FRAME_-27002_CLASS = 4
+ FRAME_-27002_CLASS_ID = -27002
+ FRAME_-27002_CENTER = -27
+ TKFRAME_-27002_SPEC = 'ANGLES'
+ TKFRAME_-27002_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-27002_ANGLES = ( 0.681000, 0.032000, -90.022800 )
+ TKFRAME_-27002_AXES = ( 1, 2, 3 )
+ TKFRAME_-27002_UNITS = 'DEGREES'
+
+ \begintext
+
+ Thomas Duxbury provided a different set of angle values for the cameras
+ (see [5]):
+
+ VISA:
+
+ CROSS_CONE = -0.707400, deg
+ CONE = -0.007600, deg
+ RASTER_ORIENTATION = 89.735400, deg
+
+ VISB:
+
+ CROSS_CONE = 0.681300, deg
+ CONE = -0.032100, deg
+ RASTER_ORIENTATION = 90.083900, deg
+
+ To make this alignment solution available, two more frames parallel
+ to the camera frames and including the ``_TB'' suffix in the name
+ and defined below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the camera to the platform frame -- see [1].)
+
+ \begindata
+
+ FRAME_VO1_VISA_TD = -27011
+ FRAME_-27011_NAME = 'VO1_VISA_TD'
+ FRAME_-27011_CLASS = 4
+ FRAME_-27011_CLASS_ID = -27011
+ FRAME_-27011_CENTER = -27
+ TKFRAME_-27011_SPEC = 'ANGLES'
+ TKFRAME_-27011_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-27011_ANGLES = ( -0.707400, 0.007600, -89.735400 )
+ TKFRAME_-27011_AXES = ( 1, 2, 3 )
+ TKFRAME_-27011_UNITS = 'DEGREES'
+
+ FRAME_VO1_VISB_TD = -27012
+ FRAME_-27012_NAME = 'VO1_VISB_TD'
+ FRAME_-27012_CLASS = 4
+ FRAME_-27012_CLASS_ID = -27012
+ FRAME_-27012_CENTER = -27
+ TKFRAME_-27012_SPEC = 'ANGLES'
+ TKFRAME_-27012_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-27012_ANGLES = ( 0.681300, 0.032100, -90.083900 )
+ TKFRAME_-27012_AXES = ( 1, 2, 3 )
+ TKFRAME_-27012_UNITS = 'DEGREES'
+
+ \begintext
+
+
+IRTM Frame
+-------------------------------------------------------------------------------
+
+ The frame for the Infrared Thermal Mapper -- VO1_IRTM -- is defined
+ as follows:
+
+ [TBD]
+
+ This diagram illustrates the IRTM frame:
+
+ [TBD]
+
+ Since the IRTM instrument was rigidly mounted on the instrument
+ platform its frame is defined as fixed offset frames with respect to
+ the platform frame.
+
+ The instrument orientation with respect to the platform can be
+ specified using the following three rotation angles:
+
+ T pl-cam = R (RASTER_ORIENTATION) R (CONE) R (-CROSS_CONE)
+ Z Y X
+
+ with the nominal angle values:
+
+ CROSS_CONE = 0.0, deg
+ CONE = 0.0, deg
+ RASTER_ORIENTATION = 90.0, deg
+
+ These angles are used in the frame definition below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the instrument to the platform frame -- see
+ [1].)
+
+ \begindata
+
+ FRAME_VO1_IRTM = -27003
+ FRAME_-27003_NAME = 'VO1_IRTM'
+ FRAME_-27003_CLASS = 4
+ FRAME_-27003_CLASS_ID = -27003
+ FRAME_-27003_CENTER = -27
+ TKFRAME_-27003_SPEC = 'ANGLES'
+ TKFRAME_-27003_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-27003_ANGLES = ( 0.0, 0.0, -90.0 )
+ TKFRAME_-27003_AXES = ( 1, 2, 3 )
+ TKFRAME_-27003_UNITS = 'DEGREES'
+
+ \begintext
+
+
+MAWD Frame
+-------------------------------------------------------------------------------
+
+ The frame for the Mars Atmosphere Water Detector (MAWD) -- VO1_MAWD
+ -- is defined as follows:
+
+ [TBD]
+
+ This diagram illustrates the MAWD frame:
+
+ [TBD]
+
+ Since the MAWD instrument was rigidly mounted on the instrument
+ platform its frame is defined as fixed offset frames with respect to
+ the platform frame.
+
+ The instrument orientation with respect to the platform can be
+ specified using the following three rotation angles:
+
+ T pl-cam = R (RASTER_ORIENTATION) R (CONE) R (-CROSS_CONE)
+ Z Y X
+
+ with the nominal angle values:
+
+ CROSS_CONE = 0.0, deg
+ CONE = 0.0, deg
+ RASTER_ORIENTATION = 90.0, deg
+
+ These angles are used in the frame definition below.
+
+ (The frame definition below contains the opposite of the rotation
+ described above because Euler angles specified in it define
+ transformation from the instrument to the platform frame -- see
+ [1].)
+
+ \begindata
+
+ FRAME_VO1_MAWD = -27004
+ FRAME_-27004_NAME = 'VO1_MAWD'
+ FRAME_-27004_CLASS = 4
+ FRAME_-27004_CLASS_ID = -27004
+ FRAME_-27004_CENTER = -27
+ TKFRAME_-27004_SPEC = 'ANGLES'
+ TKFRAME_-27004_RELATIVE = 'VO1_PLATFORM'
+ TKFRAME_-27004_ANGLES = ( 0.0, 0.0, -90.0 )
+ TKFRAME_-27004_AXES = ( 1, 2, 3 )
+ TKFRAME_-27004_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Viking Orbiter 1 NAIF ID Codes -- Definition Section
+========================================================================
+
+ This section contains name to NAIF ID mappings for the VO1. Once the
+ contents of this file is loaded into the KERNEL POOL, these mappings
+ become available within SPICE, making it possible to use names
+ instead of ID code in the high level SPICE routine calls.
+
+ Spacecraft and its structures:
+ ------------------------------
+
+ VIKING ORBITER 1 -27
+ VO1 -27
+
+ VO1_SPACECRAFT_BUS -27900
+ VO1_SC_BUS -27900
+ VO1_SPACECRAFT -27900
+
+ VO1_INSTRUMENT_PLATFORM -27000
+ VO1_PLATFORM -27000
+
+ Science Instruments:
+ --------------------
+
+ VO1_VISA -27001
+ VO1_VISB -27002
+
+ VO1_IRTM -27003
+
+ VO1_MAWD -27004
+
+ The mappings summarized in this table are implemented by the keywords
+ below.
+
+ \begindata
+
+ NAIF_BODY_NAME += ( 'VIKING ORBITER 1' )
+ NAIF_BODY_CODE += ( -27 )
+
+ NAIF_BODY_NAME += ( 'VO1' )
+ NAIF_BODY_CODE += ( -27 )
+
+ NAIF_BODY_NAME += ( 'VO1_SPACECRAFT_BUS' )
+ NAIF_BODY_CODE += ( -27900 )
+
+ NAIF_BODY_NAME += ( 'VO1_SC_BUS' )
+ NAIF_BODY_CODE += ( -27900 )
+
+ NAIF_BODY_NAME += ( 'VO1_SPACECRAFT' )
+ NAIF_BODY_CODE += ( -27900 )
+
+ NAIF_BODY_NAME += ( 'VO1_INSTRUMENT_PLATFORM' )
+ NAIF_BODY_CODE += ( -27000 )
+
+ NAIF_BODY_NAME += ( 'VO1_PLATFORM' )
+ NAIF_BODY_CODE += ( -27000 )
+
+ NAIF_BODY_NAME += ( 'VO1_VISA' )
+ NAIF_BODY_CODE += ( -27001 )
+
+ NAIF_BODY_NAME += ( 'VO1_VISB' )
+ NAIF_BODY_CODE += ( -27002 )
+
+ NAIF_BODY_NAME += ( 'VO1_IRTM' )
+ NAIF_BODY_CODE += ( -27003 )
+
+ NAIF_BODY_NAME += ( 'VO1_MAWD' )
+ NAIF_BODY_CODE += ( -27004 )
+
+ \begintext
diff --git a/tests/pytests/test_viking_drivers.py b/tests/pytests/test_viking_drivers.py
new file mode 100644
index 0000000000000000000000000000000000000000..08876e713fea2d693e0cf90c99d6cdd954cc3bd5
--- /dev/null
+++ b/tests/pytests/test_viking_drivers.py
@@ -0,0 +1,302 @@
+import pytest
+import os
+import numpy as np
+import spiceypy as spice
+from importlib import reload
+import json
+
+import unittest
+from unittest.mock import patch
+from conftest import get_image_label, get_image_kernels, convert_kernels, compare_dicts
+
+import ale
+from ale.drivers.viking_drivers import VikingIsisLabelNaifSpiceDriver
+
+image_dict = {
+ # Viking Orbiter 1 VISCA
+ 'f004a47': {
+ 'isis': {
+ 'CameraVersion': 1,
+ 'NaifKeywords': {
+ 'BODY_CODE': 499,
+ 'BODY499_RADII': [3396.19, 3396.19, 3376.2],
+ 'BODY_FRAME_CODE': 10014,
+ 'INS-27001_TRANSX': [0.0, 0.011764705882353, 0.0],
+ 'INS-27001_TRANSY': [0.0, 0.0, 0.011764705882353],
+ 'INS-27001_ITRANSS': [0.0, 85.0, 0.0],
+ 'INS-27001_ITRANSL': [0.0, 0.0, 85.0],
+ 'FRAME_-27001_CLASS_ID': -27001.0,
+ 'INS-27001_CK_REFERENCE_ID': 2.0,
+ 'TKFRAME_-27001_ANGLES': [-7.073500e-01, 7.580000e-03, -8.973569e+01],
+ 'FRAME_-27001_CENTER': -27.0,
+ 'TKFRAME_-27001_UNITS': 'DEGREES',
+ 'TKFRAME_-27001_RELATIVE': 'VO1_PLATFORM',
+ 'INS-27001_CK_FRAME_ID': -27000.0,
+ 'FRAME_-27001_NAME': 'VO1_VISA',
+ 'TKFRAME_-27001_AXES': [1., 2., 3.],
+ 'TKFRAME_-27001_SPEC': 'ANGLES',
+ 'FRAME_-27001_CLASS': 4.0,
+ 'BODY499_POLE_DEC': [52.8865, -0.0609, 0.0],
+ 'BODY499_POLE_RA': [317.68143, -0.1061, 0.0],
+ 'BODY499_PM': [176.63, 350.89198226, 0.0]},
+ 'InstrumentPointing': {
+ 'TimeDependentFrames': [-27000, 2, 1],
+ 'ConstantFrames': [-27001, -27000],
+ 'ConstantRotation': [0.0046130633441499, 0.99991314725849,
+ 0.012345751747229, -0.99998935101548,
+ 0.0046143450547129, -7.53349414399155e-05,
+ -1.32295956915258e-04, -0.012345272752653,
+ 0.99992378546489],
+ 'CkTableStartTime': -742324621.5707,
+ 'CkTableEndTime': -742324621.5707,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-742324621.5707],
+ 'Quaternions': [[0.52681010146894,-0.23107660776762,0.74879344146168,-0.32921588715745]],
+ 'AngularVelocity': [[0.0,0.0,0.0]]},
+ 'BodyRotation': {
+ 'TimeDependentFrames': [10014, 1],
+ 'CkTableStartTime': -742324621.5707,
+ 'CkTableEndTime': -742324621.5707,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-742324621.5707],
+ 'Quaternions': [[-0.61809902466787,0.31800072486684,-0.0089011036547319,0.71885318740513]],
+ 'AngularVelocity': [[3.16267887431502e-05,-2.87717183114938e-05,5.65351035056844e-05]]},
+ 'InstrumentPosition': {
+ 'SpkTableStartTime': -742324621.5707,
+ 'SpkTableEndTime': -742324621.5707,
+ 'SpkTableOriginalSize': 1.0,
+ 'EphemerisTimes': [-742324621.5707],
+ 'Positions': [[2968.0235853136,3479.4553212221,1904.2575671941]],
+ 'Velocities': [[-1.9793481062728,-0.62668469080666,3.3004150826369]]},
+ 'SunPosition': {
+ 'SpkTableStartTime': -742324621.5707,
+ 'SpkTableEndTime': -742324621.5707,
+ 'SpkTableOriginalSize': 1.0,
+ 'EphemerisTimes': [-742324621.5707],
+ 'Positions': [[244748920.95492,-35758272.270036,-23031611.614447]],
+ 'Velocities': [[3.182248924045,19.865617818691,9.025318966287]]}}},
+
+ # Viking Orbiter 1 VISCB
+ 'f735a00': {
+ 'isis': {
+ 'CameraVersion': 1,
+ 'NaifKeywords': {'BODY_CODE': 499,
+ 'BODY499_RADII': [3396.19, 3396.19, 3376.2],
+ 'BODY_FRAME_CODE': 10014,
+ 'INS-27002_TRANSX' : [0.0, 0.011764705882353, 0.0],
+ 'INS-27002_TRANSY' : [0.0, 0.0, 0.011764705882353],
+ 'INS-27002_ITRANSS' : [0.0, 85.0, 0.0],
+ 'INS-27002_ITRANSL' : [0.0, 0.0, 85.0],
+ 'INS-27002_CK_REFERENCE_ID': 2.0,
+ 'TKFRAME_-27002_ANGLES': [ 6.81000e-01, 3.20000e-02, -9.00228e+01],
+ 'FRAME_-27002_CENTER': -27.0,
+ 'FRAME_-27002_NAME': 'VO1_VISB',
+ 'TKFRAME_-27002_RELATIVE': 'VO1_PLATFORM',
+ 'INS-27002_CK_FRAME_ID': -27000.0,
+ 'TKFRAME_-27002_AXES': [1., 2., 3.],
+ 'TKFRAME_-27002_SPEC': 'ANGLES',
+ 'FRAME_-27002_CLASS_ID': -27002.0,
+ 'FRAME_-27002_CLASS': 4.0,
+ 'TKFRAME_-27002_UNITS': 'DEGREES',
+ 'BODY499_POLE_DEC': [52.8865, -0.0609, 0. ],
+ 'BODY499_POLE_RA': [ 3.1768143e+02, -1.0610000e-01, 0.0000000e+00],
+ 'BODY499_PM': [176.63 , 350.89198226, 0. ]
+ },
+ 'InstrumentPointing': {'TimeDependentFrames': [-27000, 2, 1],
+ 'CkTableStartTime': -679343589.99066,
+ 'CkTableEndTime': -679343589.99066,
+ 'CkTableOriginalSize': 1,
+ 'ConstantFrames': [-27002, -27000],
+ 'ConstantRotation': [-3.97934996888762e-04, 0.99992928417985, -0.011885633652183, -0.99999976485974,
+ -4.04545016850005e-04, -5.53736215647129e-04,-5.58505331602587e-04, 0.011885410506373,
+ 0.99992921003884],
+ 'EphemerisTimes': [-679343589.99066],
+ 'Quaternions': [[0.027631069885584,-0.042844653015238,0.63550118209549,0.77041489292473]],
+ 'AngularVelocity': [[0.0,0.0,0.0]]},
+ 'BodyRotation': {'TimeDependentFrames': [10014, 1],
+ 'CkTableStartTime': -679343589.99066,
+ 'CkTableEndTime': -679343589.99066,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-679343589.99066],
+ 'Quaternions': [[-0.7279379541667,0.013628253415821,0.31784329352737,-0.60736829547822]],
+ 'AngularVelocity': [[3.16266124745133e-05,-2.87736941823106e-05,5.6534196515818e-05]]},
+ 'InstrumentPosition': {'SpkTableStartTime': -679343589.99066,
+ 'SpkTableEndTime': -679343589.99066,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': [-679343589.99066],
+ 'Positions': [[3804.7657059701,-29029.379045591,-8152.7028148086]],
+ 'Velocities': [[0.61887065223952,-0.54866918471373,-0.037514399215278]]},
+ 'SunPosition': {'SpkTableStartTime': -679343589.99066,
+ 'SpkTableEndTime': -679343589.99066,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': [-679343589.99066],
+ 'Positions': [[242154815.26715,36901072.557543,10366793.725074]],
+ 'Velocities': [[-4.6653907628395,19.836822435663,9.2246820568878]]}}},
+
+ # Viking Orbiter 2 VISCA
+ 'f004b65': {
+ 'isis': {
+ 'CameraVersion': 1,
+ 'NaifKeywords': {'BODY_CODE': 499,
+ 'BODY499_RADII': [3396.19, 3396.19, 3376.2],
+ 'BODY_FRAME_CODE': 10014,
+ 'INS-30001_TRANSX': [0.0, 0.011764705882353, 0.0],
+ 'INS-30001_TRANSY': [0.0, 0.0, 0.011764705882353],
+ 'INS-30001_ITRANSS': [0.0, 85.0, 0.0],
+ 'INS-30001_ITRANSL': [0.0, 0.0, 85.0],
+ 'TKFRAME_-30001_UNITS': 'DEGREES',
+ 'TKFRAME_-30001_ANGLES': [-6.7933000e-01, 2.3270000e-02, -8.9880691e+01],
+ 'FRAME_-30001_CENTER': -30.0,
+ 'FRAME_-30001_NAME': 'VO2_VISA',
+ 'TKFRAME_-30001_AXES': [1., 2., 3.],
+ 'TKFRAME_-30001_SPEC': 'ANGLES',
+ 'FRAME_-30001_CLASS_ID': -30001.0,
+ 'TKFRAME_-30001_RELATIVE': 'VO2_PLATFORM',
+ 'INS-30001_CK_FRAME_ID': -30000.0,
+ 'FRAME_-30001_CLASS': 4.0,
+ 'INS-30001_CK_REFERENCE_ID': 2.0,
+ 'BODY499_POLE_DEC': [52.8865, -0.0609, 0.0],
+ 'BODY499_POLE_RA': [317.68143, -0.1061, 0.0],
+ 'BODY499_PM': [176.63, 350.89198226, 0.0]},
+ 'InstrumentPointing': {'TimeDependentFrames': [-30000, 2, 1],
+ 'ConstantFrames': [-30001, -30000],
+ 'ConstantRotation': [0.0020823332006485, 0.99992753405817,
+ 0.011857087365694, -0.99999774946761,
+ 0.0020870022808706, -3.81419977354999e-04,
+ -4.06138105773791e-04, -0.011856266437452,
+ 0.999929629523],
+ 'CkTableStartTime': -738066654.57901,
+ 'CkTableEndTime': -738066654.57901,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-738066654.57901],
+ 'Quaternions': [[0.24875871307312,-0.29788492418696,0.65237809296024,0.65098886199219]],
+ 'AngularVelocity': [[0.0,0.0,0.0]]},
+ 'BodyRotation': {'TimeDependentFrames': [10014, 1],
+ 'CkTableStartTime': -738066654.57901,
+ 'CkTableEndTime': -738066654.57901,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-738066654.57901],
+ 'Quaternions': [[-0.53502287519129,0.31507831776488,-0.043929225721799,0.7826534353237]],
+ 'AngularVelocity': [[3.16267768298231e-05,-2.87718518940354e-05,5.65350421875015e-05]]},
+ 'InstrumentPosition': {'SpkTableStartTime': -738066654.57901,
+ 'SpkTableEndTime': -738066654.57901,
+ 'SpkTableOriginalSize': 1.0,
+ 'EphemerisTimes': [-738066654.57901],
+ 'Positions': [[4553.9327290117,-1511.8974073078,1092.1996085889]],
+ 'Velocities': [[-0.24727917113306,2.4028815935793,3.0999864190804]]},
+ 'SunPosition': {'SpkTableStartTime': -738066654.57901,
+ 'SpkTableEndTime': -738066654.57901,
+ 'SpkTableOriginalSize': 1.0,
+ 'EphemerisTimes': [-738066654.57901],
+ 'Positions': [[238736005.86526,49393960.380247,16187072.695853]],
+ 'Velocities': [[-6.0452401714101,19.592116149966,9.1498650350044]]}}},
+
+ # Viking Orbiter 2 VISCB
+ 'f704b28': {
+ 'isis': {
+ 'CameraVersion': 1,
+ 'NaifKeywords': {'BODY_CODE': 499,
+ 'BODY499_RADII': [3396.19, 3396.19, 3376.2],
+ 'BODY_FRAME_CODE': 10014,
+ 'INS-30002_TRANSX': [0.0, 0.011764705882353, 0.0],
+ 'INS-30002_TRANSY': [0.0, 0.0, 0.011764705882353],
+ 'INS-30002_ITRANSS': [0.0, 85.0, 0.0],
+ 'INS-30002_ITRANSL': [0.0, 0.0, 85.0],
+ 'TKFRAME_-30002_AXES': [1., 2., 3.],
+ 'TKFRAME_-30002_SPEC': 'ANGLES',
+ 'TKFRAME_-30002_ANGLES':[ 6.630000e-01, 4.400000e-02, -8.966379e+01],
+ 'FRAME_-30002_CENTER': -30.0,
+ 'FRAME_-30002_CLASS': 4.0,
+ 'INS-30002_CK_FRAME_ID': -30000.0,
+ 'FRAME_-30002_CLASS_ID': -30002.0,
+ 'TKFRAME_-30002_UNITS': 'DEGREES',
+ 'TKFRAME_-30002_RELATIVE': 'VO2_PLATFORM',
+ 'INS-30002_CK_REFERENCE_ID': 2.0,
+ 'FRAME_-30002_NAME': 'VO2_VISB',
+ 'BODY499_POLE_DEC': [52.8865, -0.0609, 0.0],
+ 'BODY499_POLE_RA': [ 317.68143, -0.1061, 0.0],
+ 'BODY499_PM': [176.63, 350.89198226, 0.0]},
+ 'InstrumentPointing': {'TimeDependentFrames': [-30000, 2, 1],
+ 'ConstantFrames': [-30002, -30000],
+ 'ConstantRotation': [0.0058679360725137, 0.99991588736024,
+ -0.011566569536285, -0.9999824886402,
+ 0.0058586590004418, -8.35779681749578e-04,
+ -7.67944795396292e-04, 0.011571271291668,
+ 0.99993275570985],
+ 'CkTableStartTime': -676709864.3045,
+ 'CkTableEndTime': -676709864.3045,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-676709864.3045],
+ 'Quaternions': [[0.14671376032888,-0.20207775752139,0.96766874650245,0.03545207310812]],
+ 'AngularVelocity': [[0.0,0.0,0.0]]},
+ 'BodyRotation': {'TimeDependentFrames': [10014, 1],
+ 'CkTableStartTime': -676709864.3045,
+ 'CkTableEndTime': -676709864.3045,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-676709864.3045],
+ 'Quaternions': [[-0.028648237381698,0.24168074000221,-0.20688348409661,0.94761222154157]],
+ 'AngularVelocity': [[3.16266051008033e-05,-2.87737768090931e-05,5.6534158586979e-05]]},
+ 'InstrumentPosition': {'SpkTableStartTime': -676709864.3045,
+ 'SpkTableEndTime': -676709864.3045,
+ 'SpkTableOriginalSize': 1.0,
+ 'EphemerisTimes': [-676709864.3045],
+ 'Positions': [[3297.8743337482,966.46050377782,10725.740343691]],
+ 'Velocities': [[-0.44211958524766,1.2883896612093,1.9012944589374]]},
+ 'SunPosition': {'SpkTableStartTime': -676709864.3045,
+ 'SpkTableEndTime': -676709864.3045,
+ 'SpkTableOriginalSize': 1.0,
+ 'EphemerisTimes': [-676709864.3045],
+ 'Positions': [[222364052.49946,87428117.498071,34077452.005079]],
+ 'Velocities': [[-10.327617595005,18.315940117221,8.6804664968805]]}}}
+ }
+
+@pytest.fixture(scope="module")
+def test_kernels():
+ updated_kernels = {}
+ binary_kernels = {}
+ for image in image_dict.keys():
+ kernels = get_image_kernels(image)
+ updated_kernels[image], binary_kernels[image] = convert_kernels(kernels)
+ yield updated_kernels
+ for kern_list in binary_kernels.values():
+ for kern in kern_list:
+ os.remove(kern)
+
+@pytest.mark.parametrize("label_type", ['isis3'])
+@pytest.mark.parametrize("formatter", ['isis'])
+@pytest.mark.parametrize("image", image_dict.keys())
+def test_viking1_load(test_kernels, label_type, formatter, image):
+ label_file = get_image_label(image, label_type)
+ isis_isd = ale.load(label_file, props={'kernels': test_kernels[image]}, formatter=formatter)
+ print(isis_isd)
+ assert compare_dicts(isis_isd, image_dict[image][formatter]) == []
+
+# ========= Test isislabel and naifspice driver =========
+class test_isis_naif(unittest.TestCase):
+
+ def setUp(self):
+ label = get_image_label("f735a00", "isis3")
+ self.driver = VikingIsisLabelNaifSpiceDriver(label)
+
+ def test_short_mission_name(self):
+ assert self.driver.short_mission_name == 'viking'
+
+ def test_spacecraft_name(self):
+ assert self.driver.spacecraft_name == 'VIKING ORBITER 1'
+
+ def test_ikid(self):
+ assert self.driver.ikid == -27002
+
+ def test_alt_ikid(self):
+ assert self.driver.alt_ikid == -27999
+
+ def test_ephemeris_start_time(self):
+ with patch('ale.drivers.viking_drivers.spice.scs2e', return_value=54321) as scs2e:
+ assert self.driver.ephemeris_start_time == 54324.99
+ scs2e.assert_called_with(-27999, '40031801')
+
+ @patch('ale.base.label_isis.IsisLabel.exposure_duration', 0.43)
+ def test_ephemeris_start_time_different_exposure(self):
+ with patch('ale.drivers.viking_drivers.spice.scs2e', return_value=54321) as scs2e:
+ assert self.driver.ephemeris_start_time == 54322.75
+ scs2e.assert_called_with(-27999, '40031801')