From e59d297baf9d5b0a298994849426a0b2bcfbf30c Mon Sep 17 00:00:00 2001
From: Jesse Mapel <jmapel@usgs.gov>
Date: Mon, 26 Feb 2024 14:55:01 -0700
Subject: [PATCH] Adds Cassini Vims driver for use within ISIS (#466)
* Added cassini vims vis/ir drivers
* Various cassini vims centric driver changes
* fixed rebase conflict
* Finalized cassini vims drivers
* Added cassini vims test data
* Added tests for cassini vims
* Updated cassini vims tests after pck loading order change
* Changed env var monkey patch from ISIS3DATA to ISISDATA
* Fixed typos in doc strings
---------
Co-authored-by: acpaquette <acp263@nau.edu>
Co-authored-by: acpaquette <acpaquette@usgs.gov>
---
ale/drivers/co_drivers.py | 227 +-
tests/pytests/data/isds/cassinivims_isd.json | 1784 +++++
.../05357_05362ra_0_sliced_-82000.xc | 1803 +++++
.../05357_05362ra_1_sliced_-82000.xc | 1803 +++++
tests/pytests/data/v1514284191_1/cas00172.tsc | 279 +
.../data/v1514284191_1/cas_v40_usgs.tf | 4522 ++++++++++++
.../data/v1514284191_1/cpck15Dec2017.tpc | 6229 +++++++++++++++++
tests/pytests/data/v1514284191_1/naif0012.tls | 152 +
tests/pytests/data/v1514284191_1/pck00009.tpc | 3639 ++++++++++
.../v1514284191_1/v1514284191_1_vis_isis.lbl | 448 ++
.../v1514284191_1_vis_isis_0.xsp | 401 ++
.../v1514284191_1_vis_isis_1.xsp | 761 ++
.../data/v1514284191_1/vimsAddendum04.ti | 38 +
tests/pytests/test_cassini_drivers.py | 89 +-
tests/pytests/test_util.py | 4 +-
15 files changed, 22157 insertions(+), 22 deletions(-)
create mode 100644 tests/pytests/data/isds/cassinivims_isd.json
create mode 100644 tests/pytests/data/v1514284191_1/05357_05362ra_0_sliced_-82000.xc
create mode 100644 tests/pytests/data/v1514284191_1/05357_05362ra_1_sliced_-82000.xc
create mode 100644 tests/pytests/data/v1514284191_1/cas00172.tsc
create mode 100644 tests/pytests/data/v1514284191_1/cas_v40_usgs.tf
create mode 100644 tests/pytests/data/v1514284191_1/cpck15Dec2017.tpc
create mode 100644 tests/pytests/data/v1514284191_1/naif0012.tls
create mode 100644 tests/pytests/data/v1514284191_1/pck00009.tpc
create mode 100644 tests/pytests/data/v1514284191_1/v1514284191_1_vis_isis.lbl
create mode 100644 tests/pytests/data/v1514284191_1/v1514284191_1_vis_isis_0.xsp
create mode 100644 tests/pytests/data/v1514284191_1/v1514284191_1_vis_isis_1.xsp
create mode 100644 tests/pytests/data/v1514284191_1/vimsAddendum04.ti
diff --git a/ale/drivers/co_drivers.py b/ale/drivers/co_drivers.py
index a062d83..acfcce0 100644
--- a/ale/drivers/co_drivers.py
+++ b/ale/drivers/co_drivers.py
@@ -12,21 +12,36 @@ from ale.base.label_pds3 import Pds3Label
from ale.base.label_isis import IsisLabel
from ale.base.type_distortion import RadialDistortion, NoDistortion
from ale.base.type_sensor import Framer
+from ale.base.type_sensor import LineScanner
from ale.rotation import ConstantRotation
from ale.transformation import FrameChain
+from ale.util import query_kernel_pool
from scipy.spatial.transform import Rotation
-id_lookup = {
+vims_id_lookup = {
+ "VIMS_VIS" : "CASSINI_VIMS_V",
+ "VIMS_IR" : "CASSINI_VIMS_IR"
+}
+
+vims_name_lookup = {
+ "VIMS" : "Visible and Infrared Mapping Spectrometer",
+}
+
+iss_id_lookup = {
"ISSNA" : "CASSINI_ISS_NAC",
"ISSWA" : "CASSINI_ISS_WAC"
}
-name_lookup = {
+iss_name_lookup = {
"ISSNA" : "Imaging Science Subsystem Narrow Angle Camera",
"ISSWA" : "Imaging Science Subsystem Wide Angle Camera"
}
+spacecraft_name_lookup = {
+ 'Cassini-Huygens': 'Cassini'
+}
+
nac_filter_to_focal_length = {
("P0","BL2"):2002.19,
("P0","CB1"):2002.30,
@@ -126,7 +141,7 @@ class CassiniIssIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, RadialDis
: str
instrument id
"""
- return id_lookup[super().instrument_id]
+ return iss_id_lookup[super().instrument_id]
@property
def spacecraft_name(self):
@@ -151,7 +166,7 @@ class CassiniIssIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, RadialDis
: str
Name of the sensor
"""
- return name_lookup[super().instrument_id]
+ return iss_name_lookup[super().instrument_id]
@property
def ephemeris_start_time(self):
@@ -293,6 +308,204 @@ class CassiniIssIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, RadialDis
def sensor_model_version(self):
return 1
+class CassiniVimsIsisLabelNaifSpiceDriver(LineScanner, IsisLabel, NaifSpice, NoDistortion, Driver):
+
+ @property
+ def vims_channel(self):
+ if not hasattr(self, '_vims_channel'):
+ self._vims_channel = self.label['IsisCube']["Instrument"]["Channel"]
+ return self._vims_channel
+
+ @property
+ def instrument_id(self):
+ """
+ Returns an instrument id for uniquely identifying the instrument, but often
+ also used to be piped into Spice Kernels to acquire IKIDs. Therefore they
+ the same ID the Spice expects in bods2c calls.
+ Expects instrument_id to be defined in the IsisLabel mixin. This should be
+ a string of the form 'CTX'
+
+ Returns
+ -------
+ : str
+ instrument id
+ """
+ return vims_id_lookup[super().instrument_id + "_" + self.vims_channel]
+
+ @property
+ def sensor_name(self):
+ """
+ ISIS doesn't propagate this to the ingested cube label, so hard-code it.
+ """
+ return vims_name_lookup[super().instrument_id]
+
+ @property
+ def spacecraft_name(self):
+ """
+ Returns the spacecraft name used in various Spice calls to acquire
+ ephemeris data.
+ Expects the platform_name to be defined. This should be a string of
+ the form 'Mars_Reconnaissance_Orbiter'
+
+ Returns
+ -------
+ : str
+ spacecraft name
+ """
+ return spacecraft_name_lookup[super().platform_name]
+
+ @property
+ def exposure_duration(self):
+ """
+ The exposure duration of the image, in seconds
+
+ Returns
+ -------
+ : float
+ Exposure duration in seconds
+ """
+ if 'ExposureDuration' in self.label['IsisCube']['Instrument']:
+ exposure_duration = self.label['IsisCube']['Instrument']['ExposureDuration']
+
+ for i in exposure_duration:
+ if i.units == "VIS":
+ exposure_duration = i
+
+ exposure_duration = exposure_duration.value * 0.001
+ return exposure_duration
+ else:
+ return self.line_exposure_duration
+
+ @property
+ def focal_length(self):
+ """
+ Hardcoded value taken from ISIS
+ """
+ if not hasattr(self, '_focal_length'):
+ if self.vims_channel == "VIS":
+ self._focal_length = 143.0
+ else:
+ self._focal_length = 426.0
+ return self._focal_length
+
+ @property
+ def detector_center_line(self):
+ return 0
+
+ @property
+ def detector_center_sample(self):
+ return 0
+
+ def compute_vims_time(self, line, sample, number_of_samples, mode="VIS"):
+ instrument_group = self.label["IsisCube"]["Instrument"]
+ time = str(instrument_group["NativeStartTime"])
+ int_time, decimal_time = str(time).split(".")
+
+ ephemeris_time = spice.scs2e(self.spacecraft_id, int_time)
+ ephemeris_time += float(decimal_time) / 15959.0
+
+ ir_exp = float(instrument_group["ExposureDuration"][0]) * 1.01725 / 1000.0;
+ vis_exp = float(instrument_group["ExposureDuration"][1]) / 1000.0
+
+ interline_delay = (float(instrument_group["InterlineDelayDuration"]) * 1.01725) / 1000.0
+
+ swath_width = instrument_group["SwathWidth"];
+
+ if mode == "VIS":
+ ephemeris_time = (float(ephemeris_time) + (((ir_exp * swath_width) - vis_exp) / 2.0)) + ((line + 0.5) * vis_exp)
+ elif mode == "IR":
+ ephemeris_time = float(ephemeris_time) + (line * number_of_samples * ir_exp) + (line * interline_delay) + ((sample + 0.5) * ir_exp)
+
+ return ephemeris_time
+
+ @property
+ def ephemeris_start_time(self):
+ return self.compute_vims_time(0 - 0.5, 0 - 0.5, self.image_samples, mode=self.vims_channel)
+
+ @property
+ def ephemeris_stop_time(self):
+ return self.compute_vims_time((self.image_lines - 1) + 0.5, (self.image_samples - 1) + 0.5, self.image_samples, mode=self.vims_channel)
+
+ @property
+ def sensor_model_version(self):
+ """
+ Returns instrument model version
+ Returns
+ -------
+ : int
+ ISIS sensor model version
+ """
+ try:
+ return super().sensor_model_version
+ except:
+ return 1
+
+
+class CassiniVimsIsisLabelIsisSpiceDriver(LineScanner, IsisLabel, IsisSpice, NoDistortion, Driver):
+
+ @property
+ def instrument_id(self):
+ """
+ Returns an instrument id for uniquely identifying the instrument, but often
+ also used to be piped into Spice Kernels to acquire IKIDs. Therefore they
+ the same ID the Spice expects in bods2c calls.
+ Expects instrument_id to be defined in the IsisLabel mixin. This should be
+ a string of the form 'CTX'
+
+ Returns
+ -------
+ : str
+ instrument id
+ """
+
+ image_type = self.label['IsisCube']["Instrument"]["Channel"]
+ return vims_id_lookup[super().instrument_id + "_" + image_type]
+
+ @property
+ def sensor_name(self):
+ """
+ ISIS doesn't propagate this to the ingested cube label, so hard-code it.
+ """
+ return "Visible and Infrared Mapping Spectrometer"
+
+ @property
+ def spacecraft_name(self):
+ """
+ Returns the spacecraft name used in various Spice calls to acquire
+ ephemeris data.
+ Expects the platform_name to be defined. This should be a string of
+ the form 'Mars_Reconnaissance_Orbiter'
+
+ Returns
+ -------
+ : str
+ spacecraft name
+ """
+ return spacecraft_name_lookup[super().platform_name]
+
+ @property
+ def exposure_duration(self):
+ """
+ The exposure duration of the image, in seconds
+
+ Returns
+ -------
+ : float
+ Exposure duration in seconds
+ """
+ if 'ExposureDuration' in self.label['IsisCube']['Instrument']:
+ exposure_duration = self.label['IsisCube']['Instrument']['ExposureDuration']
+
+ for i in exposure_duration:
+ if i.units == "VIS":
+ exposure_duration = i
+
+ exposure_duration = exposure_duration.value * 0.001
+ return exposure_duration
+ else:
+ return self.line_exposure_duration
+
+
class CassiniIssPds3LabelNaifSpiceDriver(Framer, Pds3Label, NaifSpice, RadialDistortion, Driver):
"""
Cassini mixin class for defining Spice calls.
@@ -313,7 +526,7 @@ class CassiniIssPds3LabelNaifSpiceDriver(Framer, Pds3Label, NaifSpice, RadialDis
: str
instrument id
"""
- return id_lookup[super().instrument_id]
+ return iss_id_lookup[super().instrument_id]
@property
def focal_epsilon(self):
@@ -530,7 +743,7 @@ class CassiniIssIsisLabelIsisSpiceDriver(Framer, IsisLabel, IsisSpice, NoDistort
: str
ID of the sensor
"""
- return id_lookup[super().instrument_id]
+ return iss_id_lookup[super().instrument_id]
@property
def sensor_name(self):
@@ -542,7 +755,7 @@ class CassiniIssIsisLabelIsisSpiceDriver(Framer, IsisLabel, IsisSpice, NoDistort
: str
Name of the sensor
"""
- return name_lookup[super().instrument_id]
+ return iss_name_lookup[super().instrument_id]
@property
def center_ephemeris_time(self):
diff --git a/tests/pytests/data/isds/cassinivims_isd.json b/tests/pytests/data/isds/cassinivims_isd.json
new file mode 100644
index 0000000..98ba7fc
--- /dev/null
+++ b/tests/pytests/data/isds/cassinivims_isd.json
@@ -0,0 +1,1784 @@
+{
+ "isis_camera_version": 1,
+ "image_lines": 64,
+ "image_samples": 64,
+ "name_platform": "Cassini-Huygens",
+ "name_sensor": "Visible and Infrared Mapping Spectrometer",
+ "reference_height": {
+ "maxheight": 1000,
+ "minheight": -1000,
+ "unit": "m"
+ },
+ "name_model": "USGS_ASTRO_LINE_SCANNER_SENSOR_MODEL",
+ "interpolation_method": "lagrange",
+ "line_scan_rate": [
+ [
+ 0.5,
+ -320.0,
+ 10.0
+ ]
+ ],
+ "starting_ephemeris_time": 188863301.78065246,
+ "center_ephemeris_time": 188863621.78065246,
+ "radii": {
+ "semimajor": 2575.0,
+ "semiminor": 2575.0,
+ "unit": "km"
+ },
+ "body_rotation": {
+ "time_dependent_frames": [
+ 10044,
+ 1
+ ],
+ "ck_table_start_time": 188863301.78065246,
+ "ck_table_end_time": 188863941.78065246,
+ "ck_table_original_size": 2,
+ "ephemeris_times": [
+ 188863301.78065246,
+ 188863941.78065246
+ ],
+ "quaternions": [
+ [
+ -0.9924073603427238,
+ -0.04105238646554847,
+ 0.04000491857888657,
+ -0.10882067447211988
+ ],
+ [
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+ -0.04099395891076657,
+ 0.040064788503653366,
+ -0.10737222296087812
+ ]
+ ],
+ "angular_velocities": [
+ [
+ 4.0287683281676625e-07,
+ 3.319017759357454e-07,
+ 4.530708046784237e-06
+ ],
+ [
+ 4.028768328167665e-07,
+ 3.319017759357456e-07,
+ 4.530708046784238e-06
+ ]
+ ],
+ "reference_frame": 1
+ },
+ "instrument_pointing": {
+ "time_dependent_frames": [
+ -82000,
+ 1
+ ],
+ "ck_table_start_time": 188863301.78065246,
+ "ck_table_end_time": 188863941.78065246,
+ "ck_table_original_size": 65,
+ "ephemeris_times": [
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diff --git a/tests/pytests/data/v1514284191_1/05357_05362ra_0_sliced_-82000.xc b/tests/pytests/data/v1514284191_1/05357_05362ra_0_sliced_-82000.xc
new file mode 100644
index 0000000..d7608ad
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+'30E11140A^A'
+'30E11144A^A'
+'30E11148A^A'
+'30E1114CA^A'
+'30E11150A^A'
+'30E111541F^A'
+'30E10F6CA^A'
+'30E110FCA^A'
+'30E10DE34D^A'
+'1^1'
+'DE^2'
+END_ARRAY 1 1781
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: ../vims_files/v1514284191_1_vis_isis.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/v1514284191_1/05357_05362ra_1_sliced_-82000.xc b/tests/pytests/data/v1514284191_1/05357_05362ra_1_sliced_-82000.xc
new file mode 100644
index 0000000..08508c1
--- /dev/null
+++ b/tests/pytests/data/v1514284191_1/05357_05362ra_1_sliced_-82000.xc
@@ -0,0 +1,1803 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+'ckernel.file '
+BEGIN_ARRAY 1 1781
+'TELEMETRY CASSINI S/C ATTITUDE '
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+'30E11FA8A^A'
+'30E11FACA^A'
+'30E11FB0A^A'
+'30E11FB4A^A'
+'30E11FB8A^A'
+'30E11FBCA^A'
+'30E11FC0A^A'
+'30E11FC4A^A'
+'30E11FC8A^A'
+'30E11FCCA^A'
+'30E11FD0A^A'
+'30E11FD4A^A'
+'30E11FD8A^A'
+'30E11FDCA^A'
+'30E11FE0A^A'
+'30E11FE4A^A'
+'30E11FE8A^A'
+'30E11FECA^A'
+'30E11FF0A^A'
+'30E11FF4A^A'
+'30E11FF8A^A'
+'30E11FFCA^A'
+'30E12000A^A'
+'30E12004A^A'
+'30E12008A^A'
+'30E1200CA^A'
+'30E12010A^A'
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+'30E1201CA^A'
+'30E12020A^A'
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+'30E12230A^A'
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+'30E12240A^A'
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+'30E12248A^A'
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+'30E12250A^A'
+'30E12254A^A'
+'30E12258A^A'
+'30E1225CA^A'
+'30E12260A^A'
+'30E12264A^A'
+'30E12268A^A'
+'30E1226CA^A'
+'30E12270A^A'
+'30E12274A^A'
+'30E12278A^A'
+'30E1227CA^A'
+'30E12280A^A'
+'30E12284A^A'
+'30E12288A^A'
+'30E1228CA^A'
+'30E12290A^A'
+'30E12294A^A'
+'30E12298A^A'
+'30E1229CA^A'
+'30E122A0A^A'
+'30E122A4A^A'
+'30E122A8A^A'
+'30E122ACA^A'
+'30E122B0A^A'
+'30E122B4A^A'
+'30E122B8A^A'
+'30E122BCA^A'
+'30E122C0A^A'
+'30E122C4A^A'
+'30E122C8A^A'
+'30E122CCA^A'
+'30E122D0A^A'
+'30E122D4A^A'
+'30E122D8A^A'
+'30E122DCA^A'
+'30E122E0A^A'
+'30E122E4A^A'
+'30E122E8A^A'
+'30E122ECA^A'
+'30E122F0A^A'
+'30E122F4A^A'
+'30E122F8A^A'
+'30E122FCA^A'
+'30E12300A^A'
+'30E12304A^A'
+'30E12308A^A'
+'30E1230CA^A'
+'30E12310A^A'
+'30E12314A^A'
+'30E123167F^A'
+'30E12130A^A'
+'30E122C0A^A'
+'30E11FA67E^A'
+'1^1'
+'DE^2'
+END_ARRAY 1 1781
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: ../vims_files/v1514284191_1_vis_isis.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/v1514284191_1/cas00172.tsc b/tests/pytests/data/v1514284191_1/cas00172.tsc
new file mode 100644
index 0000000..269f1d1
--- /dev/null
+++ b/tests/pytests/data/v1514284191_1/cas00172.tsc
@@ -0,0 +1,279 @@
+KPL/SCLK
+
+This file is a SPICE spacecraft clock (SCLK) kernel. This file was generated
+by the NAIF MOSPICE utility program MAKCLK, version 4.0.0, 11-MAR-2009. Please refer to the
+SCLK Required Reading file, NAIF document number 222, and the MAKCLK User's
+Guide, NAIF document number 267, for information regarding this kernel file.
+
+\begindata
+
+SCLK_KERNEL_ID = ( @2018-02-15/13:19:44.80 )
+
+SCLK_DATA_TYPE_82 = ( 1 )
+SCLK01_TIME_SYSTEM_82 = ( 2 )
+SCLK01_N_FIELDS_82 = ( 2 )
+SCLK01_MODULI_82 = ( 4294967296 256 )
+SCLK01_OFFSETS_82 = ( 0 0 )
+SCLK01_OUTPUT_DELIM_82 = ( 1 )
+
+SCLK_PARTITION_START_82 = ( 1.7772134886400E+11 )
+
+SCLK_PARTITION_END_82 = ( 1.0995116277750E+12 )
+
+SCLK01_COEFFICIENTS_82 = (
+
+ 0.0000000000000E+00 -6.3119514881600E+08 1.0000000000000E+00
+ 1.2098765056000E+10 -5.8393434781600E+08 1.0000000000000E+00
+ 2.0171981312000E+10 -5.5239834681600E+08 1.0000000000000E+00
+ 2.8245197568000E+10 -5.2086234581600E+08 1.0000000000000E+00
+ 4.4413748224000E+10 -4.5770394481600E+08 1.0000000000000E+00
+ 6.4629966080000E+10 -3.7873434381600E+08 1.0000000000000E+00
+ 8.0798516736000E+10 -3.1557594281600E+08 1.0000000000000E+00
+ 8.8871732992000E+10 -2.8403994181600E+08 1.0000000000000E+00
+ 1.0097049804800E+11 -2.3677914081600E+08 1.0000000000000E+00
+ 1.0904371430400E+11 -2.0524313981600E+08 1.0000000000000E+00
+ 1.1711693056000E+11 -1.7370713881600E+08 1.0000000000000E+00
+ 1.2925993241600E+11 -1.2627353781600E+08 1.0000000000000E+00
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+ 2.9877684204800E+11 5.3589788642400E+08 9.9999359671737E-01
+ 2.9893120662300E+11 5.3650086918400E+08 9.9999359770177E-01
+ 2.9950603270500E+11 5.3874626919100E+08 9.9999358985534E-01
+ 3.0118704188000E+11 5.4531266918900E+08 9.9999358004700E-01
+ 3.0167364980400E+11 5.4721346918900E+08 9.9999358479558E-01
+ 3.0304499940200E+11 5.5257026919100E+08 9.9999357800000E-01 )
+
+\begintext
+
diff --git a/tests/pytests/data/v1514284191_1/cas_v40_usgs.tf b/tests/pytests/data/v1514284191_1/cas_v40_usgs.tf
new file mode 100644
index 0000000..3a381fc
--- /dev/null
+++ b/tests/pytests/data/v1514284191_1/cas_v40_usgs.tf
@@ -0,0 +1,4522 @@
+KPL/FK
+
+
+Cassini Spacecraft Frame Definitions Kernel
+==============================================================================
+
+ This frame kernel contains the Cassini spacecraft, science instrument, and
+ communication antennae frame definitions.
+
+
+Version and Date
+----------------------------------------------------------
+
+ The TEXT_KERNEL_ID stores version information of loaded project text
+ kernels. Each entry associated with the keyword is a string that consists
+ of four parts: the kernel name, version, entry date, and type. For example,
+ the ISS I-kernel might have an entry as follows:
+
+ TEXT_KERNEL_ID += 'CASSINI_ISS V0.0.0 29-SEPTEMBER-1999 IK'
+ | | | |
+ | | | |
+ KERNEL NAME <-------+ | | |
+ | | V
+ VERSION <-------+ | KERNEL TYPE
+ |
+ V
+ ENTRY DATE
+
+ Cassini Frame Kernel Version:
+
+ \begindata
+
+ TEXT_KERNEL_ID += 'CASSINI_FRAMES V4.0.0 05-NOV-2008 FK'
+
+ \begintext
+
+ Version 4.0 -- November 5, 2008 -- Boris Semenov
+
+ -- Added CASSINI_UVIS_SOL_OFF frame, ID -82849. (See [52])
+
+ -- Corrected typo in WAC rotation description.
+
+ -- Revised the ``Implementation Notes'' section and
+ spell-checked comments in the whole file.
+
+ Version 3.9 -- Oct 14, 2004 -- Lee Elson
+
+ -- Updated UVIS_EUV, UVIS_FUV and UVIS_HSP frames per Diane
+ Conner's request email and SCR 524 ( A. Jouchoux, 6/7/2002:
+ see [50]) which specifies slightly modified boresight
+ vectors. The instrument "Y" axis has also been determined
+ (see [51]) to point along the spacecraft -Z direction instead
+ of + Z. Change is effective beginning at: TIME:
+ 2002-266T00:00:00.000
+
+ Version 3.8.1 -- May 12, 2004 -- Tracie Sucharski
+
+ -- Updated Vims Vis and IR boresight angles to use new values from
+ Rick McCloskey's email dated 5/12/2004.
+
+ Version 3.8 -- May 10, 2004 -- Lee Elson
+
+ -- Updated CASSINI_XBAND per Diane Conner's request email. This
+ was done by modifying the CASSINI_KABAND boresight vector.
+ See [49] for details.
+
+ Version 3.7 -- November 20, 2003 -- Lee Elson
+
+ -- Updated CASSINI_XBAND per Diane Conner's request email. This
+ was done by modifying the CASSINI_KABAND boresight vector.
+ See [48] for details.
+
+ Version 3.6 -- April 18, 2003 -- Lee Elson
+
+ -- Modified CASSINI_XBAND frame definition so that its values
+ are the same as CASSINI_KABAND. Added a new frame called
+ CASSINI_XBAND_TRUE (NAIF ID -82108) that has the same
+ definition parameters as the old CASSINI_XBAND. Also modified
+ text structure so that changes are dated and stand out better
+ for the human reader. See [46] and [47] for details.
+
+ -- Modified descriptive text structure so that changes are dated
+ and stand out better for the human reader.
+
+ Version 3.5 -- September 4, 2002 -- Scott Turner, Richard West, and Rick
+ McCloskey
+
+ -- Entries for CASSINI_VIMS_IR_SOL, CASSINI_RADAR_2, and
+ CASSINI_RADAR_4 were updated to reflect current values. See
+ [42], [43], and [44] for details.
+
+ -- CASSINI_VIMS_IR_SOL is now referenced directly to the
+ spacecraft frame, CASSINI_SC_COORD, rather than
+ CASSINI_VIMS_IR.
+
+ Version 3.4 -- June 11, 2002 -- Scott Turner and Joshua Colwell
+
+ -- Entries for CASSINI_KABAND were updated per Diane Conner's
+ request email. See [38] for details.
+
+ -- Updated entries for CASSINI_CIRS_FPB, CASSINI_CIRS_FP1,
+ CASSINI_CIRS_FP3, and CASSINI_CIRS_FP4 based on updated
+ alignment information provided in ECR 100515. See [39] for
+ details.
+
+ -- Modified the entries for CASSINI_UVIS_HSP, CASSINI_UVIS_FUV,
+ and CASSINI_UVIS_EUV to match the body vector table provided
+ by Alain Jouchoux in May 3, 2002 e-mail. This same data set
+ is in the CASPER UVIS definition file. Verified that CASPER
+ and PDT give consistent results using this frame kernel.
+
+ -- Updated the entry for CASSINI_VIMS_IR to match the body
+ vector table entry provided by Rick McCloskey. See [41] for
+ details.
+
+ Version 3.3 -- February 20, 2002 -- Scott Turner
+
+ -- Updated the frame entry and documentation for
+ CASSINI_VIMS_RAD as a result of ECR 101029 and documentation
+ submitted with it. See [36] for details.
+
+ Version 3.2 -- January 22, 2002 -- Scott Turner
+
+ -- Updated frame entries for CASSINI_XBAND and CASSINI_KABAND as
+ a result of SCR 490. See [35] for details.
+
+ Version 3.1 -- August 9, 2001 -- Scott Turner
+
+ -- Updated frame entries for CASSINI_XBAND and CASSINI_KABAND as
+ a result of SCR 468. See [34] for details.
+
+ Version 3.0 -- April 23, 2001 -- Scott Turner
+
+ -- Restructured the articulating frames: CASSINI_MIMI_LEMMS1,
+ CASSINI_MIMI_LEMMS2, CASSINI_CDA, CASSINI_CAPS. They now
+ allow for multiple paths from the instrument frames to the
+ spacecraft frame depending on what C-kernels are available.
+ Use caution when loading conflicting C-kernels.
+
+ -- Renamed CASSINI_SRU to CASSINI_SRU-A and added CASSINI_SRU-B,
+ CASSINI_SRU-A_RAD, and CASSINI_SRU-B_RAD.
+
+ -- Added the CASSINI_UVIS_SOLAR frame definition to support the
+ UVIS solar occultation port FOV.
+
+ -- Removed CASSINI_UVIS_EUV_OCC and CASSINI_UVIS_FUV_OCC frame
+ definitions since the FOVs they support are actually tied to
+ CASSINI_UVIS_EUV and CASSINI_UVIS_FUV frames respectively.
+
+ -- Added the CASSINI_VIMS_IR_SOL frame definition to support the
+ IR channel solar port FOV.
+
+ Version 2.9 -- November 16, 2000 -- Scott Turner
+
+ -- Corrected the definition of CASSINI_MIMI_INCA to account for
+ the 9.5 degree offset from the spacecraft -Y axis.
+
+ -- Corrected the definition of CASSINI_INMS. The Z-axis of this
+ frame is now co-aligned with the -X axis of CASSINI_SC_COORD.
+
+ Version 2.8 -- October 9, 2000 -- Scott Turner
+
+ -- Updated CASSINI_ISS_NAC and CASSINI_ISS_WAC to reflect the
+ updates associated with the Fomalhaut images taken on
+ September 18, 2000.
+
+ -- Migrated the CASSINI_ISS_NAC_RAD, CASSINI_ISS_WAC_RAD,
+ CASSINI_VIMS_RAD, CASSINI_CIRS_RAD, CASSINI_CAPS,
+ CASSINI_CDA, CASSINI_INMS, CASSINI_MAG_PLUS,
+ CASSINI_MAG_MINUS, CASSINI_MIMI_CHEMS, CASSINI_MIMI_INCA,
+ CASSINI_MIMI_LEMMS1, CASSINI_MIMI_LEMMS2, CASSINI_RADAR_1,
+ CASSINI_RADAR_2, CASSINI_RADAR_3, CASSINI_RADAR_4,
+ CASSINI_RADAR_5, CASSINI_RPWS, CASSINI_RPWS_EXPLUS,
+ CASSINI_RPWS_EXMINUS, CASSINI_EZPLUS, CASSINI_RPWS_LP,
+ CASSINI_KUBAND, and CASSINI_SBAND frames from the prototype
+ section.
+
+ -- Updated CASSINI_XBAND and CASSINI_KABAND as the result of SCR
+ 367. These frames were migrated from the prototype section as
+ well.
+
+ Version 2.7 -- July 7, 2000 -- Scott Turner
+
+ -- Added the following frame entries RPWS requested:
+ CASSINI_RPWS_EXPLUS, CASSINI_RPWS_EXMINUS,
+ CASSINI_RPWS_EZPLUS, CASSINI_RPWS_LP to the prototype frame
+ section. See [14] for details.
+
+ -- Changed the following frame names: CASSINI_HGA_X ->
+ CASSINI_XBAND, CASSINI_HGA_S -> CASSINI_SBAND, CASSINI_HGA_KA
+ -> CASSINI_KABAND, CASSINI_HGA_KU -> CASSINI_KUBAND.
+
+ -- Halved the Euler angles associated with the CASSINI_CIRS_FP3
+ and CASSINI_FP4 frames. See [15] for details.
+
+ Version 2.6 -- June 26, 2000 -- Scott Turner
+
+ -- The RSS frame entries in the prototype section were renamed
+ to HGA based frames.
+
+ -- Removed the CASSINI_MAG frame and replaced it with the
+ CASSINI_MAG_PLUS and CASSINI_MAG_MINUS frames.
+
+ Version 2.5 -- April 2, 2000 -- Scott Turner
+
+ -- Added CASSINI_VIMS.
+
+ -- Added CASSINI_UVIS_FUV, CASSINI_UVIS_EUV,
+ CASSINI_UVIS_FUV_OCC, CASSINI_UVIS_EUV_OCC, CASSINI_UVIS_HSP,
+ and CASSINI_UVIS_HDAC.
+
+ -- Fixed the keywords defining the CASSINI_HGA frame to use the
+ proper ID code, -82101.
+
+ -- Updated CASSINI_ISS_NAC and CASSINI_ISS_WAC to reflect the
+ latest boresight information available in ECR's 100078 and
+ 100079.
+
+ Version 2.4 -- March 27, 2000 -- Scott Turner
+
+ -- Added the CIRS Focal Plane Boresight frame, CASSINI_CIRS_FPB.
+
+ -- CASSINI_CIRS_FP1, CASSINI_CIRS_FP3, CASSINI_CIRS_FP2 are no
+ longer relative to CASSINI_SC_COORD but to the intermediate
+ frame CASSINI_CIRS_FPB.
+
+ -- Migrated the CASSINI_UVIS frame from the prototype section
+ and added the CASSINI_UVIS_OCC frame.
+
+ -- Added the TEXT_KERNEL_ID keyword to make version information
+ accessible to programs at runtime.
+
+ Version 2.3 -- March 9, 2000 -- Scott Turner
+
+ -- Updated the Euler angles for CASSINI_CIRS_FP1,
+ CASSINI_CIRS_FP3, and CASSINI_CIRS_FP4. Migrated them from
+ the prototype section into the CIRS Section of the FK.
+
+ Version 2.2 -- September 10, 1999 -- Scott Turner
+
+ -- Removed TKFRAME_[ID]_BORESIGHT keyword for all but the
+ antenna frames present. This information can now be found in
+ the instrument kernel with the keyword: INS[ID]_BORESIGHT.
+
+ -- Added a frame for the Stellar Reference Unit (SRU).
+
+ -- Added prototype frame entries for several instruments. The
+ transformations stored here for these frames are NOT for any
+ real calculations, and in some cases are not connected with
+ the actual instrument pointing at all. These frames will
+ migrate from the prototype section as the kernel evolves.
+
+ -- Changed CASSINI_SC_BUS to CASSINI_SC_COORD.
+
+ -- Changed the LGA frame name definitions to CASSINI_LGA1 and
+ CASSINI_LGA2 to accommodate simple translation to flight
+ software frame names.
+
+ -- Changed NAC and WAC ID codes from -82010 and -82020 to -82360
+ and -82361 respectively. This is to conform to the new ID
+ code scheme proposed by Jeff Boyer.
+
+ -- Altered the textual description of the spacecraft coordinate
+ system to conform with [8].
+
+ -- Added some text from [8] to the ISS_NAC frame description.
+
+ Version 2.1 -- July 14, 1999 -- Scott Turner
+
+ -- Fixed incorrect comments regarding the NAC images.
+
+ -- Fixed an improperly specified transformation for LGA2.
+
+ -- Added TKFRAME_[ID]_BORESIGHT keyword for the frames present.
+
+ Version 2.0 -- May 5, 1999 -- Scott Turner
+
+ -- Added ISS NAC and WAC instrument frames.
+
+ Version 1.0 -- May 14, 1998 -- Jeff Bytof
+
+ -- Initial Release.
+
+
+References
+----------------------------------------------------------
+
+ 1. ``C-kernel Required Reading''
+
+ 2. ``Kernel Pool Required Reading''
+
+ 3. ``Frames Required Reading''
+
+ 4. Cassini spacecraft blueprints. Provided by Kevin Tong, JPL.
+
+ 5. ``Cassini Science Instruments and Investigations'', Revised
+ Second Printing. Stephen J. Edberg.
+
+ 6. ``Determination of the ISS Boresights in Cassini Spacecraft
+ Coordinate System.'' Carolyn Porco and Vance Haemmerle.
+
+ 7. Email from Vance Haemmerle regarding WAC alignment.
+
+ 8. Cassini Document No. 699-406 ``Project Guidance Analysis
+ Book''
+
+ 9. CASPER CIRS I-kernel Version 3.2
+
+ 10. CIRS Fields-of-View PDF attached in an email from Stephen
+ Edberg to Diane Conner.
+
+ 11. Cassini Engineering Change Request #100078
+
+ 12. Cassini Engineering Change Request #100079
+
+ 13. CASPER VIMS I-kernel Version Version 4.2
+
+ 14. Email from Terry Averkamp regarding new RPWS frame entries.
+
+ 15. Email from Richard Achterberg regarding the CIRS frame
+ entries.
+
+ 16. Email from Vance Haemmerle regarding the Fomalhaut updates to
+ the ISS NAC and WAC alignments.
+
+ 17. Email from Jeff Boyer regarding radiator boresight
+ alignments, MIMI_CHEMS orientation, and RPWS orientation.
+
+ 18. Email from Sascha Kempf regarding CDA articulation.
+
+ 19. CASPER INMS I-kernel Version 5.0
+
+ 20. Email from Marcia Burton regarding the MAG field of views and
+ frame definitions.
+
+ 21. CASPER MAG I-kernel Version 6.0
+
+ 22. CASPER MIMI I-kernel Version 4.0
+
+ 23. CASPER RADAR I-kernel Version 2.2
+
+ 24. Email from Terry Averkamp discussing the new RPWS frame
+ entries.
+
+ 25. Email from Thomas Burk regarding the updates to CASSINI_XBAND
+ and CASSINI_KABAND frames that were the result of SCR 367.
+
+ 26. Email from Deborah Bass regarding a correct in the
+ CASSINI_INMS frame definition.
+
+ 27. Email from Donald Mitchell regarding a correction in the
+ CASSINI_MIMI_INCA frame definition.
+
+ 28. Email from Rick McCloskey regarding updates and additions to
+ the VIMS frame set.
+
+ 29. Email from Joshua Colwell regarding the CASSINI_UVIS_SOLAR
+ frame definition.
+
+ 30. Email from Joshua Colwell verifying the CASSINI_UVIS_SOLAR
+ frame definition.
+
+ 31. Email from Rick McCloskey confirming the CASSINI_VIMS_V,
+ CASSINI_VIMS_IR, CASSINI_VIMS_IR_SOL frame definitions.
+
+ 32. Email from Jeff Boyer providing CASSINI_SRU_RAD frame
+ definition.
+
+ 33. Email from Don Mitchell describing the CASSINI_MIMI_LEMMS1
+ and CASSINI_MIMI_LEMMS2 articulation characteristics.
+
+ 34. Email from Trina Ray describing updates for the CASSINI_XBAND
+ and CASSINI_KABAND frame definitions.
+
+ 35. Email from Diane Conner describing updates for the
+ CASSINI_XBAND and CASSINI_KABAND boresights.
+
+ 36. Cassini ECR 101029 - Change CASSINI_VIMS_RAD frame
+ definition.
+
+ 37. Cassini ECR 10325-B -- Change VIMS Sun Viewing Constraints
+ Flight Rule FF37B2.
+
+ 38. Email from Diane Conner regarding CASSINI_KABAND updated
+ boresight information.
+
+ 39. Page 28 from ECR 100515 listing updated alignment information
+ for CASSINI_CIRS detectors.
+
+ 40. Joshua Colwell's updated version 3.3.1 Cassini Spacecraft
+ Frame Definition kernel.
+
+ 41. Email from Rick McCloskey regarding the values in the body
+ vector table for CASSINI_VIMS_IR.
+
+ 42. Email from Rick McCloskey regarding the Euler angles for
+ CASSINI_VIMS_IR_SOL, the VIMS solar port.
+
+ 43. Email correction from Rick McCloskey regarding the Euler
+ angles for CASSINI_VIMS_IR_SOL.
+
+ 44. Email from Richard West regarding the CASSINI_RADAR_2 and
+ CASSINI_RADAR_4 Euler angles.
+
+ 45. Spreadsheet (gnumeric format) from Rick McCloskey regarding
+ the Euler angles for CASSINI_VIMS_IR_SOL.
+
+ 46. Email from Nicole Rappaport outlining needed changes to frame
+ and radio science instrument kernel due to project use of Ka
+ band data for X band pointing.
+
+ 47. Cassini ECR number 102788 -- Additional Frame and FOV
+ definitions to SPICE FK & IK Files for RSS
+
+ 48. Cassini R/SCR NO: 613 -- Update the Onboard XBAND body vector
+ table entries for GWE#3
+
+ 49. C44 - New CASSINI Rev / Sequence Change Request email
+ forwarded by Diane Conner
+
+ 50. Cassini R/SCR NO: 524 -- Update UVIS_EUV, UVIS_FUV and
+ UVIS_HSP boresight vectors. ( A. Jouchoux, 6/7/2002).
+
+ 51. Email from Josh Colwell indicating that the UVIS instrument Y
+ axis is co-aligned with the spacecraft -Z axis.
+
+ 52. Email from Diane Conner, 11/04/08, providing suggested FK and
+ IK changes per ECR-108546 ``Add UVIS_SOL_OFF vector to SPICE
+ Frame, Instrument, and Status Kernels''
+
+
+Contact Information
+----------------------------------------------------------
+
+ Direct questions, comments, or concerns about the contents of this kernel
+ to:
+
+ Boris Semenov, NAIF/JPL, (818)-354-8136, Boris.Semenov@jpl.nasa.gov
+
+
+Implementation Notes
+----------------------------------------------------------
+
+ This file is used by the SPICE system as follows: programs that make use of
+ this frame kernel must `load' the kernel, normally during program
+ initialization. The SPICELIB routine FURNSH loads a kernel file as shown
+ below:
+
+ FORTRAN: (SPICELIB)
+
+ CALL FURNSH ( frame_kernel_name )
+
+ C: (CSPICE)
+
+ furnsh_c ( frame_kernel_name );
+
+ IDL: (Icy)
+
+ cspice_furnsh, frame_kernel_name
+
+ MATLAB: (Mice)
+
+ cspice_furnsh( frame_kernel_name )
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+ Note: the keyword TKFRAME_[ID]_BORESIGHT defines the instrument or antenna
+ boresight axis in the instrument or antenna frame. In order for a program
+ or subroutine to extract data for this keyword, the SPICELIB routine GDPOOL
+ is used. See [2] for more details.
+
+
+Cassini Frames
+----------------------------------------------------------
+
+ The following Cassini frames are defined in this kernel file:
+
+ Frame Name Relative To Type NAIF ID
+ ======================= =================== ======= =======
+
+ AACS Body Frame:
+ ----------------
+ CASSINI_SC_COORD J2000 CK -82000
+ CASSINI_SRU-A CASSINI_SC_COORD FIXED -82001
+ CASSINI_SRU-B CASSINI_SC_COORD FIXED -82002
+ CASSINI_SRU-A_RAD CASSINI_SC_COORD FIXED -82008
+ CASSINI_SRU-B_RAD CASSINI_SC_COORD FIXED -82009
+
+ Antenna Frames (-821xx):
+ ------------------------
+ CASSINI_HGA CASSINI_SC_COORD FIXED -82101
+ CASSINI_LGA1 CASSINI_SC_COORD FIXED -82102
+ CASSINI_LGA2 CASSINI_SC_COORD FIXED -82103
+ CASSINI_XBAND CASSINI_SC_COORD FIXED -82104
+ CASSINI_KABAND CASSINI_SC_COORD FIXED -82105
+ CASSINI_KUBAND CASSINI_SC_COORD FIXED -82106
+ CASSINI_SBAND CASSINI_SC_COORD FIXED -82107
+ CASSINI_XBAND_TRUE CASSINI_SC_COORD FIXED -82108
+
+
+ ISS Frames (-8236x):
+ ------------------------
+ CASSINI_ISS_NAC CASSINI_SC_COORD FIXED -82360
+ CASSINI_ISS_WAC CASSINI_SC_COORD FIXED -82361
+ CASSINI_ISS_NAC_RAD CASSINI_SC_COORD FIXED -82368
+ CASSINI_ISS_WAC_RAD CASSINI_SC_COORD FIXED -82369
+
+ CIRS Frames (-8289x):
+ ------------------------
+ CASSINI_CIRS_FP1 CASSINI_CIRS_FPB FIXED -82890
+ CASSINI_CIRS_FP3 CASSINI_CIRS_FPB FIXED -82891
+ CASSINI_CIRS_FP4 CASSINI_CIRS_FPB FIXED -82892
+ CASSINI_CIRS_FPB CASSINI_SC_COORD FIXED -82893
+ CASSINI_CIRS_RAD CASSINI_SC_COORD FIXED -82898
+
+ UVIS Frames (-8284x):
+ ------------------------
+ CASSINI_UVIS_FUV CASSINI_SC_COORD FIXED -82840
+ CASSINI_UVIS_EUV CASSINI_SC_COORD FIXED -82842
+ CASSINI_UVIS_SOLAR CASSINI_SC_COORD FIXED -82843
+ CASSINI_UVIS_SOL_OFF CASSINI_SC_COORD FIXED -82849
+ CASSINI_UVIS_HSP CASSINI_SC_COORD FIXED -82844
+ CASSINI_UVIS_HDAC CASSINI_SC_COORD FIXED -82845
+
+ VIMS Frames (-8283x):
+ ------------------------
+ CASSINI_VIMS_V CASSINI_SC_COORD FIXED -82370
+ CASSINI_VIMS_IR CASSINI_SC_COORD FIXED -82371
+ CASSINI_VIMS_IR_SOL CASSINI_SC_COORD FIXED -82372
+ CASSINI_VIMS_RAD CASSINI_SC_COORD FIXED -82378
+
+ CAPS Frames (-8282x):
+ ------------------------
+ CASSINI_CAPS_BASE CASSINI_SC_COORD FIXED -82822
+ CASSINI_CAPS_ART CASSINI_CAPS_BASE CK -82821
+ CASSINI_CAPS CASSINI_CAPS_ART CK -82820
+ CASSINI_SC_COORD CK -82820
+
+ CDA Frames (-8279x):
+ ------------------------
+ CASSINI_CDA_BASE CASSINI_SC_COORD FIXED -82792
+ CASSINI_CDA_ART CASSINI_CDA_BASE CK -82971
+ CASSINI_CDA CASSINI_CDA_ART CK -82790
+ CASSINI_SC_COORD CK -82790
+
+ INMS Frames (-8274x):
+ ------------------------
+ CASSINI_INMS CASSINI_SC_COORD FIXED -82740
+
+ MAG Frames (-8235x):
+ ------------------------
+ CASSINI_MAG_PLUS CASSINI_SC_COORD FIXED -82350
+ CASSINI_MAG_MINUS CASSINI_SC_COORD FIXED -82351
+
+ MIMI Frames (-8276x):
+ ------------------------
+ CASSINI_MIMI_CHEMS CASSINI_SC_COORD FIXED -82760
+ CASSINI_MIMI_INCA CASSINI_SC_COORD FIXED -82761
+ CASSINI_MIMI_LEMMS_BASE CASSINI_SC_COORD FIXED -82765
+ CASSINI_MIMI_LEMMS_ART CASSINI_MIMI_LEMMS_BASE CK -82764
+ CASSINI_MIMI_LEMMS1 CASSINI_MIMI_LEMMS_ART CK -82762
+ CASSINI_SC_COORD CK -82762
+ CASSINI_MIMI_LEMMS2 CASSINI_MIMI_LEMMS_ART CK -82763
+ CASSINI_SC_COORD CK -82763
+
+ RADAR Frames (-8281x):
+ ------------------------
+ CASSINI_RADAR_1 CASSINI_SC_COORD FIXED -82810
+ CASSINI_RADAR_2 CASSINI_SC_COORD FIXED -82811
+ CASSINI_RADAR_3 CASSINI_SC_COORD FIXED -82812
+ CASSINI_RADAR_4 CASSINI_SC_COORD FIXED -82813
+ CASSINI_RADAR_5 CASSINI_SC_COORD FIXED -82814
+
+ RPWS Frames (-8273x):
+ ------------------------
+ CASSINI_RPWS CASSINI_SC_COORD FIXED -82730
+ CASSINI_RPWS_EXPLUS CASSINI_SC_COORD FIXED -82731
+ CASSINI_RPWS_EXMINUS CASSINI_SC_COORD FIXED -82732
+ CASSINI_RPWS_EZPLUS CASSINI_SC_COORD FIXED -82733
+ CASSINI_RPWS_LP CASSINI_SC_COORD FIXED -82734
+
+
+ where: the frame ID codes are built from the spacecraft ID code, the
+ instrument subsystem number, and the instrument number in a multiple
+ instrument subsystem. The numbers 8 and 9 are reserved for the radiators.
+ For example the ISS frame IDs are constructed as follows:
+
+ CASSINI_ISS_WAC ID = -82 36 1
+ | | |
+ | | |
+ SPACECRAFT ID CODE <-----+ | +----> INSTRUMENT NUMBER
+ |
+ V
+ INSTRUMENT SUBSYSTEM NUMBER
+
+
+Cassini Frames Hierarchy
+----------------------------------------------------------
+
+ Notes:
+
+ This diagram is subject to major revisions as this kernel evolves to suit
+ the needs of each instrument.
+
+ The articulating instrument frames have two paths back to the spacecraft
+ frame. The first is a direct path via a single C-kernel connecting the
+ instrument frame to the spacecraft frame. The second is one that utilizes a
+ fixed offset C-kernel to rotate the instrument frame into the articulation
+ frame, and then an articulation C-kernel and a base frame. For details see
+ the sections for CASSINI_CDA, CASSINI_CAPS, and CASSINI_MIMI_LEMMS.
+
+ The diagram below shows the Cassini frames hierarchy:
+
+
+ 'IAU_EARTH' (EARTH BODY FIXED)
+ |
+ |<--- pck
+ |
+ 'J2000' INERTIAL
+ |
+ |<--- ck
+ |
+ 'CASSINI_SC_COORD'
+ |
+ 'CASSINI_SRU-A'
+ |
+ 'CASSINI_SRU-B'
+ |
+ 'CASSINI_SRU-A_RAD'
+ |
+ 'CASSINI_SRU-B_RAD'
+ |
+ 'CASSINI_HGA'
+ |
+ 'CASSINI_XBAND'
+ |
+ 'CASSINI_KABAND'
+ | |
+ | 'CASSINI_XBAND_TRUE'
+ |
+ 'CASSINI_KUBAND'
+ |
+ 'CASSINI_SBAND'
+ |
+ 'CASSINI_LGA1'
+ |
+ 'CASSINI_LGA2'
+ |
+ 'CASSINI_ISS_NAC'
+ |
+ 'CASSINI_ISS_WAC'
+ |
+ 'CASSINI_ISS_NAC_RAD'
+ |
+ 'CASSINI_ISS_WAC_RAD'
+ |
+ 'CASSINI_CIRS_FPB'
+ | |
+ | 'CASSINI_CIRS_FP1'
+ | |
+ | 'CASSINI_CIRS_FP3'
+ | |
+ | 'CASSINI_CIRS_FP4'
+ |
+ 'CASSINI_CIRS_RAD'
+ |
+ 'CASSINI_UVIS_FUV'
+ |
+ 'CASSINI_UVIS_EUV'
+ |
+ 'CASSINI_UVIS_SOLAR'
+ |
+ 'CASSINI_UVIS_SOL_OFF'
+ |
+ 'CASSINI_UVIS_HSP'
+ |
+ 'CASSINI_UVIS_HDAC'
+ |
+ 'CASSINI_VIMS_V'
+ |
+ 'CASSINI_VIMS_IR'
+ |
+ 'CASSINI_VIMS_IR_SOL'
+ |
+ 'CASSINI_VIMS_RAD'
+ |
+ 'CASSINI_CAPS_BASE'
+ | |
+ | |<--- ck
+ | |
+ | 'CASSINI_CAPS_ART'
+ | |
+ | |<--- ck
+ | |
+ o------'CASSINI_CAPS'
+ | ^
+ | |
+ | + ck
+ |
+ 'CASSINI_CDA_BASE'
+ | |
+ | |<--- ck
+ | |
+ | 'CASSINI_CDA_ART'
+ | |
+ | |<--- ck
+ | |
+ o------'CASSINI_CDA'
+ | ^
+ | |
+ | + ck
+ |
+ 'CASSINI_INMS'
+ |
+ 'CASSINI_MAG_PLUS'
+ |
+ 'CASSINI_MAG_MINUS'
+ |
+ 'CASSINI_MIMI_CHEMS'
+ |
+ 'CASSINI_MIMI_INCA'
+ |
+ 'CASSINI_MIMI_LEMMS_BASE'
+ | |
+ | |<--- ck
+ | |
+ | 'CASSINI_MIMI_LEMMS_ART'
+ | |
+ | |<--- ck
+ | |
+ o------'CASSINI_MIMI_LEMMS1'
+ | ^ |
+ | | |
+ | + ck |
+ | |
+ o------'CASSINI_MIMI_LEMMS2'
+ | ^
+ | |
+ | + ck
+ |
+ 'CASSINI_RADAR_1'
+ |
+ 'CASSINI_RADAR_2'
+ |
+ 'CASSINI_RADAR_3'
+ |
+ 'CASSINI_RADAR_4'
+ |
+ 'CASSINI_RADAR_5'
+ |
+ 'CASSINI_RPWS'
+ |
+ 'CASSINI_RPWS_EXPLUS'
+ |
+ 'CASSINI_RPWS_EXMINUS'
+ |
+ 'CASSINI_RPWS_EZPLUS'
+ |
+ 'CASSINI_RPWS_LP'
+
+
+
+
+Spacecraft Frame
+----------------------------------------------------------
+
+ From [8]: (Note: The figures referenced below can not be reproduced here.
+ There is a diagram below that basically illustrates what is contained
+ there.)
+
+ ``The Stellar reference Unit (SRU) detector is a CCD. Its coordinate system
+ is defined according to the geometry of the detector. Figure 2.1.2a depicts
+ the SRU orientation and coordinates relative to the S/C coordinates. From
+ the ACS point of view, the S/C coordinate system is defined with respect to
+ the SRU coordinate frame, such that :
+
+ +X = +b (SRU boresight)
+
+ +Y = +v
+
+ +Z = -h
+
+ Therefore, by definition, there are no misalignments between the SRU and
+ the S/C coordinate frames.
+
+ The SRU coordinate system is defined by the pixel and line shift directions
+ defined in Figure 2.1.2b. These directions are represented by unit vectors
+ h and v respectively. Both h and v pass through the origin which is located
+ at the exact center of the 1024 x 1024 array. As indicated in Figure
+ 2.1.2b, the SRU boresight b passes through this point, is normal to both h
+ and v, and points outward through the optics towards the scene being
+ viewed.''
+
+ Stellar Reference Unit Frame:
+
+
+ Cassini Spacecraft
+
+ /\
+ ----------------------------------
+ \ /
+ \ / HGA
+ \ /
+ MAG Boom --------------------------
+ ... =================| |
+ | h |
+ \ ^ /
+ | | |
+ | | |
+ Y <-------| v <---o |
+ sc | b, X |
+ | sc |
+ | |
+ | |
+ | |
+ | |
+ ----------------------
+ / \
+ / \ Main Rocket Engine
+ ----------
+ |
+ |
+ |
+ V
+
+ Z
+ sc
+
+ where b and X point out of the screen or page.
+ sc
+
+
+ From [8]:
+
+ ``The spacecraft basebody coordinate system is a body fixed coordinate
+ system. It is a structural coordinate system defined when the spacecraft is
+ assembled. The primary geometrical and mass properties are fixed to this
+ system. The (X,Y,Z) coordinate system is not observable in space.
+
+ Referring to Figure 2.1.1, the origin of the spacecraft coordinate system
+ lies at the center of the field joint between the bus and the upper
+ equipment module (UEM) upper shell structure assembly [7]. This location is
+ defined by bolt holes A, D, and H (as shown on the Configuration lay out
+ 10129891, Figure 3). The Z-axis emanates from the origin and is
+ perpendicular to a plane generated by the mating surfaces of the bus at
+ bolt holes A, D, and H. The +Z-axis is on the propulsion module side of the
+ interface. The X-axis emanates from the origin and is parallel to the line
+ through the true centers of bolt holes A and H at the bus and the UEM upper
+ shell structure assembly interface. The -X-axis points towards the Huygens
+ probe. The Y-axis is mutually perpendicular to the X and Z axes, with the
+ +Y axis oriented along the magnetometer boom.''
+
+ Spacecraft bus attitude with respect to an inertial frame is provided by a
+ C kernel (see [1] for more information).
+
+ \begindata
+
+ FRAME_CASSINI_SC_COORD = -82000
+ FRAME_-82000_NAME = 'CASSINI_SC_COORD'
+ FRAME_-82000_CLASS = 3
+ FRAME_-82000_CLASS_ID = -82000
+ FRAME_-82000_CENTER = -82
+ CK_-82000_SCLK = -82
+ CK_-82000_SPK = -82
+
+ \begintext
+
+ The nominal definition of the Stellar Reference Unit-A frame is displayed
+ below. As described above and in [8], the boresight axis lies along the
+ spacecraft +X axis. The rotation matrix that takes vectors from the SRU-A
+ frame into the spacecraft frame is computed:
+
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ -90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_SRU-A = -82001
+ FRAME_-82001_NAME = 'CASSINI_SRU-A'
+ FRAME_-82001_CLASS = 4
+ FRAME_-82001_CLASS_ID = -82001
+ FRAME_-82001_CENTER = -82
+ TKFRAME_-82001_SPEC = 'ANGLES'
+ TKFRAME_-82001_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82001_ANGLES = ( 0.0, -90.0, 0.0 )
+ TKFRAME_-82001_AXES = ( 3, 2, 1 )
+ TKFRAME_-82001_UNITS = 'DEGREES'
+
+ \begintext
+
+ The nominal definition of the Stellar Reference Unit-B frame is displayed
+ below. Nominally SRU-A and SRU-B are aligned, so the boresight axis lies
+ along the spacecraft +X axis. The rotation matrix that takes vectors from
+ the SRU-B frame into the spacecraft frame is computed:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ -90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+
+ \begindata
+
+ FRAME_CASSINI_SRU-B = -82002
+ FRAME_-82002_NAME = 'CASSINI_SRU-B'
+ FRAME_-82002_CLASS = 4
+ FRAME_-82002_CLASS_ID = -82002
+ FRAME_-82002_CENTER = -82
+ TKFRAME_-82002_SPEC = 'ANGLES'
+ TKFRAME_-82002_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82002_ANGLES = ( 0.0, -90.0, 0.0 )
+ TKFRAME_-82002_AXES = ( 3, 2, 1 )
+ TKFRAME_-82002_UNITS = 'DEGREES'
+
+ \begintext
+
+ The nominal definition of the Stellar Reference Unit-A Radiator frame is
+ displayed below. As described in [32], the rotation matrix that takes
+ vectors from the SRU-A_RAD frame into the spacecraft frame is computed:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 180.0 ] [ -90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+
+ \begindata
+ FRAME_CASSINI_SRU-A_RAD = -82008
+ FRAME_-82008_NAME = 'CASSINI_SRU-A_RAD'
+ FRAME_-82008_CLASS = 4
+ FRAME_-82008_CLASS_ID = -82008
+ FRAME_-82008_CENTER = -82
+ TKFRAME_-82008_SPEC = 'ANGLES'
+ TKFRAME_-82008_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82008_ANGLES = ( 180.0, -90.0, 0.0 )
+ TKFRAME_-82008_AXES = ( 3, 1, 3 )
+ TKFRAME_-82008_UNITS = 'DEGREES'
+ \begintext
+
+ The nominal definition of the Stellar Reference Unit-B Radiator frame is
+ displayed below. As with the SRU-B frame, this is nominally the same frame
+ as SRU-A_RAD. The rotation matrix that takes vectors from the SRU-B_RAD
+ frame into the spacecraft frame is computed:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 180.0 ] [ -90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+ FRAME_CASSINI_SRU-B_RAD = -82009
+ FRAME_-82009_NAME = 'CASSINI_SRU-B_RAD'
+ FRAME_-82009_CLASS = 4
+ FRAME_-82009_CLASS_ID = -82009
+ FRAME_-82009_CENTER = -82
+ TKFRAME_-82009_SPEC = 'ANGLES'
+ TKFRAME_-82009_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82009_ANGLES = ( 180.0, -90.0, 0.0 )
+ TKFRAME_-82009_AXES = ( 3, 1, 3 )
+ TKFRAME_-82009_UNITS = 'DEGREES'
+ \begintext
+
+
+Antenna Frame Definitions
+----------------------------------------------------------
+
+ This section of the frames kernel defines the Cassini spacecraft antenna
+ frames. The ID codes associated with each of the frames are determined by
+ subtracting the three digit antenna code (101-103) from the DSN Cassini
+ spacecraft bus ID code (-82000).
+
+ Note the angles in the frame definitions are specified for the "from
+ antenna to (relative to) base frame" transformation.
+
+
+High Gain Antenna (HGA)
+
+ The high gain antenna points nominally along the spacecraft -Z axis. As
+ such the rotation matrix required that takes vectors represented in the
+ high gain antenna frame into the spacecraft frame is constructed as
+ follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ +180.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_HGA = -82101
+ FRAME_-82101_NAME = 'CASSINI_HGA'
+ FRAME_-82101_CLASS = 4
+ FRAME_-82101_CLASS_ID = -82101
+ FRAME_-82101_CENTER = -82
+ TKFRAME_-82101_SPEC = 'ANGLES'
+ TKFRAME_-82101_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82101_ANGLES = ( 0.0, 180.0, 0.0 )
+ TKFRAME_-82101_AXES = ( 3, 2, 1 )
+ TKFRAME_-82101_UNITS = 'DEGREES'
+ TKFRAME_-82101_BORESIGHT = ( 0.0, 0.0, 1.0 )
+
+ \begintext
+
+ The XBAND, XBAND_TRUE, KABAND, KUBAND, and SBAND frames are all frames
+ associated with the orbiter's High Gain Antenna. These names were chosen
+ for reasons of consistency with AACS, PDT, and sequencing software.
+
+
+High Gain Antenna X Band (XBAND)
+
+ The high gain antenna is capable of operating in several bands, each of
+ which may be calibrated and adjusted independently. The nominal frame
+ definition for the XBAND is displayed below:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ 180.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ FRAME_CASSINI_XBAND = -82104
+ FRAME_-82104_NAME = 'CASSINI_XBAND'
+ FRAME_-82104_CLASS = 4
+ FRAME_-82104_CLASS_ID = -82104
+ FRAME_-82104_CENTER = -82
+ TKFRAME_-82104_SPEC = 'ANGLES'
+ TKFRAME_-82104_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82104_ANGLES = ( 0.0, 0.0, 180.0 )
+ TKFRAME_-82104_AXES = ( 3, 2, 1 )
+ TKFRAME_-82104_UNITS = 'DEGREES'
+
+
+ From [25], the XBAND boresight has been adjusted to the following vector in
+ spacecraft coordinates:
+
+ [ 0.0005000 ]
+ XBAND Boresight Vector = [ 0.0004000 ]
+ [ -0.9999998 ]
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ By the methodology outlined above, this produces the following frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -128.659808 ] [ -179.963313 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ First Updated Frame Definition:
+
+ FRAME_CASSINI_XBAND = -82104
+ FRAME_-82104_NAME = 'CASSINI_XBAND'
+ FRAME_-82104_CLASS = 4
+ FRAME_-82104_CLASS_ID = -82104
+ FRAME_-82104_CENTER = -82
+ TKFRAME_-82104_SPEC = 'ANGLES'
+ TKFRAME_-82104_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82104_ANGLES = ( -128.659808, -179.963313, 0.0 )
+ TKFRAME_-82104_AXES = ( 3, 1, 3 )
+ TKFRAME_-82104_UNITS = 'DEGREES'
+
+
+ From [34], the XBAND boresight has been adjusted again to the following
+ vector in spacecraft coordinates:
+
+ [ 0.0005200 ]
+ XBAND Boresight Vector = [ 0.0005800 ]
+ [ -0.9999997 ]
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ By the methodology outlined above, this produces the following frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -138.12213046232 ] [ -179.95536809121 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+
+ Second Updated Frame Definition:
+
+ FRAME_CASSINI_XBAND = -82104
+ FRAME_-82104_NAME = 'CASSINI_XBAND'
+ FRAME_-82104_CLASS = 4
+ FRAME_-82104_CLASS_ID = -82104
+ FRAME_-82104_CENTER = -82
+ TKFRAME_-82104_SPEC = 'ANGLES'
+ TKFRAME_-82104_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82104_ANGLES = ( -138.12213046232,
+ -179.95536809121,
+ 0.0 )
+ TKFRAME_-82104_AXES = ( 3,
+ 1,
+ 3 )
+ TKFRAME_-82104_UNITS = 'DEGREES'
+
+
+ From [35], the XBAND boresight has been adjusted to the following vector in
+ spacecraft coordinates:
+
+ [ 0.0004839 ]
+ XBAND Boresight Vector = [ 0.0001745 ]
+ [ -0.9999999 ]
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ By the methodology outlined above, this produces the following frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -109.82989689352 ] [ -179.97052693372 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Third Updated Frame Definition:
+
+
+ FRAME_CASSINI_XBAND = -82104
+ FRAME_-82104_NAME = 'CASSINI_XBAND'
+ FRAME_-82104_CLASS = 4
+ FRAME_-82104_CLASS_ID = -82104
+ FRAME_-82104_CENTER = -82
+ TKFRAME_-82104_SPEC = 'ANGLES'
+ TKFRAME_-82104_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82104_ANGLES = ( -109.82989689352,
+ -179.97052693372,
+ 0.0 )
+ TKFRAME_-82104_AXES = ( 3,
+ 1,
+ 3 )
+ TKFRAME_-82104_UNITS = 'DEGREES'
+
+
+
+ ______________________________________________________________
+ ++++++++++++++++++++March 18, 2003++++++++++++++++++++++++++++
+
+ From [46], the XBAND boresight has been adjusted so that it is co-aligned
+ with the KABAND boresight. By defining the frame relative to
+ 'CASSINI_KABAND', the following frame definition is valid:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Y
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+
+ \begindata
+
+ FRAME_CASSINI_XBAND = -82104
+ FRAME_-82104_NAME = 'CASSINI_XBAND'
+ FRAME_-82104_CLASS = 4
+ FRAME_-82104_CLASS_ID = -82104
+ FRAME_-82104_CENTER = -82
+ TKFRAME_-82104_SPEC = 'ANGLES'
+ TKFRAME_-82104_RELATIVE = 'CASSINI_KABAND'
+ TKFRAME_-82104_ANGLES = ( 0.0,
+ 0.0,
+ 0.0 )
+ TKFRAME_-82104_AXES = ( 3,
+ 1,
+ 2 )
+ TKFRAME_-82104_UNITS = 'DEGREES'
+
+ \begintext
+
+
+High Gain Antenna X Band True (XBAND_TRUE)
+______________________________________________________________
+++++++++++++++++++++March 18, 2003++++++++++++++++++++++++++++
+
+ In order to preserve the original boresight information for the XBAND
+ antenna, a new frame is defined containing that information. The change
+ history is documented above under the XBAND frame.
+
+ From [35], the XBAND boresight has been adjusted to the following vector in
+ spacecraft coordinates:
+
+ [ 0.0004839 ]
+ XBAND Boresight Vector = [ 0.0001745 ]
+ [ -0.9999999 ]
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ By the methodology outlined above, this produces the following frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -109.82989689352 ] [ -179.97052693372 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_XBAND_TRUE = -82108
+ FRAME_-82108_NAME = 'CASSINI_XBAND_TRUE'
+ FRAME_-82108_CLASS = 4
+ FRAME_-82108_CLASS_ID = -82108
+ FRAME_-82108_CENTER = -82
+ TKFRAME_-82108_SPEC = 'ANGLES'
+ TKFRAME_-82108_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82108_ANGLES = ( -109.82989689352,
+ -179.97052693372,
+ 0.0 )
+ TKFRAME_-82108_AXES = ( 3,
+ 1,
+ 3 )
+ TKFRAME_-82108_UNITS = 'DEGREES'
+
+ \begintext
+
+
+High Gain Antenna KA Band (KABAND)
+
+ The high gain antenna is capable of operating in several bands, each of
+ which may be calibrated and adjusted independently. The nominal frame
+ definition for the KABAND is displayed below:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ 180.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ FRAME_CASSINI_KABAND = -82105
+ FRAME_-82105_NAME = 'CASSINI_KABAND'
+ FRAME_-82105_CLASS = 4
+ FRAME_-82105_CLASS_ID = -82105
+ FRAME_-82105_CENTER = -82
+ TKFRAME_-82105_SPEC = 'ANGLES'
+ TKFRAME_-82105_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82105_ANGLES = ( 0.0, 0.0, 180.0 )
+ TKFRAME_-82105_AXES = ( 3, 2, 1 )
+ TKFRAME_-82105_UNITS = 'DEGREES'
+
+
+ From [25], the KABAND boresight has been adjusted to the following vector
+ in spacecraft coordinates:
+
+ [ 0.0005000 ]
+ KABAND Boresight Vector = [ 0.0004000 ]
+ [ -0.9999998 ]
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ By the methodology outlined above, this produces the following frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -128.659808 ] [ -179.963313 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ First Updated Frame Definition:
+
+ FRAME_CASSINI_KABAND = -82105
+ FRAME_-82105_NAME = 'CASSINI_KABAND'
+ FRAME_-82105_CLASS = 4
+ FRAME_-82105_CLASS_ID = -82105
+ FRAME_-82105_CENTER = -82
+ TKFRAME_-82105_SPEC = 'ANGLES'
+ TKFRAME_-82105_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82105_ANGLES = ( -128.659808, -179.963313, 0.0 )
+ TKFRAME_-82105_AXES = ( 3, 1, 3 )
+ TKFRAME_-82105_UNITS = 'DEGREES'
+
+
+ From [34], the KABAND boresight has been adjusted again to the following
+ vector in spacecraft coordinates:
+
+ [ 0.0005300 ]
+ KABAND Boresight Vector = [ 0.0006600 ]
+ [ -0.9999996 ]
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ By the methodology outlined above, this produces the following frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -141.23448009520 ] [ -179.95150122158 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Second Updated Frame Definition:
+
+ FRAME_CASSINI_KABAND = -82105
+ FRAME_-82105_NAME = 'CASSINI_KABAND'
+ FRAME_-82105_CLASS = 4
+ FRAME_-82105_CLASS_ID = -82105
+ FRAME_-82105_CENTER = -82
+ TKFRAME_-82105_SPEC = 'ANGLES'
+ TKFRAME_-82105_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82105_ANGLES = ( -141.23448009520,
+ -179.95150122158,
+ 0.0 )
+ TKFRAME_-82105_AXES = ( 3,
+ 1,
+ 3 )
+ TKFRAME_-82105_UNITS = 'DEGREES'
+
+
+ From [35], the KABAND boresight has been adjusted to the following vector
+ in spacecraft coordinates:
+
+ [ 0.0004839 ]
+ KABAND Boresight Vector = [ 0.0001745 ]
+ [ -0.9999999 ]
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ By the methodology outlined above, this produces the following frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -109.82989689352 ] [ -179.97052693372 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+
+ FRAME_CASSINI_KABAND = -82105
+ FRAME_-82105_NAME = 'CASSINI_KABAND'
+ FRAME_-82105_CLASS = 4
+ FRAME_-82105_CLASS_ID = -82105
+ FRAME_-82105_CENTER = -82
+ TKFRAME_-82105_SPEC = 'ANGLES'
+ TKFRAME_-82105_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82105_ANGLES = ( -109.82989689352,
+ -179.97052693372,
+ 0.0 )
+ TKFRAME_-82105_AXES = ( 3,
+ 1,
+ 3 )
+ TKFRAME_-82105_UNITS = 'DEGREES'
+
+
+ From [38], the KABAND boresight has been adjusted to the following vector
+ in spacecraft coordinates:
+
+ [ 0.0005280 ]
+ KABAND Boresight Vector = [ 0.0003500 ]
+ [ -0.9999998 ]
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ By the methodology outlined above, this produces the following frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -123.53955356526 ] [ -179.96370485104 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+
+
+ FRAME_CASSINI_KABAND = -82105
+ FRAME_-82105_NAME = 'CASSINI_KABAND'
+ FRAME_-82105_CLASS = 4
+ FRAME_-82105_CLASS_ID = -82105
+ FRAME_-82105_CENTER = -82
+ TKFRAME_-82105_SPEC = 'ANGLES'
+ TKFRAME_-82105_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82105_ANGLES = ( -123.53955356526,
+ -179.96370485104,
+ 0.0 )
+ TKFRAME_-82105_AXES = ( 3,
+ 1,
+ 3 )
+ TKFRAME_-82105_UNITS = 'DEGREES'
+
+
+ ______________________________________________________________
+ ++++++++++++++++++++November 20, 2003++++++++++++++++++++++++++++
+
+ From [48], the KABAND boresight has been adjusted to the following vector
+ in spacecraft coordinates:
+
+ [ 0.0004273 ]
+ KABAND Boresight Vector = [ 0.0008606 ]
+ [ -0.9999995 ]
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ By the methodology outlined above, this produces the following frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -153.59495523828 ] [ -179.94494778906 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+
+
+ FRAME_CASSINI_KABAND = -82105
+ FRAME_-82105_NAME = 'CASSINI_KABAND'
+ FRAME_-82105_CLASS = 4
+ FRAME_-82105_CLASS_ID = -82105
+ FRAME_-82105_CENTER = -82
+ TKFRAME_-82105_SPEC = 'ANGLES'
+ TKFRAME_-82105_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82105_ANGLES = ( -153.59495523828,
+ -179.94494778906,
+ 0.0 )
+ TKFRAME_-82105_AXES = ( 3,
+ 1,
+ 3 )
+ TKFRAME_-82105_UNITS = 'DEGREES'
+
+
+
+ ______________________________________________________________
+ ++++++++++++++++++++May 10, 2004++++++++++++++++++++++++++++
+
+ From [49], the KABAND boresight has been adjusted to the following vector
+ in spacecraft coordinates:
+
+ [ 0.0004900 ]
+ KABAND Boresight Vector = [ 0.0004500 ]
+ [ -0.9999998 ]
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ By the methodology outlined above, this produces the following frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -132.56335175319 ] [ -179.96188215322 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_KABAND = -82105
+ FRAME_-82105_NAME = 'CASSINI_KABAND'
+ FRAME_-82105_CLASS = 4
+ FRAME_-82105_CLASS_ID = -82105
+ FRAME_-82105_CENTER = -82
+ TKFRAME_-82105_SPEC = 'ANGLES'
+ TKFRAME_-82105_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82105_ANGLES = ( -132.56335175319,
+ -179.96188215322,
+ 0.0 )
+ TKFRAME_-82105_AXES = ( 3,
+ 1,
+ 3 )
+ TKFRAME_-82105_UNITS = 'DEGREES'
+
+ \begintext
+
+
+High Gain Antenna KU Band (KUBAND)
+
+ The high gain antenna is capable of operating in several bands, each of
+ which may be calibrated and adjusted independently. The nominal frame
+ definition for the KUBAND is displayed below:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ 180.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_KUBAND = -82106
+ FRAME_-82106_NAME = 'CASSINI_KUBAND'
+ FRAME_-82106_CLASS = 4
+ FRAME_-82106_CLASS_ID = -82106
+ FRAME_-82106_CENTER = -82
+ TKFRAME_-82106_SPEC = 'ANGLES'
+ TKFRAME_-82106_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82106_ANGLES = ( 0.0, 0.0, 180.0 )
+ TKFRAME_-82106_AXES = ( 3, 2, 1 )
+ TKFRAME_-82106_UNITS = 'DEGREES'
+
+ \begintext
+
+
+High Gain Antenna S Band (SBAND)
+
+ The high gain antenna is capable of operating in several bands, each of
+ which may be calibrated and adjusted independently. The nominal frame
+ definition for the SBAND is displayed below:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ 180.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_SBAND = -82107
+ FRAME_-82107_NAME = 'CASSINI_SBAND'
+ FRAME_-82107_CLASS = 4
+ FRAME_-82107_CLASS_ID = -82107
+ FRAME_-82107_CENTER = -82
+ TKFRAME_-82107_SPEC = 'ANGLES'
+ TKFRAME_-82107_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82107_ANGLES = ( 0.0, 0.0, 180.0 )
+ TKFRAME_-82107_AXES = ( 3, 2, 1 )
+ TKFRAME_-82107_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Low Gain Antenna One (LGA1)
+
+ The first low gain antenna points nominally along the spacecraft -Z axis.
+ As such the rotation matrix required that takes vectors represented in the
+ first low gain antenna frame into the spacecraft frame is constructed as
+ follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ +180.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_LGA1 = -82102
+ FRAME_-82102_NAME = 'CASSINI_LGA1'
+ FRAME_-82102_CLASS = 4
+ FRAME_-82102_CLASS_ID = -82102
+ FRAME_-82102_CENTER = -82
+ TKFRAME_-82102_SPEC = 'ANGLES'
+ TKFRAME_-82102_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82102_ANGLES = ( 0.0, 180.0, 0.0 )
+ TKFRAME_-82102_AXES = ( 3, 2, 1 )
+ TKFRAME_-82102_UNITS = 'DEGREES'
+ TKFRAME_-82102_BORESIGHT = ( 0.0, 0.0, 1.0 )
+
+ \begintext
+
+
+Low Gain Antenna Two (LGA2)
+
+ The second low gain antenna points nominally along the spacecraft -X axis.
+ As such the rotation matrix required that takes vectors represented in the
+ second low gain antenna frame into the spacecraft frame is constructed as
+ follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_LGA2 = -82103
+ FRAME_-82103_NAME = 'CASSINI_LGA2'
+ FRAME_-82103_CLASS = 4
+ FRAME_-82103_CLASS_ID = -82103
+ FRAME_-82103_CENTER = -82
+ TKFRAME_-82103_SPEC = 'ANGLES'
+ TKFRAME_-82103_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82103_ANGLES = ( 0.0, 90.0, 0.0 )
+ TKFRAME_-82103_AXES = ( 3, 2, 1 )
+ TKFRAME_-82103_UNITS = 'DEGREES'
+ TKFRAME_-82103_BORESIGHT = ( 0.0, 0.0, 1.0 )
+
+ \begintext
+
+
+ISS Frames
+----------------------------------------------------------
+
+ The Narrow Angle Camera (NAC) and Wide Angle Camera (WAC) are mounted on
+ the remote sensing pallet on the +X side of the Cassini spacecraft, and
+ nominally directed along the -Y axis of the AACS body frame.
+
+ Note the angles in the frame definitions are specified for the "from
+ instrument to (relative to) base frame" transformation.
+
+
+Imaging Science Subsystem Narrow Angle Camera (ISS_NAC)
+
+ The ISS NAC points nominally along the spacecraft -Y axis. The following
+ frame definition encapsulates this nominal frame.
+
+ From [8]:
+
+ ``The Narrow Angle Camera (NAC) detector is a CCD. Its coordinate system is
+ defined according to the geometry of the detector. The narrow angle
+ coordinate system is defined in the same manner as the SRU coordinate
+ systems defined above and the four central pixels of center of the full CCD
+ are selected for the definition of the origin of the coordinate system.
+
+ The Narrow Angle Camera is the primary instrument on the Remote Sensing
+ Pallet (RSP). AACS is responsible for providing pointing knowledge of the
+ boresight vector of this instrument. All other RSP instruments use the
+ pointing provided to the NAC as their reference for determining their
+ pointing.''
+
+ Nominal Frame Definition:
+
+ FRAME_CASSINI_ISS_NAC = -82360
+ FRAME_-82360_NAME = 'CASSINI_ISS_NAC'
+ FRAME_-82360_CLASS = 4
+ FRAME_-82360_CLASS_ID = -82360
+ FRAME_-82360_CENTER = -82
+ TKFRAME_-82360_SPEC = 'ANGLES'
+ TKFRAME_-82360_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82360_ANGLES = ( -90.0, 0.0, 90.0 )
+ TKFRAME_-82360_AXES = ( 1, 2, 3 )
+ TKFRAME_-82360_UNITS = 'DEGREES'
+
+
+ [6] describes the inflight calibration of the ISS that was the result of
+ the CICLOPS (Cassini Imaging Central Laboratory for Operations) analysis of
+ 8 NAC images that were taken during ICO (Instrument Checkout). The rotation
+ matrix that takes vectors represented in the ISS_NAC frame into the
+ spacecraft frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -90.024236 ] [ -0.047029483 ] [ 89.892082 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ The angles were taken directly from [6].
+
+
+ FRAME_CASSINI_ISS_NAC = -82360
+ FRAME_-82360_NAME = 'CASSINI_ISS_NAC'
+ FRAME_-82360_CLASS = 4
+ FRAME_-82360_CLASS_ID = -82360
+ FRAME_-82360_CENTER = -82
+ TKFRAME_-82360_SPEC = 'ANGLES'
+ TKFRAME_-82360_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82360_ANGLES = ( -90.024236, -0.047029483, 89.892082 )
+ TKFRAME_-82360_AXES = ( 1, 2, 3 )
+ TKFRAME_-82360_UNITS = 'DEGREES'
+
+
+ From [10]:
+
+ ``The NAC boresight is not precisely aligned with the S/C -Y body vector.
+ Its alignment was determined during ICO-1 ISS observations of Spica, when
+ the spacecraft was using SRU-B for orientation determination. The alignment
+ parameters cited under Change Requested take into account the offset, as
+ determined by AACS, between SRU-A and SRU-B.''
+
+ [10] also describes a series of frame transformations that convert the
+ CASSINI_ISS_NAC frame into the CASSINI_SC_COORD frame, accounting for the
+ offset between SRU-A and SRU-B. This results in following frame definition:
+
+ The rotation matrix that takes vectors represented in the ISS_NAC frame
+ into the spacecraft frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -89.99231636 ] [ -0.03586589 ] [ 89.93339682 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+
+ FRAME_CASSINI_ISS_NAC = -82360
+ FRAME_-82360_NAME = 'CASSINI_ISS_NAC'
+ FRAME_-82360_CLASS = 4
+ FRAME_-82360_CLASS_ID = -82360
+ FRAME_-82360_CENTER = -82
+ TKFRAME_-82360_SPEC = 'ANGLES'
+ TKFRAME_-82360_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82360_ANGLES = (-89.99231636, -0.03586589, 89.93339682)
+ TKFRAME_-82360_AXES = ( 1, 2, 3 )
+ TKFRAME_-82360_UNITS = 'DEGREES'
+
+
+ From [16]:
+
+ ``The following results were obtained by using 3 long exposure Fomalhaut
+ NAC frames, each with 6 stars and using a 3 parameter fit (shift in line,
+ shift in sample and rotation about optic axis).''
+
+ AACS NAC boresight
+
+ X 0.0005760 +/- 0.0000018
+ Y -0.99999982 +/- 0.00000001
+ Z -0.0001710 +/- 0.0000016
+
+ The results of the Fomalhaut image calibrations produced the following
+ update to the ISS_NAC frame definition:
+
+ The rotation matrix that takes vectors represented in the ISS_NAC frame
+ into the spacecraft frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -90.009796 ] [ -0.03300 ] [ 89.9148 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_ISS_NAC = -82360
+ FRAME_-82360_NAME = 'CASSINI_ISS_NAC'
+ FRAME_-82360_CLASS = 4
+ FRAME_-82360_CLASS_ID = -82360
+ FRAME_-82360_CENTER = -82
+ TKFRAME_-82360_SPEC = 'ANGLES'
+ TKFRAME_-82360_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82360_ANGLES = (-90.009796, -0.03300, 89.9148 )
+ TKFRAME_-82360_AXES = ( 1, 2, 3 )
+ TKFRAME_-82360_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Imaging Science Subsystem Wide Angle Camera (ISS_WAC)
+
+ The ISS WAC points nominally along the spacecraft -Y axis. The following
+ frame definition encapsulates this nominal frame.
+
+ Nominal Frame Definition:
+
+ FRAME_CASSINI_ISS_WAC = -82361
+ FRAME_-82361_NAME = 'CASSINI_ISS_WAC'
+ FRAME_-82361_CLASS = 4
+ FRAME_-82361_CLASS_ID = -82361
+ FRAME_-82361_CENTER = -82
+ TKFRAME_-82361_SPEC = 'ANGLES'
+ TKFRAME_-82361_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82361_ANGLES = ( -90.0, 0.0, 90.0 )
+ TKFRAME_-82361_AXES = ( 1, 2, 3 )
+ TKFRAME_-82361_UNITS = 'DEGREES'
+
+
+ [6] describes the inflight calibration of ISS that was the result of the
+ CICLOPS (Cassini Imaging Central Laboratory for Operations) analysis of 36
+ WAC images taken during ICO (Instrument Checkout). At this time the images
+ taken were only sufficient to develop the location of the WAC's optical
+ axis. There are three determinations of this axes location in the
+ spacecraft frame. In [7] V.Haemmerle suggests that the 2-parameter fit
+ average coupled with nominal twist would be the safest assumption to
+ determine the frame transformation from ISS_WAC to the AACS body frame. The
+ rotation matrix that takes ISS_WAC vectors into the spacecraft frame would
+ be constructed as follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ +89.9116120 ] [ -90.00059931 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ These angles were computed using the assumption that the WAC optical axis
+ lies along the vector:
+
+ [ 0.00154266 ]
+ WAC Optical Axis Vector = [ -0.99999881 ]
+ [ -0.00001046 ]
+
+ in AACS body coordinates. Further we assume nominal twist, hence the first
+ rotation about Z is 0.0 degrees.
+
+
+ FRAME_CASSINI_ISS_WAC = -82361
+ FRAME_-82361_NAME = 'CASSINI_ISS_WAC'
+ FRAME_-82361_CLASS = 4
+ FRAME_-82361_CLASS_ID = -82361
+ FRAME_-82361_CENTER = -82
+ TKFRAME_-82361_SPEC = 'ANGLES'
+ TKFRAME_-82361_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82361_ANGLES = ( 89.9116120, -90.00059931, 0.0 )
+ TKFRAME_-82361_AXES = ( 3, 2, 3 )
+ TKFRAME_-82361_UNITS = 'DEGREES'
+
+
+ From [11]:
+
+ ``The WAC boresight is not precisely aligned with the S/C -Y body vector.
+ Its alignment was determined during ICO-1 ISS observations of Spica, when
+ the spacecraft was using SRU-B for orientation determination. The alignment
+ parameters cited under Change Request take into account the offset, as
+ determined by AACS, between SRU-A and SRU-B.''
+
+ Taking the boresight from the ECR ([11]):
+
+ [ 0.0013481161 ]
+ WAC Optical Axis Vector = [ -0.99999894 ]
+ [ 0.00054612156 ]
+
+ and assuming no twist, we derive the following angles:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ +89.9227586 ] [ -89.96870954 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ These angles were computed using the assumption that the WAC optical axis
+ lies along the vector listed above. Further we assume nominal twist, hence
+ the first rotation about Z is 0.0 degrees.
+
+
+ FRAME_CASSINI_ISS_WAC = -82361
+ FRAME_-82361_NAME = 'CASSINI_ISS_WAC'
+ FRAME_-82361_CLASS = 4
+ FRAME_-82361_CLASS_ID = -82361
+ FRAME_-82361_CENTER = -82
+ TKFRAME_-82361_SPEC = 'ANGLES'
+ TKFRAME_-82361_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82361_ANGLES = ( 89.9227586, -89.96870954, 0.0 )
+ TKFRAME_-82361_AXES = ( 3, 2, 3 )
+ TKFRAME_-82361_UNITS = 'DEGREES'
+
+
+ From [16]:
+
+ ``The following results were obtained by using 3 long exposure Fomalhaut
+ WAC frames, each using 12 stars near the center of frame and using a 3
+ parameter fit (shift in line, shift in sample and rotation about optic
+ axis).''
+
+ AACS WAC boresight
+
+ X 0.00121834 +/- 0.00000078
+ Y -0.99999923 +/- 0.00000001
+ Z 0.00025445 +/- 0.00000094
+
+ The results of the Fomalhaut image calibrations produced the following
+ update to the ISS_WAC frame definition:
+
+ The rotation matrix that takes vectors represented in the ISS_WAC frame
+ into the spacecraft frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -89.985421 ] [ -0.069806 ] [ 89.9736 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_ISS_WAC = -82361
+ FRAME_-82361_NAME = 'CASSINI_ISS_WAC'
+ FRAME_-82361_CLASS = 4
+ FRAME_-82361_CLASS_ID = -82361
+ FRAME_-82361_CENTER = -82
+ TKFRAME_-82361_SPEC = 'ANGLES'
+ TKFRAME_-82361_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82361_ANGLES = ( -89.985421, -0.069806, 89.9736 )
+ TKFRAME_-82361_AXES = ( 1, 2, 3 )
+ TKFRAME_-82361_UNITS = 'DEGREES'
+
+ \begintext
+
+
+ISS Radiators (ISS_NAC_RAD and ISS_WAC_RAD)
+
+ The ISS radiators are nominally oriented with their +Z axes directed down
+ the spacecraft +X axis.
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ As [17] indicates, both the ISS_NAC_RAD and ISS_WAC_RAD boresights are
+ nominally aligned with the +X axis in the spacecraft frame. By the
+ methodology outlined above, this produces the following frame definitions:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -90.0 ] [ -90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_ISS_NAC_RAD = -82368
+ FRAME_-82368_NAME = 'CASSINI_ISS_NAC_RAD'
+ FRAME_-82368_CLASS = 4
+ FRAME_-82368_CLASS_ID = -82368
+ FRAME_-82368_CENTER = -82
+ TKFRAME_-82368_SPEC = 'ANGLES'
+ TKFRAME_-82368_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82368_ANGLES = ( -90.0, -90.0, 0.0 )
+ TKFRAME_-82368_AXES = ( 3, 1, 3 )
+ TKFRAME_-82368_UNITS = 'DEGREES'
+
+ \begintext
+
+ Since the boresights are the same, both frame definitions are also the
+ same, thus we have:
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_ISS_WAC_RAD = -82369
+ FRAME_-82369_NAME = 'CASSINI_ISS_WAC_RAD'
+ FRAME_-82369_CLASS = 4
+ FRAME_-82369_CLASS_ID = -82369
+ FRAME_-82369_CENTER = -82
+ TKFRAME_-82369_SPEC = 'ANGLES'
+ TKFRAME_-82369_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82369_ANGLES = ( -90.0, -90.0, 0.0 )
+ TKFRAME_-82369_AXES = ( 3, 1, 3 )
+ TKFRAME_-82369_UNITS = 'DEGREES'
+
+ \begintext
+
+
+CIRS Frames
+----------------------------------------------------------
+
+ The Composite Infrared Spectrometer (CIRS) is mounted on the remote sensing
+ pallet on the +X side of the Cassini spacecraft, and nominally directed
+ along the -Y axis of the AACS body frame.
+
+ Note the angles in the frame definitions are specified for the "from
+ instrument to (relative to) base frame" transformation.
+
+
+Composite Infrared Spectrometer Focal Plane Boresight (CIRS_FPB)
+
+ The CIRS FPB points nominally along the spacecraft -Y axis. The rotation
+ matrix that takes vectors represented in the CIRS_FPB frame into the
+ spacecraft frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [-90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Y
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ The following frame definition encapsulates this nominal frame:
+
+ Nominal Frame Definition
+
+ FRAME_CASSINI_CIRS_FPB = -82893
+ FRAME_-82893_NAME = 'CASSINI_CIRS_FPB'
+ FRAME_-82893_CLASS = 4
+ FRAME_-82893_CLASS_ID = -82893
+ FRAME_-82893_CENTER = -82
+ TKFRAME_-82893_SPEC = 'ANGLES'
+ TKFRAME_-82893_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82893_ANGLES = ( 0.0, -90.0, 0.0 )
+ TKFRAME_-82893_AXES = ( 3, 1, 2 )
+ TKFRAME_-82893_UNITS = 'DEGREES'
+
+
+ ECR 100515 [39] included mounting alignment updates for all CIRS focal
+ planes. The optical boresight has moved from it's nominal configuration of
+ the -Y axis in the spacecraft frame 1.7 milliradians towards +X and -0.04
+ milliradians towards -Z. The rotation matrix that takes vectors represented
+ in the CIRS_FPB frame into the spacecraft frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ -90.002291831180 ] [ -0.09740282517 ]
+ [ ] [ ] [ ] [ ]
+ Z X Y
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_CIRS_FPB = -82893
+ FRAME_-82893_NAME = 'CASSINI_CIRS_FPB'
+ FRAME_-82893_CLASS = 4
+ FRAME_-82893_CLASS_ID = -82893
+ FRAME_-82893_CENTER = -82
+ TKFRAME_-82893_SPEC = 'ANGLES'
+ TKFRAME_-82893_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82893_ANGLES = (
+ 0.0
+ -90.0022918311805233
+ -0.097402825172240,
+ )
+ TKFRAME_-82893_AXES = ( 3, 1, 2 )
+
+ TKFRAME_-82893_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Composite Infrared Spectrometer Focal Plane #1 (CIRS_FP1)
+
+ The CIRS FP1 points nominally along the spacecraft -Y axis. The following
+ frame definition encapsulates this nominal frame.
+
+ Nominal Frame Definition:
+
+ FRAME_CASSINI_CIRS_FP1 = -82890
+ FRAME_-82890_NAME = 'CASSINI_CIRS_FP1'
+ FRAME_-82890_CLASS = 4
+ FRAME_-82890_CLASS_ID = -82890
+ FRAME_-82890_CENTER = -82
+ TKFRAME_-82890_SPEC = 'ANGLES'
+ TKFRAME_-82890_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82890_ANGLES = ( -90.0, 0.0, 90.0 )
+ TKFRAME_-82890_AXES = ( 1, 2, 3 )
+ TKFRAME_-82890_UNITS = 'DEGREES'
+
+
+ [9] and [10] describe the most up to date values the orientation of the
+ CIRS focal planes. The rotation matrix that takes vectors represented in
+ the CIRS_FP1 frame into the CIRS_FPB frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ 0.23319382 ]
+ [ ] [ ] [ ] [ ]
+ Z X Y
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ The angles were computed from [10].
+
+
+ FRAME_CASSINI_CIRS_FP1 = -82890
+ FRAME_-82890_NAME = 'CASSINI_CIRS_FP1'
+ FRAME_-82890_CLASS = 4
+ FRAME_-82890_CLASS_ID = -82890
+ FRAME_-82890_CENTER = -82
+ TKFRAME_-82890_SPEC = 'ANGLES'
+ TKFRAME_-82890_RELATIVE = 'CASSINI_CIRS_FPB'
+ TKFRAME_-82890_ANGLES = ( 0.0, 0.0, -0.23319382 )
+ TKFRAME_-82890_AXES = ( 3, 1, 2 )
+ TKFRAME_-82890_UNITS = 'DEGREES'
+
+
+ [39] introduces new offsets for the FP1 from the optical boresight (FPB).
+ They are: 3.98 milliradians towards +X in the spacecraft frame and 0.07
+ milliradians towards +Z in the spacecraft frame. These offsets result in
+ the following rotation matrix:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0040107045659 ] [ -0.22803720246 ]
+ [ ] [ ] [ ] [ ]
+ Z X Y
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_CIRS_FP1 = -82890
+ FRAME_-82890_NAME = 'CASSINI_CIRS_FP1'
+ FRAME_-82890_CLASS = 4
+ FRAME_-82890_CLASS_ID = -82890
+ FRAME_-82890_CENTER = -82
+ TKFRAME_-82890_SPEC = 'ANGLES'
+ TKFRAME_-82890_RELATIVE = 'CASSINI_CIRS_FPB'
+ TKFRAME_-82890_ANGLES = (
+ 0.0,
+ 4.0107045659158E-03,
+ -2.2803720246207E-01
+ )
+ TKFRAME_-82890_AXES = ( 3, 1, 2 )
+ TKFRAME_-82890_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Composite Infrared Spectrometer Focal Plane #3 (CIRS_FP3)
+
+ The CIRS FP3 points nominally along the spacecraft -Y axis. The following
+ frame definition encapsulates this nominal frame.
+
+ Nominal Frame Definition:
+
+ FRAME_CASSINI_CIRS_FP3 = -82891
+ FRAME_-82891_NAME = 'CASSINI_CIRS_FP3'
+ FRAME_-82891_CLASS = 4
+ FRAME_-82891_CLASS_ID = -82891
+ FRAME_-82891_CENTER = -82
+ TKFRAME_-82891_SPEC = 'ANGLES'
+ TKFRAME_-82891_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82891_ANGLES = ( -90.0, 0.0, 90.0 )
+ TKFRAME_-82891_AXES = ( 1, 2, 3 )
+ TKFRAME_-82891_UNITS = 'DEGREES'
+
+
+ [9] and [10] describe the most up to date values the orientation of the
+ CIRS focal planes. The rotation matrix that takes vectors represented in
+ the CIRS_FP3 frame into the CIRS_FPB frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ 0.002549662 ]
+ [ ] [ ] [ ] [ ]
+ Z X Y
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ The angles were computed from [10] with updates from [15].
+
+
+ FRAME_CASSINI_CIRS_FP3 = -82891
+ FRAME_-82891_NAME = 'CASSINI_CIRS_FP3'
+ FRAME_-82891_CLASS = 4
+ FRAME_-82891_CLASS_ID = -82891
+ FRAME_-82891_CENTER = -82
+ TKFRAME_-82891_SPEC = 'ANGLES'
+ TKFRAME_-82891_RELATIVE = 'CASSINI_CIRS_FPB'
+ TKFRAME_-82891_ANGLES = ( 0.0, 0.0, 0.02549662 )
+ TKFRAME_-82891_AXES = ( 3, 1, 2 )
+ TKFRAME_-82891_UNITS = 'DEGREES'
+
+
+ [39] includes an update to the offset of CASSINI_CIRS_FP3 from
+ CASSINI_CIRS_FPB. Instead of 0.445 milliradians, the new value is 0.47
+ milliradians of separation between the optical boresight and focal plane
+ 3's boresight. The rotation matrix that takes vectors represented in the
+ CIRS_FP3 frame into the CIRS_FPB frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ 0.002692902 ]
+ [ ] [ ] [ ] [ ]
+ Z X Y
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_CIRS_FP3 = -82891
+ FRAME_-82891_NAME = 'CASSINI_CIRS_FP3'
+ FRAME_-82891_CLASS = 4
+ FRAME_-82891_CLASS_ID = -82891
+ FRAME_-82891_CENTER = -82
+ TKFRAME_-82891_SPEC = 'ANGLES'
+ TKFRAME_-82891_RELATIVE = 'CASSINI_CIRS_FPB'
+ TKFRAME_-82891_ANGLES = ( 0.0, 0.0, 2.6929016371149E-02 )
+ TKFRAME_-82891_AXES = ( 3, 1, 2 )
+ TKFRAME_-82891_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Composite Infrared Spectrometer Focal Plane #4 (CIRS_FP4)
+
+ The CIRS FP4 points nominally along the spacecraft -Y axis. The following
+ frame definition encapsulates this nominal frame.
+
+ Nominal Frame Definition:
+
+ FRAME_CASSINI_CIRS_FP4 = -82892
+ FRAME_-82892_NAME = 'CASSINI_CIRS_FP4'
+ FRAME_-82892_CLASS = 4
+ FRAME_-82892_CLASS_ID = -82892
+ FRAME_-82892_CENTER = -82
+ TKFRAME_-82892_SPEC = 'ANGLES'
+ TKFRAME_-82892_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82892_ANGLES = ( -90.0, 0.0, 90.0 )
+ TKFRAME_-82892_AXES = ( 1, 2, 3 )
+ TKFRAME_-82892_UNITS = 'DEGREES'
+
+
+ [9] and [10] describe the most up to date values the orientation of the
+ CIRS focal planes. The rotation matrix that takes vectors represented in
+ the CIRS_FP4 frame into the CIRS_FPB frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ -0.02549662 ]
+ [ ] [ ] [ ] [ ]
+ Z X Y
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ The angles were taken directly from [10] with updates from [15].
+
+
+ FRAME_CASSINI_CIRS_FP4 = -82892
+ FRAME_-82892_NAME = 'CASSINI_CIRS_FP4'
+ FRAME_-82892_CLASS = 4
+ FRAME_-82892_CLASS_ID = -82892
+ FRAME_-82892_CENTER = -82
+ TKFRAME_-82892_SPEC = 'ANGLES'
+ TKFRAME_-82892_RELATIVE = 'CASSINI_CIRS_FPB'
+ TKFRAME_-82892_ANGLES = ( 0.0, 0.0, -0.02549662 )
+ TKFRAME_-82892_AXES = ( 3, 1, 2 )
+ TKFRAME_-82892_UNITS = 'DEGREES'
+
+
+ [39] includes an update to the offset of CASSINI_CIRS_FP4 from
+ CASSINI_CIRS_FPB. Instead of 0.445 milliradians, the new value is 0.47
+ milliradians of separation between the optical boresight and focal plane
+ 4's boresight. The rotation matrix that takes vectors represented in the
+ CIRS_FP4 frame into the CIRS_FPB frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ -0.002692902 ]
+ [ ] [ ] [ ] [ ]
+ Z X Y
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_CIRS_FP4 = -82892
+ FRAME_-82892_NAME = 'CASSINI_CIRS_FP4'
+ FRAME_-82892_CLASS = 4
+ FRAME_-82892_CLASS_ID = -82892
+ FRAME_-82892_CENTER = -82
+ TKFRAME_-82892_SPEC = 'ANGLES'
+ TKFRAME_-82892_RELATIVE = 'CASSINI_CIRS_FPB'
+ TKFRAME_-82892_ANGLES = ( 0.0, 0.0, -2.6929016371149E-02 )
+ TKFRAME_-82892_AXES = ( 3, 1, 2 )
+ TKFRAME_-82892_UNITS = 'DEGREES'
+
+ \begintext
+
+
+CIRS Radiator (CIRS_RAD)
+
+ The CIRS radiator is nominally oriented with its +Z axis directed down the
+ spacecraft +X axis.
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ As [17] indicates, the CIRS_RAD boresight is nominally aligned with the +X
+ axis in the spacecraft frame. By the methodology outlined above, this
+ produces the following frame definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -90.0 ] [ -90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_CIRS_RAD = -82898
+ FRAME_-82898_NAME = 'CASSINI_CIRS_RAD'
+ FRAME_-82898_CLASS = 4
+ FRAME_-82898_CLASS_ID = -82898
+ FRAME_-82898_CENTER = -82
+ TKFRAME_-82898_SPEC = 'ANGLES'
+ TKFRAME_-82898_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82898_ANGLES = ( -90.0, -90.0, 0.0 )
+ TKFRAME_-82898_AXES = ( 3, 1, 3 )
+ TKFRAME_-82898_UNITS = 'DEGREES'
+
+ \begintext
+
+
+UVIS Frames
+----------------------------------------------------------
+
+ The Ultraviolet Imaging Spectrograph (UVIS) is mounted on the remote
+ sensing pallet on the +X side of the Cassini spacecraft, and nominally
+ directed along the -Y axis of the AACS body frame.
+
+ Note the angles in the frame definitions are specified for the "from
+ instrument to (relative to) base frame" transformation.
+
+
+Ultraviolet Imaging Spectrograph Far Ultraviolet Spectrograph (UVIS_FUV)
+
+ An examination of [5] reveals that UVIS_FUV points nominally along the
+ spacecraft -Y axis. The rotation matrix that takes vectors represented in
+ the UVIS_FUV frame into the spacecraft frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ -90.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ The following frame definition describes this nominal frame:
+
+ Nominal Frame Definition:
+
+ FRAME_CASSINI_UVIS_FUV = -82840
+ FRAME_-82840_NAME = 'CASSINI_UVIS_FUV'
+ FRAME_-82840_CLASS = 4
+ FRAME_-82840_CLASS_ID = -82840
+ FRAME_-82840_CENTER = -82
+ TKFRAME_-82840_SPEC = 'ANGLES'
+ TKFRAME_-82840_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82840_ANGLES = ( 0.0, 0.0, -90.0 )
+ TKFRAME_-82840_AXES = ( 3, 2, 1 )
+ TKFRAME_-82840_UNITS = 'DEGREES'
+
+
+ From [40], the UVIS_FUV boresight has been adjusted to the following vector
+ in spacecraft coordinates:
+
+ [ 0.0002 ]
+ UVIS_FUV Boresight Vector = [ -0.99999998 ]
+ [ 0.0001 ]
+
+ This leads to the following rotation matrix that takes vectors represented
+ in the UVIS_FUV frame into the spacecraft frame:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -89.9999 ] [ -0.011459 ] [ 0.005729 ]
+ [ ] [ ] [ ] [ ]
+ X Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+
+ FRAME_CASSINI_UVIS_FUV = -82840
+ FRAME_-82840_NAME = 'CASSINI_UVIS_FUV'
+ FRAME_-82840_CLASS = 4
+ FRAME_-82840_CLASS_ID = -82840
+ FRAME_-82840_CENTER = -82
+ TKFRAME_-82840_SPEC = 'ANGLES'
+ TKFRAME_-82840_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82840_ANGLES = (
+ -89.999999,
+ -0.01145916,
+ 0.005729578
+ )
+ TKFRAME_-82840_AXES = ( 1, 2, 1 )
+ TKFRAME_-82840_UNITS = 'DEGREES'
+
+
+ ______________________________________________________________
+ ++++++++++++++++++++October 14, 2004++++++++++++++++++++++++++++
+
+ From [50], the UVIS_FUV boresight has been adjusted to the following vector
+ in spacecraft coordinates:
+
+ [ 0.0002000 ]
+ UVIS_FUV Boresight Vector = [ -0.9999999 ]
+ [ 0.0001000 ]
+
+ In addition, from [51] the instrument Y axis is specified to be parallel to
+ the spacecraft -Z axis. This leads to the following rotation matrix that
+ takes vectors represented in the UVIS_FUV frame into the spacecraft frame:
+
+ [ ] [ ] [ ] [ ]
+ [ROT] = [ -90.00000000000] [+179.98854084310] [+179.99427042161]
+ [ ] [ ] [ ] [ ]
+ X Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_UVIS_FUV = -82840
+ FRAME_-82840_NAME = 'CASSINI_UVIS_FUV'
+ FRAME_-82840_CLASS = 4
+ FRAME_-82840_CLASS_ID = -82840
+ FRAME_-82840_CENTER = -82
+ TKFRAME_-82840_SPEC = 'ANGLES'
+ TKFRAME_-82840_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82840_ANGLES = (
+ -90.00000000000,
+ +179.98854084310 ,
+ +179.99427042161
+ )
+ TKFRAME_-82840_AXES = ( 1, 2, 1 )
+ TKFRAME_-82840_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Ultraviolet Imaging Spectrograph Extreme Ultraviolet Spectrograph (UVIS_EUV)
+
+ An examination of [5] reveals that the UVIS_EUV points nominally along the
+ spacecraft -Y axis. The rotation matrix that takes vectors represented in
+ the UVIS_EUV frame into the spacecraft frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ -90.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ The following frame definition describes this nominal frame:
+
+ Nominal Frame Definition:
+
+ FRAME_CASSINI_UVIS_EUV = -82842
+ FRAME_-82842_NAME = 'CASSINI_UVIS_EUV'
+ FRAME_-82842_CLASS = 4
+ FRAME_-82842_CLASS_ID = -82842
+ FRAME_-82842_CENTER = -82
+ TKFRAME_-82842_SPEC = 'ANGLES'
+ TKFRAME_-82842_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82842_ANGLES = ( 0.0, 0.0, -90.0 )
+ TKFRAME_-82842_AXES = ( 3, 2, 1 )
+ TKFRAME_-82842_UNITS = 'DEGREES'
+
+
+ From [40], the UVIS_EUV boresight has been adjusted to the following vector
+ in spacecraft coordinates:
+
+ [ 0.0012 ]
+ UVIS_EUV Boresight Vector = [ -0.99999843 ]
+ [ 0.0013 ]
+
+ This leads to the following rotation matrix that takes vectors represented
+ in the UVIS_EUV frame into the spacecraft frame:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -89.8984 ] [ -0.068755 ] [ -0.02704 ]
+ [ ] [ ] [ ] [ ]
+ X Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+
+ FRAME_CASSINI_UVIS_EUV = -82842
+ FRAME_-82842_NAME = 'CASSINI_UVIS_EUV'
+ FRAME_-82842_CLASS = 4
+ FRAME_-82842_CLASS_ID = -82842
+ FRAME_-82842_CENTER = -82
+ TKFRAME_-82842_SPEC = 'ANGLES'
+ TKFRAME_-82842_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82842_ANGLES = (
+ -89.8984716,
+ -0.068755,
+ -0.027044457
+ )
+ TKFRAME_-82842_AXES = ( 1, 2, 1 )
+ TKFRAME_-82842_UNITS = 'DEGREES'
+
+
+ ______________________________________________________________
+ ++++++++++++++++++++October 14, 2004++++++++++++++++++++++++++++
+
+ From [50], the UVIS_EUV boresight has been adjusted to the following vector
+ in spacecraft coordinates:
+
+ [ 0.0011999 ]
+ UVIS_EUV Boresight Vector = [ -0.9999984 ]
+ [ 0.0012999 ]
+
+ In addition, from [51] the instrument Y axis is specified to be parallel to
+ the spacecraft -Z axis. This leads to the following rotation matrix that
+ takes vectors represented in the UVIS_EUV frame into the spacecraft frame:
+
+ [ ] [ ] [ ] [ ]
+ [ROT] = [-90.00000000000] [+179.93125071716] [+179.92552119261]
+ [ ] [ ] [ ] [ ]
+ X Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_UVIS_EUV = -82842
+ FRAME_-82842_NAME = 'CASSINI_UVIS_EUV'
+ FRAME_-82842_CLASS = 4
+ FRAME_-82842_CLASS_ID = -82842
+ FRAME_-82842_CENTER = -82
+ TKFRAME_-82842_SPEC = 'ANGLES'
+ TKFRAME_-82842_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82842_ANGLES = (
+ -90.00000000000,
+ +179.93125071716 ,
+ +179.92552119261
+ )
+ TKFRAME_-82842_AXES = ( 1, 2, 1 )
+ TKFRAME_-82842_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Ultraviolet Imaging Spectrograph Solar Occultation Port (UVIS_SOLAR)
+
+ [29] and [30] indicate that the UVIS solar occultation port points
+ nominally 20 degrees offset from the nominal UVIS boresights in the -Y
+ direction of the nominal instrument frames. The rotation matrix that takes
+ vectors represented in the CASSINI_UVIS_SOLAR frame into the
+ CASSINI_SC_COORD frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ -110.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_UVIS_SOLAR = -82843
+ FRAME_-82843_NAME = 'CASSINI_UVIS_SOLAR'
+ FRAME_-82843_CLASS = 4
+ FRAME_-82843_CLASS_ID = -82843
+ FRAME_-82843_CENTER = -82
+ TKFRAME_-82843_SPEC = 'ANGLES'
+ TKFRAME_-82843_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82843_ANGLES = ( 0.0, 0.0, -110.0 )
+ TKFRAME_-82843_AXES = ( 3, 2, 1 )
+ TKFRAME_-82843_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Ultraviolet Imaging Spectrograph Solar Occultation Port with Offset
+(UVIS_SOL_OFF)
+
+ In reality the UVIS solar occultation port boresight has an offset from its
+ nominal viewing direction. For convenience of the ground system tools,
+ instead of incorporating this offset into the definition of the
+ CASSINI_UVIS_SOLAR frame, this FK defines a separate frame,
+ CASSINI_UVIS_SOL_OFF (ID -82849), aligned with the actual view direction.
+ The rotation matrix that takes vectors represented in the
+ CASSINI_UVIS_SOL_OFF frame into the CASSINI_SC_COORD frame is (from [52]):
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -110.0 ] [ 0.0 ] [ -0.11459 ]
+ [ ] [ ] [ ] [ ]
+ X Z Y
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_UVIS_SOL_OFF = -82849
+ FRAME_-82849_NAME = 'CASSINI_UVIS_SOL_OFF'
+ FRAME_-82849_CLASS = 4
+ FRAME_-82849_CLASS_ID = -82849
+ FRAME_-82849_CENTER = -82
+ TKFRAME_-82849_SPEC = 'ANGLES'
+ TKFRAME_-82849_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82849_ANGLES = ( -110.0, 0.0, -0.11459 )
+ TKFRAME_-82849_AXES = ( 1, 3, 2 )
+ TKFRAME_-82849_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Ultraviolet Imaging Spectrograph High Speed Photometer (UVIS_HSP)
+
+ An examination of [5] reveals that the UVIS_HSP points nominally along the
+ spacecraft -Y axis. The rotation matrix that takes vectors represented in
+ the UVIS_HSP frame into the spacecraft frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ -90.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ The following frame definition describes this nominal frame:
+
+ Nominal Frame Definition:
+
+ FRAME_CASSINI_UVIS_HSP = -82844
+ FRAME_-82844_NAME = 'CASSINI_UVIS_HSP'
+ FRAME_-82844_CLASS = 4
+ FRAME_-82844_CLASS_ID = -82844
+ FRAME_-82844_CENTER = -82
+ TKFRAME_-82844_SPEC = 'ANGLES'
+ TKFRAME_-82844_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82844_ANGLES = ( 0.0, 0.0, -90.0 )
+ TKFRAME_-82844_AXES = ( 3, 2, 1 )
+ TKFRAME_-82844_UNITS = 'DEGREES'
+
+
+ From [40], the UVIS_HSP boresight has been adjusted to the following vector
+ in spacecraft coordinates:
+
+ [ 0.0012 ]
+ UVIS_HSP Boresight Vector = [ -0.99999856 ]
+ [ -0.0012 ]
+
+ This leads to the following rotation matrix that takes vectors represented
+ in the UVIS_HSP frame into the spacecraft frame:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -89.9028 ] [ -0.068755 ] [ -0.16599 ]
+ [ ] [ ] [ ] [ ]
+ X Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+
+ FRAME_CASSINI_UVIS_HSP = -82844
+ FRAME_-82844_NAME = 'CASSINI_UVIS_HSP'
+ FRAME_-82844_CLASS = 4
+ FRAME_-82844_CLASS_ID = -82844
+ FRAME_-82844_CENTER = -82
+ TKFRAME_-82844_SPEC = 'ANGLES'
+ TKFRAME_-82844_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82844_ANGLES = (
+ -89.9027658,
+ -0.068755,
+ -0.1659861
+ )
+ TKFRAME_-82844_AXES = ( 1, 2, 1 )
+ TKFRAME_-82844_UNITS = 'DEGREES'
+
+
+ ______________________________________________________________
+ ++++++++++++++++++++October 14, 2004++++++++++++++++++++++++++++
+
+ From [50], the UVIS_HSP boresight has been adjusted to the following vector
+ in spacecraft coordinates:
+
+ [ 0.0011999 ]
+ UVIS_HSP Boresight Vector = [ -0.9999985 ]
+ [ -0.0011999 ]
+
+ In addition, from [51] the instrument Y axis is specified to be parallel to
+ the spacecraft -Z axis. This leads to the following rotation matrix that
+ takes vectors represented in the UVIS_HSP frame into the spacecraft frame:
+
+ [ ] [ ] [ ] [ ]
+ [ROT] = [- 90.00000000000] [+179.93125072403] [-179.93125077352]
+ [ ] [ ] [ ] [ ]
+ X Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_UVIS_HSP = -82844
+ FRAME_-82844_NAME = 'CASSINI_UVIS_HSP'
+ FRAME_-82844_CLASS = 4
+ FRAME_-82844_CLASS_ID = -82844
+ FRAME_-82844_CENTER = -82
+ TKFRAME_-82844_SPEC = 'ANGLES'
+ TKFRAME_-82844_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82844_ANGLES = (
+ -90.00000000000,
+ +179.93125072403,
+ -179.93125077352
+ )
+ TKFRAME_-82844_AXES = ( 1, 2, 1 )
+ TKFRAME_-82844_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Ultraviolet Imaging Spectrograph Hydrogen - Deuterium Absorption Cell
+(UVIS_HDAC)
+
+ An examination of [5] reveals that the UVIS_HDAC points nominally along the
+ spacecraft -Y axis. The rotation matrix that takes vectors represented in
+ the UVIS_HSP frame into the spacecraft frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ -90.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ The following frame definition describes this nominal frame:
+
+ \begindata
+
+ FRAME_CASSINI_UVIS_HDAC = -82845
+ FRAME_-82845_NAME = 'CASSINI_UVIS_HDAC'
+ FRAME_-82845_CLASS = 4
+ FRAME_-82845_CLASS_ID = -82845
+ FRAME_-82845_CENTER = -82
+ TKFRAME_-82845_SPEC = 'ANGLES'
+ TKFRAME_-82845_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82845_ANGLES = ( 0.0, 0.0, -90.0 )
+ TKFRAME_-82845_AXES = ( 3, 2, 1 )
+ TKFRAME_-82845_UNITS = 'DEGREES'
+
+ \begintext
+
+
+VIMS Frames
+----------------------------------------------------------
+
+ The Visible and Infrared Mapping Spectrometer is mounted on the remote
+ sensing pallet on the +X side of the Cassini spacecraft, and nominally
+ directed along the -Y axis of the AACS body frame.
+
+ Note the angles in the frame definitions are specified for the ``from
+ instrument to (relative to) base frame'' transformation.
+
+
+Visible and Infrared Mapping Spectrometer Visible (VIMS_V)
+
+ The VIMS_V detector points nominally along the spacecraft -Y axis. The
+ following frame definition encapsulates this nominal frame.
+
+ From [13]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ -90.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_VIMS_V = -82370
+ FRAME_-82370_NAME = 'CASSINI_VIMS_V'
+ FRAME_-82370_CLASS = 4
+ FRAME_-82370_CLASS_ID = -82370
+ FRAME_-82370_CENTER = -82
+ TKFRAME_-82370_SPEC = 'ANGLES'
+ TKFRAME_-82370_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82370_ANGLES = (
+ 179.9169210948516,
+ 90.0052712114302,
+ -179.2606182385525
+ )
+ TKFRAME_-82370_AXES = ( 3, 1, 3 )
+ TKFRAME_-82370_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Visible and Infrared Mapping Spectrometer Infrared (VIMS_IR)
+
+ The VIMS_IR detector points nominally along the spacecraft -Y axis. The
+ following frame definition encapsulates this nominal frame.
+
+ From [13]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ -90.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ FRAME_CASSINI_VIMS_IR = -82371
+ FRAME_-82371_NAME = 'CASSINI_VIMS_IR'
+ FRAME_-82371_CLASS = 4
+ FRAME_-82371_CLASS_ID = -82371
+ FRAME_-82371_CENTER = -82
+ TKFRAME_-82371_SPEC = 'ANGLES'
+ TKFRAME_-82371_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82371_ANGLES = ( 0.0, 0.0, -90.0 )
+ TKFRAME_-82371_AXES = ( 3, 2, 1 )
+ TKFRAME_-82371_UNITS = 'DEGREES'
+
+
+ From [41], the VIMS_IR boresight has been adjusted to the following vector
+ in spacecraft coordinates:
+
+ [ 0.0021251 ]
+ VIMS_IR Boresight Vector = [ -0.9999974 ]
+ [ -0.0008495 ]
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ By the methodology outlined above, this produces the following frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -360.121759 ] [ -90.0486727 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_VIMS_IR = -82371
+ FRAME_-82371_NAME = 'CASSINI_VIMS_IR'
+ FRAME_-82371_CLASS = 4
+ FRAME_-82371_CLASS_ID = -82371
+ FRAME_-82371_CENTER = -82
+ TKFRAME_-82371_SPEC = 'ANGLES'
+ TKFRAME_-82371_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82371_ANGLES = (
+ 179.8773296781574,
+ 90.0476127679153,
+ 179.5901924534006
+ )
+ TKFRAME_-82371_AXES = ( 3, 1, 3 )
+ TKFRAME_-82371_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Visible and Infrared Mapping Spectrometer Infrared Solar Port (VIMS_IR_SOL)
+
+ [28] indicates that the VIMS IR channel solar port points nominally 20
+ degrees offset from the VIMS IR boresight in the -Y direction of the
+ VIMS_IR frame. The rotation matrix that takes vectors represented in the
+ VIMS_IR_SOL frame into the VIMS_IR frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ -20.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+
+ FRAME_CASSINI_VIMS_IR_SOL = -82372
+ FRAME_-82372_NAME = 'CASSINI_VIMS_IR_SOL'
+ FRAME_-82372_CLASS = 4
+ FRAME_-82372_CLASS_ID = -82372
+ FRAME_-82372_CENTER = -82
+ TKFRAME_-82372_SPEC = 'ANGLES'
+ TKFRAME_-82372_RELATIVE = 'CASSINI_VIMS_IR'
+ TKFRAME_-82372_ANGLES = ( 0.0, 0.0, -20.0 )
+ TKFRAME_-82372_AXES = ( 3, 2, 1 )
+ TKFRAME_-82372_UNITS = 'DEGREES'
+
+
+ [42] requested that CASSINI_VIMS_IR_SOL be referenced directly to
+ CASSINI_SC_COORD. In addition, [42], [43], and [45] also carry updates to
+ the alignment of the solar port. The rotation matrix that takes vectors
+ represented in the VIMS_IR_SOL frame into the CASSINI_SC_COORD frame
+ follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0859436686699 ] [ 0.0 ] [ -110.630253571 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_VIMS_IR_SOL = -82372
+ FRAME_-82372_NAME = 'CASSINI_VIMS_IR_SOL'
+ FRAME_-82372_CLASS = 4
+ FRAME_-82372_CLASS_ID = -82372
+ FRAME_-82372_CENTER = -82
+ TKFRAME_-82372_SPEC = 'ANGLES'
+ TKFRAME_-82372_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82372_ANGLES = ( 0.085943668669984,
+ 0.0,
+ -110.63025357166 )
+ TKFRAME_-82372_AXES = ( 3, 2, 1 )
+ TKFRAME_-82372_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Visible and Infrared Mapping Spectrometer Radiator (VIMS_RAD)
+
+ The VIMS radiator is nominally oriented with its +Z axis directed down the
+ spacecraft +X axis. This is not the case for the radiator plate itself,
+ which is mounted in the housing such that it is canted by 28.05 degrees. In
+ the spacecraft coordinate frame, the cant is towards the spacecraft -Y
+ axis.
+
+ This, however, is not the end of the story. Thermally, the radiator housing
+ and the radiator plate have interaction with respect to solar heating so
+ that the effective boresight for symmetric solar heating, regardless of
+ direction, is not offset by 28.05 degrees from the spacecraft +X axis.
+ Initially the +Z axis of the radiator frame was determined to be the +X
+ axis of the spacecraft frame. This results in the following:
+
+ Since only boresight information has been provided, the frame
+ transformation outlined below was constructed by computing the RA and DEC
+ of the boresight vector relative to the CASSINI_SC_COORD frame. These
+ angles are then utilized in the following fashion to construct the frame
+ definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -(RA+90) ] [ -(90-DEC) ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ This produces a frame whose Z-axis agrees with the specified boresight.
+
+ As [17] indicates, the VIMS_RAD boresight is nominally aligned with the +X
+ axis in the spacecraft frame. By the methodology outlined above, this
+ produces the following frame definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -90.0 ] [ -90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ FRAME_CASSINI_VIMS_RAD = -82378
+ FRAME_-82378_NAME = 'CASSINI_VIMS_RAD'
+ FRAME_-82378_CLASS = 4
+ FRAME_-82378_CLASS_ID = -82378
+ FRAME_-82378_CENTER = -82
+ TKFRAME_-82378_SPEC = 'ANGLES'
+ TKFRAME_-82378_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82378_ANGLES = ( -90.0, -90.0, 0.0 )
+ TKFRAME_-82378_AXES = ( 3, 1, 3 )
+ TKFRAME_-82378_UNITS = 'DEGREES'
+
+
+ From [36]:
+
+ A solar heating analysis and identification of a solar heating
+ ``effective'' radiator boresight was performed for ECR 100325-B covering
+ Flight Rule FF37B2 [37]. The solar heating analysis identified that a VIMS
+ radiator boresight offset from the spacecraft +X axis in the direction of
+ the spacecraft -Y axis by 4.5 degrees would define a thermally
+ ``effective'' boresight.
+
+ To implement this change, the rotation about the Z-axis needs to be
+ increased by 4.5 degrees as follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -85.5 ] [ -90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z X Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_VIMS_RAD = -82378
+ FRAME_-82378_NAME = 'CASSINI_VIMS_RAD'
+ FRAME_-82378_CLASS = 4
+ FRAME_-82378_CLASS_ID = -82378
+ FRAME_-82378_CENTER = -82
+ TKFRAME_-82378_SPEC = 'ANGLES'
+ TKFRAME_-82378_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82378_ANGLES = ( -85.5, -90.0, 0.0 )
+ TKFRAME_-82378_AXES = ( 3, 1, 3 )
+ TKFRAME_-82378_UNITS = 'DEGREES'
+
+ \begintext
+
+
+CAPS Frames
+----------------------------------------------------------
+
+ The Cassini Plasma Spectrometer is mounted on an actuator which is in turn
+ attached to the fields and particles pallet which is roughly located on the
+ -X side of the Cassini spacecraft.
+
+ The actuator allows the instrument to articulate, so to make proper use of
+ this frame requires a C-kernel (or set of C-kernels) with appropriate
+ coverage for the epochs of interest.
+
+ To connect the CASSINI_CAPS frame with the spacecraft coordinate frame
+ (CASSINI_SC_COORD) two possible branches exist depending on the set of
+ C-kernels loaded:
+
+
+ CASSINI_SC_COORD CASSINI_SC_COORD
+ ---------------- ----------------
+ | |
+ |<--- fixed offset |
+ | |
+ V |
+ CASSINI_CAPS_BASE |
+ ----------------- |
+ | |
+ |<--- c-kernel |<--- c-kernel
+ | |
+ V |
+ CASSINI_CAPS_ART |
+ ---------------- |
+ | |
+ |<--- c-kernel |
+ | |
+ V V
+ CASSINI_CAPS CASSINI_CAPS
+ ------------ ------------
+
+
+ The branch illustrated on the left of the figure above utilizes a series of
+ transformations to connect the spacecraft frame with the instrument frame.
+ The general strategy in this branch is the following:
+
+ -- Define a fixed offset frame that connects the spacecraft
+ frame to the base or 'zero-point' of the articulation of the
+ instrument.
+
+ -- Define a C-kernel based frame to perform the rotation about
+ the articulation axis.
+
+ -- Define a C-kernel based frame that performs the final
+ rotation necessary to produce the instrument frame.
+
+ This last frame in the absence of the right branch could be another fixed
+ offset frame. However, making it a C-kernel allows the branch on the right
+ to exist. This alternate route up the frame tree allows the construction
+ and use of C-kernels that tie the instrument frame directly back to the
+ spacecraft frame. This is often convenient for science data analysis.
+
+ Without further ado, the frame definitions:
+
+
+Cassini Plasma Spectrometer Zero-Articulation Base Frame (CAPS_BASE)
+
+ The Z-axis of this frame is the articulation axis of CAPS. The X-axis is
+ constructed by taking the vector product of the CAPS articulation axis with
+ the boresight in the 'zero-angle' or base position. The Y-axis completes
+ the right handed frame. The articulation axis of CAPS is the Z-axis of
+ CASSINI_SC_COORD, and the boresight in its 'zero-angle' configuration is
+ the negative Y-axis of this spacecraft frame, so we end up with the
+ following:
+
+ The rotation matrix that takes vectors represented in the CAPS_BASE frame
+ into the spacecraft coordinate frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 0.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_CAPS_BASE = -82822
+ FRAME_-82822_NAME = 'CASSINI_CAPS_BASE'
+ FRAME_-82822_CLASS = 4
+ FRAME_-82822_CLASS_ID = -82822
+ FRAME_-82822_CENTER = -82
+ TKFRAME_-82822_SPEC = 'ANGLES'
+ TKFRAME_-82822_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82822_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-82822_AXES = ( 3, 2, 1 )
+ TKFRAME_-82822_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Cassini Plasma Spectrometer Articulation Frame (CAPS_ART)
+
+ The Z-axis of this frame is the articulation axis of CAPS. The X-axis is
+ constructed by taking the vector product of the CAPS articulation axis with
+ the boresight at some articulated position. The Y-axis completes the right
+ handed frame.
+
+ This frame encapsulates the articulation characteristics of the CAPS
+ instrument. To make use of it requires a C-kernel with coverage at the
+ epochs of interest be loaded.
+
+ The rotation matrix that takes vectors from the CAPS_ART frame to the
+ CAPS_BASE frame follows:
+
+ [ ] [ ]
+ [ ROT ] = [ ANGLE ]
+ [ ] [ ]
+ Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i, and ANGLE is the articulation angle.
+
+ \begindata
+
+ FRAME_CASSINI_CAPS_ART = -82821
+ FRAME_-82821_NAME = 'CASSINI_CAPS_ART'
+ FRAME_-82821_CLASS = 3
+ FRAME_-82821_CLASS_ID = -82821
+ FRAME_-82821_CENTER = -82
+ CK_-82821_SCLK = -82
+ CK_-82821_SPK = -82
+
+ \begintext
+
+
+Cassini Plasma Spectrometer Frame (CAPS)
+
+ The negative Y-axis of this frame is the instrument boresight. The Z-axis
+ is defined as the articulation axis of the detectors, and the X-axis
+ completes the right handed frame.
+
+ This frame requires one of two possible C-kernels:
+
+ -- One kernel connects this instrument frame (-82820) directly
+ to the spacecraft frame (-82000).
+
+ -- The other possible kernel connects this instrument frame
+ (-82820) to the articulation frame (-82821) defined above.
+ The kernel that makes this connection for all epochs after
+ launch is delivered with the kernel set. See the kernel
+ comments for details of frame construction.
+
+ One should take care in the simultaneous loading of C-kernels that utilize
+ different paths of the frame tree to connect CASSINI_CAPS to
+ CASSINI_SC_COORD. See [1] for details regarding C-kernel precedence.
+
+ \begindata
+
+ FRAME_CASSINI_CAPS = -82820
+ FRAME_-82820_NAME = 'CASSINI_CAPS'
+ FRAME_-82820_CLASS = 3
+ FRAME_-82820_CLASS_ID = -82820
+ FRAME_-82820_CENTER = -82
+ CK_-82820_SCLK = -82
+ CK_-82820_SPK = -82
+
+ \begintext
+
+
+CDA Frames
+----------------------------------------------------------
+
+ The Cosmic Dust Analyzer is mounted on the -X side of the Cassini
+ spacecraft. The entire assembly is capable of articulating from it's zero
+ angle position. The following describes the boresight in the spacecraft
+ frame as a function of the articulation angle a:
+
+ From [18]:
+
+ x = 1/8 ( -1 - SQRT(3) + (-1 + SQRT(3)) COS(a) - 2 SQRT(6) SIN(a) )
+ y = 1/8 ( 3 + SQRT(3) + (-3 + SQRT(3)) COS(a) - 2 SQRT(2) SIN(a) )
+ z = 1/4 ( -1 + SQRT(3) + ( 1 + SQRT(3)) COS(a) )
+
+
+ The actuator allows the instrument to articulate, so to make proper use of
+ this frame requires a C-kernel (or set of C-kernels) with appropriate
+ coverage for the epochs of interest.
+
+ To connect the CASSINI_CDA frame with the spacecraft coordinate frame
+ (CASSINI_SC_COORD) two possible branches exist depending on the set of
+ C-kernels loaded:
+
+
+ CASSINI_SC_COORD CASSINI_SC_COORD
+ ---------------- ----------------
+ | |
+ |<--- fixed offset |
+ | |
+ V |
+ CASSINI_CDA_BASE |
+ ---------------- |
+ | |
+ |<--- c-kernel |<--- c-kernel
+ | |
+ V |
+ CASSINI_CDA_ART |
+ --------------- |
+ | |
+ |<--- c-kernel |
+ | |
+ V V
+ CASSINI_CDA CASSINI_CDA
+ ----------- -----------
+
+
+ The branch illustrated on the left of the figure above utilizes a series of
+ transformations to connect the spacecraft frame with the instrument frame.
+ The general strategy in this branch is the following:
+
+ -- Define a fixed offset frame that connects the spacecraft
+ frame to the base or 'zero-point' of the articulation of the
+ instrument.
+
+ -- Define a C-kernel based frame to perform the rotation about
+ the articulation axis.
+
+ -- Define a C-kernel based frame that performs the final
+ rotation necessary to produce the instrument frame.
+
+ This last frame in the absence of the right branch could be another fixed
+ offset frame. However, making it a C-kernel allows the branch on the right
+ to exist. This alternate route up the frame tree allows the construction
+ and use of C-kernels that tie the instrument frame directly back to the
+ spacecraft frame. This is often convenient for science data analysis.
+
+ Without further ado, the frame definitions:
+
+
+Cosmic Dust Analyzer Zero-Articulation Base Frame (CDA_BASE)
+
+ The Z-axis of this frame is the articulation axis of CDA. The X-axis is
+ constructed by taking the vector product of the CDA articulation axis with
+ the boresight in the 'zero-angle' or base position. The Y-axis completes
+ the right handed frame.
+
+ An examination of the relationship connecting the boresight position in the
+ spacecraft frame with the articulation angle, yields the following:
+
+ The articulation axis of CDA in CASSINI_SC_COORD is:
+
+ (+4.8296291314453E-01, -8.3651630373781E-01, -2.5881904510252E-01)
+
+ The 'zero-angle' boresight in CASSINI_SC_COORD is:
+
+ (-2.5000000000000E-01, 4.3301270189222E-01, 8.6602540378444E-01)
+
+
+ The articulation axis points in the opposite direction of the cone swept
+ out by the boresight vectors. This was done to preserve the sense of the
+ positive angle in the definition provided in [18].
+
+ Computing the frame described above we end up with:
+
+ The rotation matrix that takes vectors represented in the CDA_BASE frame
+ into the spacecraft coordinate frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 150.0 ] [ 0.0 ] [ 105.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_CDA_BASE = -82792
+ FRAME_-82792_NAME = 'CASSINI_CDA_BASE'
+ FRAME_-82792_CLASS = 4
+ FRAME_-82792_CLASS_ID = -82792
+ FRAME_-82792_CENTER = -82
+ TKFRAME_-82792_SPEC = 'ANGLES'
+ TKFRAME_-82792_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82792_ANGLES = ( 150.0, 0.0, 105.0 )
+ TKFRAME_-82792_AXES = ( 3, 2, 1 )
+ TKFRAME_-82792_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Cosmic Dust Analyzer Articulation Frame (CDA_ART)
+
+ The Z-axis of this frame is the articulation axis of CDA. The X-axis is
+ constructed by taking the vector product of the CDA articulation axis with
+ the boresight at some articulated position. The Y-axis completes the right
+ handed frame.
+
+ This frame encapsulates the articulation characteristics of the CDA
+ instrument. To make use of it requires a C-kernel with coverage at the
+ epochs of interest be loaded.
+
+ The rotation matrix that takes vectors from the CDA_ART frame to the
+ CDA_BASE frame follows:
+
+ [ ] [ ]
+ [ ROT ] = [ ANGLE ]
+ [ ] [ ]
+ Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i, and ANGLE is the articulation angle.
+
+ \begindata
+
+ FRAME_CASSINI_CDA_ART = -82791
+ FRAME_-82791_NAME = 'CASSINI_CDA_ART'
+ FRAME_-82791_CLASS = 3
+ FRAME_-82791_CLASS_ID = -82791
+ FRAME_-82791_CENTER = -82
+ CK_-82791_SCLK = -82
+ CK_-82791_SPK = -82
+
+ \begintext
+
+
+Cosmic Dust Analyzer Frame (CDA)
+
+ The Z-axis of this frame is the instrument boresight. The X-axis of is the
+ same as the X-axis of CASSINI_CDA_ART, and the Y-axis completes the right
+ handed frame.
+
+ This frame requires one of two possible C-kernels:
+
+ -- One kernel connects this instrument frame (-82790) directly
+ to the spacecraft frame (-82000).
+
+ -- The other possible kernel connects this instrument frame
+ (-82790) to the articulation frame (-82791) defined above.
+ The kernel that makes this connection for all epochs after
+ launch is delivered with the kernel set. See the kernel
+ comments for details of frame construction.
+
+ One should take care in the simultaneous loading of C-kernels that utilize
+ different paths of the frame tree to connect CASSINI_CDA to
+ CASSINI_SC_COORD. See [1] for details regarding C-kernel precedence.
+
+ \begindata
+
+ FRAME_CASSINI_CDA = -82790
+ FRAME_-82790_NAME = 'CASSINI_CDA'
+ FRAME_-82790_CLASS = 3
+ FRAME_-82790_CLASS_ID = -82790
+ FRAME_-82790_CENTER = -82
+ CK_-82790_SCLK = -82
+ CK_-82790_SPK = -82
+
+ \begintext
+
+
+INMS Frames
+----------------------------------------------------------
+
+ The Ion and Neutral Mass Spectrometer is mounted on the fields and
+ particles pallet roughly located on the -X side of the Cassini spacecraft.
+ The instrument boresight is nominally directed along the -X axis of the
+ AACS body frame.
+
+ Note the angles in the frame definitions are specified for the ``from
+ instrument to (relative to) base frame'' transformation.
+
+ From [19], we have the following nominal frame definition:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ +90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_INMS = -82740
+ FRAME_-82740_NAME = 'CASSINI_INMS'
+ FRAME_-82740_CLASS = 4
+ FRAME_-82740_CLASS_ID = -82740
+ FRAME_-82740_CENTER = -82
+ TKFRAME_-82740_SPEC = 'ANGLES'
+ TKFRAME_-82740_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82740_ANGLES = ( 0.0, +90.0, 0.0 )
+ TKFRAME_-82740_AXES = ( 1, 2, 3 )
+ TKFRAME_-82740_UNITS = 'DEGREES'
+
+ \begintext
+
+
+MAG Frames
+----------------------------------------------------------
+
+ The Magnetometer is mounted on the magnetometer boom which protrudes from
+ the spacecraft body in the direction of the +Y axis of the AACS body frame.
+ [20] establishes the need for two separate frame definitions, one for the
+ Plus-X directed frame, the other for the Minux-X one.
+
+ Note the angles in the frame definitions are specified for the ``from
+ instrument to (relative to) base frame'' transformation.
+
+
+Magnetometer Plus-X (MAG_PLUS)
+
+ The MAG_PLUS detector is pointed nominally in the direction of the
+ spacecraft +X axis. The following definition encapsulates this frame:
+
+ From [21]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ -90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_MAG_PLUS = -82350
+ FRAME_-82350_NAME = 'CASSINI_MAG_PLUS'
+ FRAME_-82350_CLASS = 4
+ FRAME_-82350_CLASS_ID = -82350
+ FRAME_-82350_CENTER = -82
+ TKFRAME_-82350_SPEC = 'ANGLES'
+ TKFRAME_-82350_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82350_ANGLES = ( 0.0, -90.0, 0.0 )
+ TKFRAME_-82350_AXES = ( 1, 2, 3 )
+ TKFRAME_-82350_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Magnetometer Minus-X (MAG_MINUS)
+
+ The MAG_MINUS detector is pointed nominally in the direction of the
+ spacecraft -X axis. The following definition encapsulates this frame:
+
+ From [21]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_MAG_MINUS = -82351
+ FRAME_-82351_NAME = 'CASSINI_MAG_MINUS'
+ FRAME_-82351_CLASS = 4
+ FRAME_-82351_CLASS_ID = -82351
+ FRAME_-82351_CENTER = -82
+ TKFRAME_-82351_SPEC = 'ANGLES'
+ TKFRAME_-82351_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82351_ANGLES = ( 0.0, 90.0, 0.0 )
+ TKFRAME_-82351_AXES = ( 1, 2, 3 )
+ TKFRAME_-82351_UNITS = 'DEGREES'
+
+ \begintext
+
+
+MIMI Frames
+----------------------------------------------------------
+
+ Most of the components of the Magnetospheric Imaging Instrument are mounted
+ on the fields and particles pallet roughly located on the -X side of the
+ Cassini spacecraft. The one exception is the Ion and Neutral Camera which
+ is mounted on the -Y side of the orbiter.
+
+ Note the angles in the frame definitions are specified for the ``from
+ instrument to (relative to) base frame'' transformation.
+
+
+Magnetospheric Imaging Instrument Charge Energy Mass Spectrometer (MIMI_CHEMS)
+
+ The MIMI_CHEMS detector is nominally pointed along the -X axis of the
+ spacecraft frame. The following definition encapsulates this frame:
+
+ From [17]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 0.0 ] [ 90.0 ] [ 90.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_MIMI_CHEMS = -82760
+ FRAME_-82760_NAME = 'CASSINI_MIMI_CHEMS'
+ FRAME_-82760_CLASS = 4
+ FRAME_-82760_CLASS_ID = -82760
+ FRAME_-82760_CENTER = -82
+ TKFRAME_-82760_SPEC = 'ANGLES'
+ TKFRAME_-82760_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82760_ANGLES = ( 0.0, 90.0, 90.0 )
+ TKFRAME_-82760_AXES = ( 1, 2, 3 )
+ TKFRAME_-82760_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Magnetospheric Imaging Instrument Ion and Neutral Camera (MIMI_INCA)
+
+ The MIMI_INCA detector is nominally pointed along the -Y axis of the
+ spacecraft frame with a 9.5 degree offset in the direction of the +X axis
+ of the spacecraft. The following definition encapsulates this frame:
+
+ From [22]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -90.0 ] [ -9.5 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_MIMI_INCA = -82761
+ FRAME_-82761_NAME = 'CASSINI_MIMI_INCA'
+ FRAME_-82761_CLASS = 4
+ FRAME_-82761_CLASS_ID = -82761
+ FRAME_-82761_CENTER = -82
+ TKFRAME_-82761_SPEC = 'ANGLES'
+ TKFRAME_-82761_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82761_ANGLES = ( -90.0, -9.5, 0.0 )
+ TKFRAME_-82761_AXES = ( 1, 2, 3 )
+ TKFRAME_-82761_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Magnetospheric Imaging Instrument Low Energy Magnetospheric Measurements
+(MIMI_LEMMS)
+
+ The actuator allows the detectors to articulate, so to make proper use of
+ this frame requires a C-kernel (or set of C-kernels) with appropriate
+ coverage for the epochs of interest.
+
+ To connect the CASSINI_MIMI_LEMMS1 and CASSINI_MIMI_LEMMS2 frames with the
+ spacecraft coordinate frame (CASSINI_SC_COORD) two possible branches exist
+ depending on the set of C-kernels loaded:
+
+
+ CASSINI_SC_COORD CASSINI_SC_COORD
+ ---------------- ----------------
+ | | |
+ |<--- fixed offset | |
+ | | |
+ V | |
+ CASSINI_MIMI_LEMMS_BASE | |
+ ----------------------- | |
+ | | |
+ |<--- c-kernel |<--- c-kernel |
+ | | |
+ V | |
+ CASSINI_MIMI_LEMMS_ART | |
+ ---------------------- | |
+ | | | |
+ |<--- c-kernel | | c-kernel --->|
+ | | | |
+ V | V |
+ CASSINI_MIMI_LEMMS1 | CASSINI_MIMI_LEMMS1 |
+ ------------------- | ------------------- |
+ | |
+ c-kernel --->| |
+ | |
+ V V
+ CASSINI_MIMI_LEMMS2 CASSINI_MIMI_LEMMS2
+ ------------------- -------------------
+
+
+ The branches illustrated on the left of the figure above utilize a series
+ of transformations to connect the spacecraft frame with the detector
+ frames. The general strategy in these branches is the following:
+
+ -- Define a fixed offset frame that connects the spacecraft
+ frame to the base or 'zero-point' of the articulation of the
+ detectors.
+
+ -- Define a C-kernel based frame to perform the rotation about
+ the articulation axis.
+
+ -- Define a C-kernel based frame that performs the final
+ rotation necessary to produce either of the instrument frame.
+
+ These last frames (MIMI_LEMMS1 and MIMI_LEMMS2) in the absence of the right
+ branch could be another fixed offset frame. However, making them C-kernels
+ allows the branches on the right to exist. This alternate route up the
+ frame tree allows the construction and use of C-kernels that tie the
+ individual detector frames directly back to the spacecraft frame. This is
+ often convenient for science data analysis.
+
+ Without further ado, the frame definitions:
+
+
+Magnetospheric Imaging Instrument Low Energy Magnetospheric Measurements
+Zero-Articulation Base Frame (MIMI_LEMMS_BASE)
+
+ The Z-axis of this frame is the articulation axis of MIMI_LEMMS. The X-axis
+ is constructed by taking the vector product of the MIMI_LEMMS articulation
+ axis with the MIMI_LEMMS1 boresight in the 'zero-angle' or base position.
+ The Y-axis completes the right handed frame.
+
+ As [33] indicates, the articulation axis is the Y-axis in CASSINI_SC_COORD
+ and the 'zero-angle' boresight of MIMI_LEMMS1 is the -Z-axis in
+ CASSINI_SC_COORD. Combining this information with the frame definition laid
+ out above, we have:
+
+ The rotation matrix that takes vectors represented in the MIMI_LEMMS_BASE
+ frame into the spacecraft coordinate frame follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 180.0 ] [ 0.0 ] [ -90.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_MIMI_LEMMS_BASE = -82765
+ FRAME_-82765_NAME = 'CASSINI_MIMI_LEMMS_BASE'
+ FRAME_-82765_CLASS = 4
+ FRAME_-82765_CLASS_ID = -82765
+ FRAME_-82765_CENTER = -82
+ TKFRAME_-82765_SPEC = 'ANGLES'
+ TKFRAME_-82765_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82765_ANGLES = ( 180.0, 0.0, -90.0 )
+ TKFRAME_-82765_AXES = ( 3, 2, 1 )
+ TKFRAME_-82765_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Magnetospheric Imaging Instrument Low Energy Magnetospheric Measurements
+Articulation Frame (MIMI_LEMMS_ART)
+
+ The Z-axis of this frame is the articulation axis of MIMI_LEMMS. The X-axis
+ is constructed by taking the vector product of the MIMI_LEMMS articulation
+ axis with the MIMI_LEMMS1 boresight at some articulated position. The
+ Y-axis completes the right handed frame.
+
+ This frame encapsulates the articulation characteristics of the MIMI_LEMMS
+ instrument. To make use of it requires a C-kernel with coverage at the
+ epochs of interest be loaded.
+
+ The rotation matrix that takes vectors from the MIMI_LEMMS_ART frame to the
+ MIMI_LEMMS_BASE frame follows:
+
+ [ ] [ ]
+ [ ROT ] = [ ANGLE ]
+ [ ] [ ]
+ Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i, and ANGLE is the articulation angle.
+
+ \begindata
+
+ FRAME_CASSINI_MIMI_LEMMS_ART = -82764
+ FRAME_-82764_NAME = 'CASSINI_MIMI_LEMMS_ART'
+ FRAME_-82764_CLASS = 3
+ FRAME_-82764_CLASS_ID = -82764
+ FRAME_-82764_CENTER = -82
+ CK_-82764_SCLK = -82
+ CK_-82764_SPK = -82
+
+ \begintext
+
+
+Magnetospheric Imaging Instrument Low Energy Magnetospheric Measurements 1
+(MIMI_LEMMS1)
+
+ The Z-axis of this frame is the instrument boresight.
+
+ This frame requires one of two possible C-kernels:
+
+ -- One kernel connects this instrument frame (-82762) directly
+ to the spacecraft frame (-82000).
+
+ -- The other possible kernel connects this instrument frame
+ (-82762) to the articulation frame (-82764) defined above.
+ The kernel that makes this connection for all epochs after
+ launch is delivered with the kernel set. See the kernel
+ comments for details of the frame construction.
+
+ One should take care in the simultaneous loading of C-kernels that utilize
+ different paths of the frame tree to connect CASSINI_MIMI_LEMMS1 to
+ CASSINI_SC_COORD. See [1] for details regarding C-kernel precedence.
+
+ \begindata
+
+ FRAME_CASSINI_MIMI_LEMMS1 = -82762
+ FRAME_-82762_NAME = 'CASSINI_MIMI_LEMMS1'
+ FRAME_-82762_CLASS = 3
+ FRAME_-82762_CLASS_ID = -82762
+ FRAME_-82762_CENTER = -82
+ CK_-82762_SCLK = -82
+ CK_-82762_SPK = -82
+
+ \begintext
+
+
+Magnetospheric Imaging Instrument Low Energy Magnetospheric Measurements 2
+(MIMI_LEMMS2)
+
+ The Z-axis of this frame is the instrument boresight.
+
+ This frame requires one of two possible C-kernels:
+
+ -- One kernel connects this instrument frame (-82763) directly
+ to the spacecraft frame (-82000).
+
+ -- The other possible kernel connects this instrument frame
+ (-82763) to the articulation frame (-82764) defined above.
+ The kernel that makes this connection for all epochs after
+ launch is delivered with the kernel set. See the kernel
+ comments for details of the frame construction.
+
+ One should take care in the simultaneous loading of C-kernels that utilize
+ different paths of the frame tree to connect CASSINI_MIMI_LEMMS2 to
+ CASSINI_SC_COORD. See [1] for details regarding C-kernel precedence.
+
+ \begindata
+
+ FRAME_CASSINI_MIMI_LEMMS2 = -82763
+ FRAME_-82763_NAME = 'CASSINI_MIMI_LEMMS2'
+ FRAME_-82763_CLASS = 3
+ FRAME_-82763_CLASS_ID = -82763
+ FRAME_-82763_CENTER = -82
+ CK_-82763_SCLK = -82
+ CK_-82763_SPK = -82
+
+ \begintext
+
+
+RADAR Frames
+----------------------------------------------------------
+
+ Compiled from [23] and [5]:
+
+ The RADAR instrument consists of 5 beams in the following configuration:
+
+
+ ^ Xsc
+ |
+ |
+ Ysc |
+ <------o
+ | Zsc
+ |
+
+ .
+ .
+ .
+
+ Beam 1 Beam 2 Beam 3 Beam 4 Beam 5
+ |
+ |-----x-----|-----x-----|----x----|-----x-----|-----x-----|
+ |
+ |-- 1.35 ---|-- 0.85 --|-- 0.85 --|-- 1.35 ---|
+ |
+ |
+ V
+
+ Beam 3 Direction
+
+
+ The above figure illustrates the separation in degrees between the beam
+ centers and their relation to the spacecraft frame.
+
+ Note the angles in the frame definitions are specified fro the ``from
+ instrument to (relative to) base frame'' transformation.
+
+
+RADAR Beam 1 (RADAR_1)
+
+ RADAR Beam 1 is directed nominally 2.2 degrees off of the -Z axis of the
+ spacecraft in the direction of the +Y axis of the spacecraft frame. The
+ following definition encapsulates this frame:
+
+ From [23]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 177.8 ] [ 0.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_RADAR_1 = -82810
+ FRAME_-82810_NAME = 'CASSINI_RADAR_1'
+ FRAME_-82810_CLASS = 4
+ FRAME_-82810_CLASS_ID = -82810
+ FRAME_-82810_CENTER = -82
+ TKFRAME_-82810_SPEC = 'ANGLES'
+ TKFRAME_-82810_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82810_ANGLES = ( 177.8, 0.0, 0.0 )
+ TKFRAME_-82810_AXES = ( 1, 2, 3 )
+ TKFRAME_-82810_UNITS = 'DEGREES'
+
+ \begintext
+
+
+RADAR Beam 2 (RADAR_2)
+
+ RADAR Beam 2 is directed nominally 0.85 degrees off of the -Z axis of the
+ spacecraft in the direction of the +Y axis of the spacecraft frame. The
+ following definition encapsulates this frame:
+
+ From [23]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 179.15 ] [ 0.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ FRAME_CASSINI_RADAR_2 = -82811
+ FRAME_-82811_NAME = 'CASSINI_RADAR_2'
+ FRAME_-82811_CLASS = 4
+ FRAME_-82811_CLASS_ID = -82811
+ FRAME_-82811_CENTER = -82
+ TKFRAME_-82811_SPEC = 'ANGLES'
+ TKFRAME_-82811_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82811_ANGLES = ( 179.15, 0.0, 0.0 )
+ TKFRAME_-82811_AXES = ( 1, 2, 3 )
+ TKFRAME_-82811_UNITS = 'DEGREES'
+
+
+ From [44], the RADAR Beam 2 reference frame is to be adjusted to the
+ following:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 179.15 ] [ -1.2 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_RADAR_2 = -82811
+ FRAME_-82811_NAME = 'CASSINI_RADAR_2'
+ FRAME_-82811_CLASS = 4
+ FRAME_-82811_CLASS_ID = -82811
+ FRAME_-82811_CENTER = -82
+ TKFRAME_-82811_SPEC = 'ANGLES'
+ TKFRAME_-82811_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82811_ANGLES = ( 179.15, -1.2, 0.0 )
+ TKFRAME_-82811_AXES = ( 1, 2, 3 )
+ TKFRAME_-82811_UNITS = 'DEGREES'
+
+ \begintext
+
+
+RADAR Beam 3 (RADAR_3)
+
+ RADAR Beam 3 is directed nominally along the -Z axis of the spacecraft
+ frame. The following definition encapsulates this frame:
+
+ From [23]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 180.0 ] [ 0.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_RADAR_3 = -82812
+ FRAME_-82812_NAME = 'CASSINI_RADAR_3'
+ FRAME_-82812_CLASS = 4
+ FRAME_-82812_CLASS_ID = -82812
+ FRAME_-82812_CENTER = -82
+ TKFRAME_-82812_SPEC = 'ANGLES'
+ TKFRAME_-82812_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82812_ANGLES = ( 180.0, 0.0, 0.0 )
+ TKFRAME_-82812_AXES = ( 1, 2, 3 )
+ TKFRAME_-82812_UNITS = 'DEGREES'
+
+ \begintext
+
+
+RADAR Beam 4 (RADAR_4)
+
+ RADAR Beam 4 is directed nominally 0.85 degrees off of the -Z axis of the
+ spacecraft in the direction of the -Y axis of the spacecraft frame. The
+ following definition encapsulates this frame:
+
+ From [23]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 180.85 ] [ 0.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_RADAR_4 = -82813
+ FRAME_-82813_NAME = 'CASSINI_RADAR_4'
+ FRAME_-82813_CLASS = 4
+ FRAME_-82813_CLASS_ID = -82813
+ FRAME_-82813_CENTER = -82
+ TKFRAME_-82813_SPEC = 'ANGLES'
+ TKFRAME_-82813_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82813_ANGLES = ( 180.85, 0.0, 0.0 )
+ TKFRAME_-82813_AXES = ( 1, 2, 3 )
+ TKFRAME_-82813_UNITS = 'DEGREES'
+
+ \begintext
+
+ From [44], the RADAR Beam 4 reference frame is to be adjusted to the
+ following:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 180.85 ] [ -1.2 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ \begindata
+
+ FRAME_CASSINI_RADAR_4 = -82813
+ FRAME_-82813_NAME = 'CASSINI_RADAR_4'
+ FRAME_-82813_CLASS = 4
+ FRAME_-82813_CLASS_ID = -82813
+ FRAME_-82813_CENTER = -82
+ TKFRAME_-82813_SPEC = 'ANGLES'
+ TKFRAME_-82813_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82813_ANGLES = ( 180.85, -1.2, 0.0 )
+ TKFRAME_-82813_AXES = ( 1, 2, 3 )
+ TKFRAME_-82813_UNITS = 'DEGREES'
+
+ \begintext
+
+
+RADAR Beam 5 (RADAR_5)
+
+ RADAR Beam 5 is directed nominally 2.2 degrees off of the -Z axis of the
+ spacecraft in the direction of the -Y axis of the spacecraft frame. The
+ following definition encapsulates this frame:
+
+ From [23]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 182.2 ] [ 0.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_RADAR_5 = -82814
+ FRAME_-82814_NAME = 'CASSINI_RADAR_5'
+ FRAME_-82814_CLASS = 4
+ FRAME_-82814_CLASS_ID = -82814
+ FRAME_-82814_CENTER = -82
+ TKFRAME_-82814_SPEC = 'ANGLES'
+ TKFRAME_-82814_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82814_ANGLES = ( 182.2, 0.0, 0.0 )
+ TKFRAME_-82814_AXES = ( 1, 2, 3 )
+ TKFRAME_-82814_UNITS = 'DEGREES'
+
+ \begintext
+
+
+RPWS Frames
+----------------------------------------------------------
+
+ The RPWS antennae are located roughly on the +Y side of the Cassini
+ orbiter, while the RPWS Langmuir Probe is roughly located on the -X side.
+
+ Note the angles in the frame definitions are specified for the ``from
+ instrument to (relative to) base frame'' transformation.
+
+
+Radio and Plasma Wave Science (RPWS)
+
+ As [17] indicates, the ``collective'' RPWS boresight is nominally directed
+ along the spacecraft +Y axis. Utilizing the Euler angles specified in this
+ email, we obtain the following frame definition:
+
+ From [17]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 180.0 ] [ -90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ X Y Z
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_RPWS = -82730
+ FRAME_-82730_NAME = 'CASSINI_RPWS'
+ FRAME_-82730_CLASS = 4
+ FRAME_-82730_CLASS_ID = -82730
+ FRAME_-82730_CENTER = -82
+ TKFRAME_-82730_SPEC = 'ANGLES'
+ TKFRAME_-82730_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82730_ANGLES = ( 180.0, -90.0, 0.0 )
+ TKFRAME_-82730_AXES = ( 3, 1, 3 )
+ TKFRAME_-82730_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Radio and Plasma Wave Science Electric Antenna System (RPWS_E[AXIS][SIGN])
+
+ From [24]:
+
+ ``The RPWS electric antenna system is a triad of 10-meter conducting
+ monopoles, symmetric about the Y-Z plane. Two of the elements are extended
+ in a 120-degree "V" on either side of the magnetometer boom (i.e., the S/C
+ Y-axis) and in a plane which is rotated up from the S/C X-Y plane
+ containing the magnetometer boom by 37 degrees. These two elements are
+ referred to as the EXPLUS and EXMINUS sensors. The third element is
+ extended downward in the S/C Y-Z plane at an angle of 37 degrees from the
+ S/C +Z axis. That said, it now should be explained that the "electrical"
+ characteristics of these three antennas deviate from the physical alignment
+ and lengths of the elements due to the complex ground plane provided by the
+ spacecraft. It is these electrical characteristics that the three RPWS
+ Frame definitions RPWS_EXPLUS, RPWS_EXMINUS, and RPWS_EZPLUS are intended
+ to specify. Based upon model rheometry experiments, in which a model of the
+ Cassini Spacecraft with fully extended RPWS antennas was immersed in a tank
+ filled with an electrolytic, the following estimates have been made for the
+ electrical axes of the three antenna elements:
+
+ Frame Frame Z-Axis in CASSINI_SC_COORD "boresight"
+ ------ --------------------------------
+ RPWS_EXPLUS [ 0.91202578, 0.27709462, -0.30236989 ]
+ RPWS_EXMINUS [ -0.91202578, 0.27709462, -0.30236989 ]
+ RPWS_EZPLUS [ -0.01091120, 0.52089537, 0.85355080 ]
+
+ These numbers may change after the RPWS Jupiter Calibrations.''
+
+ Antenna Frame Definitions:
+
+ From [14]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -16.9 ] [ -107.6 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_RPWS_EXPLUS = -82731
+ FRAME_-82731_NAME = 'CASSINI_RPWS_EXPLUS'
+ FRAME_-82731_CLASS = 4
+ FRAME_-82731_CLASS_ID = -82731
+ FRAME_-82731_CENTER = -82
+ TKFRAME_-82731_SPEC = 'ANGLES'
+ TKFRAME_-82731_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82731_ANGLES = ( -16.9, -107.6, 0.0 )
+ TKFRAME_-82731_AXES = ( 3, 2, 1 )
+ TKFRAME_-82731_UNITS = 'DEGREES'
+
+ \begintext
+
+ From [14]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -163.1 ] [ -107.6 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_RPWS_EXMINUS= -82732
+ FRAME_-82732_NAME = 'CASSINI_RPWS_EXMINUS'
+ FRAME_-82732_CLASS = 4
+ FRAME_-82732_CLASS_ID = -82732
+ FRAME_-82732_CENTER = -82
+ TKFRAME_-82732_SPEC = 'ANGLES'
+ TKFRAME_-82732_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82732_ANGLES = (-163.1, -107.6, 0.0 )
+ TKFRAME_-82732_AXES = ( 3, 2, 1 )
+ TKFRAME_-82732_UNITS = 'DEGREES'
+
+ \begintext
+
+ From [14]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ -91.2 ] [ -31.4 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_RPWS_EZPLUS = -82733
+ FRAME_-82733_NAME = 'CASSINI_RPWS_EZPLUS'
+ FRAME_-82733_CLASS = 4
+ FRAME_-82733_CLASS_ID = -82733
+ FRAME_-82733_CENTER = -82
+ TKFRAME_-82733_SPEC = 'ANGLES'
+ TKFRAME_-82733_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82733_ANGLES = ( -91.2, -31.4, 0.0 )
+ TKFRAME_-82733_AXES = ( 3, 2, 1 )
+ TKFRAME_-82733_UNITS = 'DEGREES'
+
+ \begintext
+
+
+Radio and Plasma Wave Science Langmuir Probe (RPWS_LP)
+
+ From [24]:
+
+ ``The RPWS Langmuir Probe is on the -X side of the spacecraft and can sense
+ roughly the entire hemisphere defined by the RPWS_LP Frame.''
+
+ From [14]:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ 180.0 ] [ -90.0 ] [ 0.0 ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where [x] represents the rotation matrix of a given angle x about
+ i
+ axis i.
+
+ Nominal Frame Definition:
+
+ \begindata
+
+ FRAME_CASSINI_RPWS_LP = -82734
+ FRAME_-82734_NAME = 'CASSINI_RPWS_LP'
+ FRAME_-82734_CLASS = 4
+ FRAME_-82734_CLASS_ID = -82734
+ FRAME_-82734_CENTER = -82
+ TKFRAME_-82734_SPEC = 'ANGLES'
+ TKFRAME_-82734_RELATIVE = 'CASSINI_SC_COORD'
+ TKFRAME_-82734_ANGLES = ( 180.0, -90.0, 0.0 )
+ TKFRAME_-82734_AXES = ( 3, 2, 1 )
+ TKFRAME_-82734_UNITS = 'DEGREES'
+
+ \begintext
+
diff --git a/tests/pytests/data/v1514284191_1/cpck15Dec2017.tpc b/tests/pytests/data/v1514284191_1/cpck15Dec2017.tpc
new file mode 100644
index 0000000..320214d
--- /dev/null
+++ b/tests/pytests/data/v1514284191_1/cpck15Dec2017.tpc
@@ -0,0 +1,6229 @@
+KPL/PCK
+
+\begindata
+ CASSINI_PCK_VERSION = ( '2017-DEC-15' )
+\begintext
+
+
+P_constants (PcK) SPICE kernel file
+
+Refer to the notes at the bottom of the file for help, contacts, version history,
+references, and Cassini-specific parameter descriptions.
+
+
+
+-------- SUN
+
+ BODY10_GM [162].
+
+ \begindata
+ BODY10_GM = ( +1.327124400419e+11 )
+
+ \begintext
+
+
+-------- VENUS
+
+ BODY2_GM [64].
+ BODY299_GM [162].
+
+ \begindata
+ BODY2_GM = ( 324858.592000001 )
+ BODY299_GM = ( +3.248585920000e+05 )
+
+ \begintext
+
+
+-------- EARTH
+
+ BODY3_GM [162].
+ BODY399_GM [162].
+
+ \begindata
+ BODY3_GM = ( +4.035032355023e+05 )
+ BODY399_GM = ( +3.986004353851e+05 )
+
+ \begintext
+
+
+-------- JUPITER
+
+ BODY5_GM [162].
+ BODY599_GM [107].
+
+ \begindata
+ BODY5_GM = ( +1.267127641334e+08 )
+ BODY599_GM = ( +1.267127654544e+08 )
+
+ \begintext
+
+
+-------- SATURN
+
+ BODY6_GM [162].
+ BODY699_POLE_RA(3) [1].
+ BODY699_POLE_RA(2) [142].
+ BODY699_POLE_RA(1) [162].
+ BODY699_POLE_DEC(3) [1].
+ BODY699_POLE_DEC(2) [142].
+ BODY699_POLE_DEC(1) [162].
+ BODY699_JCOEF(9) [162].
+ BODY699_JCOEF(8) [162].
+ BODY699_JCOEF(7) [162].
+ BODY699_JCOEF(6) [162].
+ BODY699_JCOEF(5) [162].
+ BODY699_JCOEF(4) [162].
+ BODY699_JCOEF(3) [162].
+ BODY699_JCOEF(2) [162].
+ BODY699_JCOEF(14) [162].
+ BODY699_JCOEF(13) [162].
+ BODY699_JCOEF(12) [162].
+ BODY699_JCOEF(11) [162].
+ BODY699_JCOEF(10) [162].
+ BODY699_JCOEF(1) [1].
+ BODY699_GM [162].
+ BODY699_CCOEF(3) [1].
+ BODY699_CCOEF(2) [1].
+ BODY699_CCOEF(1) [1].
+
+ \begindata
+ BODY6_GM = ( +3.794058443092e+07 )
+ BODY699_GM = ( +3.793120689736e+07 )
+ BODY699_POLE_RA = ( +4.058386928634e+01 , -3.099714786917e-02 , 0. )
+ BODY699_POLE_DEC = ( +8.353795862295e+01 , -7.584170141686e-03 , 0. )
+ BODY699_JCOEF = ( 0.0 ,
+ +1.629071819646e-02 ,
+ -1.719725091833e-07 ,
+ -9.355171512888e-04 ,
+ +9.385669376989e-07 ,
+ +8.696709053146e-05 ,
+ -2.265811401077e-06 ,
+ -1.359656452114e-05 ,
+ +2.810564746209e-06 ,
+ +1.655341282022e-07 ,
+ +2.684326453530e-07 ,
+ -8.942151312331e-07 ,
+ -2.123089169715e-06 ,
+ -1.305944904496e-06 )
+ BODY699_CCOEF = ( 0.0 , 0.0 , 0.0000000000000 )
+ BODY699_SCOEF = ( 0.0 , 0.0 , 0.00000000 )
+
+ \begintext
+
+
+-------- URANUS
+
+ BODY7_GM [162].
+
+ \begindata
+ BODY7_GM = ( +5.794556465752e+06 )
+
+ \begintext
+
+
+-------- MOON
+
+ BODY301_GM [162].
+
+ \begindata
+ BODY301_GM = ( +4.902800117136e+03 )
+
+ \begintext
+
+
+-------- MIMAS
+
+ BODY601_GM [158].
+
+ \begindata
+ BODY601_GM = ( +2.502817739550e+00 )
+
+ \begintext
+
+
+-------- ENCELADUS
+
+ BODY602_JCOEF(2) [142].
+ BODY602_JCOEF(1) [23].
+ BODY602_GM [158].
+ BODY602_CCOEF(3) [142].
+ BODY602_CCOEF(2) [23].
+ BODY602_CCOEF(1) [23].
+
+ \begindata
+ BODY602_GM = ( +7.211777492985e+00 )
+ BODY602_JCOEF = ( 0.0 , +5.435200000000e-03 )
+ BODY602_CCOEF = ( 0.0 , 0.0 , +1.549800000000e-03 )
+
+ \begintext
+
+
+-------- TETHYS
+
+ BODY603_GM [162].
+
+ \begindata
+ BODY603_GM = ( +4.120850186975e+01 )
+
+ \begintext
+
+
+-------- DIONE
+
+ BODY604_JCOEF(3) [23].
+ BODY604_JCOEF(2) [142].
+ BODY604_JCOEF(1) [23].
+ BODY604_GM [162].
+ BODY604_CCOEF(3) [142].
+ BODY604_CCOEF(2) [23].
+ BODY604_CCOEF(1) [23].
+
+ \begindata
+ BODY604_GM = ( +7.311605842130e+01 )
+ BODY604_JCOEF = ( 0.0 , +1.436865258838e-03 )
+ BODY604_CCOEF = ( 0.0 , 0.0 , +3.651494811184e-04 )
+
+ \begintext
+
+
+-------- RHEA
+
+ BODY605_JCOEF(3) [23].
+ BODY605_JCOEF(2) [142].
+ BODY605_JCOEF(1) [23].
+ BODY605_GM [162].
+ BODY605_CCOEF(3) [142].
+ BODY605_CCOEF(2) [23].
+ BODY605_CCOEF(1) [23].
+
+ \begindata
+ BODY605_GM = ( +1.539500870013e+02 )
+ BODY605_JCOEF = ( 0.0 , +9.496088222042e-04 )
+ BODY605_CCOEF = ( 0.0 , 0.0 , +2.366835799998e-04 )
+
+ \begintext
+
+
+-------- TITAN
+
+ BODY606_SCOEF(3) [152].
+ BODY606_SCOEF(2) [41].
+ BODY606_SCOEF(1) [41].
+ BODY606_JCOEF(2) [152].
+ BODY606_JCOEF(1) [41].
+ BODY606_GM [162].
+ BODY606_CCOEF(3) [152].
+ BODY606_CCOEF(2) [41].
+ BODY606_CCOEF(1) [41].
+
+ \begindata
+ BODY606_GM = ( +8.978130958559e+03 )
+ BODY606_JCOEF = ( 0.0 , +3.341349498806e-05 )
+ BODY606_CCOEF = ( 0.0 , 0.0 , +1.046258225998e-05 )
+ BODY606_SCOEF = ( 0.0 , 0.0 , +3.915574411619e-07 )
+
+ \begintext
+
+
+-------- HYPERION
+
+ BODY607_GM [158].
+
+ \begindata
+ BODY607_GM = ( +3.713685396357e-01 )
+
+ \begintext
+
+
+-------- IAPETUS
+
+ BODY608_GM [162].
+
+ \begindata
+ BODY608_GM = ( +1.204890219402e+02 )
+
+ \begintext
+
+
+-------- PHOEBE
+
+ BODY609_GM [158].
+
+ \begindata
+ BODY609_GM = ( +5.527094668508e-01 )
+
+ \begintext
+
+
+
+ Note that GM values >= 1.0 are packaged as is into 7CONIC_VEC
+ commands for AACS to propagate the body's ephemeris.
+ For GM values < 1.0, the value in the G_MASS parameter
+ of the 7CONIC_VEC command is set to 1.0. One is the minimum
+ value for the G_MASS parameter. The resetting of the G_MASS
+ parameter to the minimum acceptable where the actual
+ GM is < 1.0 is acceptable since Cassini will not pass close enough
+ to any of the affected bodies for the gravitational mass
+ to have an effect.
+
+
+-------- CONSTANTS AND NOTES FOR CASPER USERS
+
+
+ \begindata
+ BODY601_GM/PRIMARY = ( 6.59087D-08 )
+ BODY602_GM/PRIMARY = ( 1.29181D-07 )
+ BODY603_GM/PRIMARY = ( 1.1022D-06 )
+ BODY604_GM/PRIMARY = ( 1.92865D-06 )
+ BODY605_GM/PRIMARY = ( 4.05998D-06 )
+ BODY606_GM/PRIMARY = ( 2.36697D-04 )
+ BODY607_GM/PRIMARY = ( 2.60998D-08 )
+ BODY608_GM/PRIMARY = ( 2.79453D-06 )
+ BODY609_GM/PRIMARY = ( 1.26545D-08 )
+ BODY610_GM/PRIMARY = ( 3.38507D-09 )
+ BODY611_GM/PRIMARY = ( 9.41176D-10 )
+ BODY612_GM/PRIMARY = ( 4.48179D-11 )
+ BODY613_GM/PRIMARY = ( 1.26545D-11 )
+ BODY614_GM/PRIMARY = ( 6.32723D-12 )
+ BODY615_GM/PRIMARY = ( 1.89817D-11 )
+ BODY616_GM/PRIMARY = ( 5.79996D-10 )
+ BODY617_GM/PRIMARY = ( 3.42725D-10 )
+ BODY618_GM/PRIMARY = ( 4.74543D-12 )
+ \begintext
+
+-------- URLS AND CONTACTS
+
+
+Description of PCK format and contents can be found in NAIF's PCK "required
+reading" document, at:
+
+ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/ascii/individual_docs/pck.req
+
+
+NAIF tutorial on PCK formatting and use at:
+
+ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/Tutorials/office/individual_docs/16_pck.ppt
+ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/Tutorials/office/packages/
+SPICE_Tutorials_Office.zip
+
+
+The Cassini PCK & ephemeris files can be found on the DOM, and at:
+
+ftp://naif.jpl.nasa.gov/pub/naif/CASSINI/kernels/
+
+
+Questions regarding this file can be directed to:
+
+Adrian Tinio (818)393-5995 Adrian.Tinio@jpl.nasa.gov
+
+
+
+
+
+
+
+-------- VERSION HISTORY
+
+2017-Dec-15 (published)
+Automated Process
+
+Applicable current Ephemeris = 171214R_SCPSE_17224_17258.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170915_1_288GF
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY603_GM +4.120850186975e+01 +4.120850186975e+01
+BODY604_GM +7.311605842130e+01 +7.311605842130e+01
+BODY605_GM +1.539500870013e+02 +1.539500870013e+02
+BODY606_GM +8.978130958559e+03 +8.978130958559e+03
+BODY608_GM +1.204890219402e+02 +1.204890219402e+02
+BODY699_GM +3.793120689736e+07 +3.793120689736e+07
+BODY699_JCOEF(10) +3.786000947517e-06 +1.655341282022e-07
+BODY699_JCOEF(11) +6.616273947210e-08 +2.684326453530e-07
+BODY699_JCOEF(12) -2.311925417381e-06 -8.942151312331e-07
+BODY699_JCOEF(13) -6.130127942069e-08 -2.123089169715e-06
+BODY699_JCOEF(14) -1.163170055382e-06 -1.305944904496e-06
+BODY699_JCOEF(2) +1.629057982688e-02 +1.629071819646e-02
+BODY699_JCOEF(3) +2.884389291908e-07 -1.719725091833e-07
+BODY699_JCOEF(4) -9.353674705844e-04 -9.355171512888e-04
+BODY699_JCOEF(5) +4.643582928107e-08 +9.385669376989e-07
+BODY699_JCOEF(6) +8.614756119106e-05 +8.696709053146e-05
+BODY699_JCOEF(7) +5.084433057059e-07 -2.265811401077e-06
+BODY699_JCOEF(8) -1.508059888260e-05 -1.359656452114e-05
+BODY699_JCOEF(9) +8.338320981889e-07 +2.810564746209e-06
+BODY699_POLE_DEC(1) +8.353795996624e+01 +8.353795862295e+01
+BODY699_POLE_RA(1) +4.058384124232e+01 +4.058386928634e+01
+BODY6_GM +3.794058443092e+07 +3.794058443092e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2017-Oct-31 (published)
+Automated Process
+
+Applicable current Ephemeris = 171031R_SCPSE_17177_17226.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170813_281GF
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY603_GM +4.120850186975e+01 +4.120850186975e+01
+BODY604_GM +7.311605842130e+01 +7.311605842130e+01
+BODY605_GM +1.539500870013e+02 +1.539500870013e+02
+BODY606_GM +8.978130958559e+03 +8.978130958559e+03
+BODY608_GM +1.204890219402e+02 +1.204890219402e+02
+BODY699_GM +3.793120689736e+07 +3.793120689736e+07
+BODY699_JCOEF(10) +3.748382572185e-06 +3.786000947517e-06
+BODY699_JCOEF(11) +2.886182422314e-08 +6.616273947210e-08
+BODY699_JCOEF(12) -2.332907321960e-06 -2.311925417381e-06
+BODY699_JCOEF(13) -8.423790343048e-08 -6.130127942069e-08
+BODY699_JCOEF(14) -1.172747659727e-06 -1.163170055382e-06
+BODY699_JCOEF(2) +1.629056935466e-02 +1.629057982688e-02
+BODY699_JCOEF(3) +2.965003945711e-07 +2.884389291908e-07
+BODY699_JCOEF(4) -9.353714329544e-04 -9.353674705844e-04
+BODY699_JCOEF(5) +4.685956775618e-09 +4.643582928107e-08
+BODY699_JCOEF(6) +8.610467107942e-05 +8.614756119106e-05
+BODY699_JCOEF(7) +4.738809141506e-07 +5.084433057059e-07
+BODY699_JCOEF(8) -1.511356193045e-05 -1.508059888260e-05
+BODY699_JCOEF(9) +8.047857413151e-07 +8.338320981889e-07
+BODY699_POLE_DEC(1) +8.353796209170e+01 +8.353795996624e+01
+BODY699_POLE_RA(1) +4.058381078301e+01 +4.058384124232e+01
+BODY6_GM +3.794058443092e+07 +3.794058443092e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2017-Oct-30 (published)
+Automated Process
+
+Applicable current Ephemeris = 171024R_SCPSE_17146_17177.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170714_276GF
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY603_GM +4.120850186975e+01 +4.120850186975e+01
+BODY604_GM +7.311605842130e+01 +7.311605842130e+01
+BODY605_GM +1.539500870013e+02 +1.539500870013e+02
+BODY606_GM +8.978130958559e+03 +8.978130958559e+03
+BODY608_GM +1.204890219402e+02 +1.204890219402e+02
+BODY699_GM +3.793120689736e+07 +3.793120689736e+07
+BODY699_JCOEF(10) +3.641907938036e-06 +3.748382572185e-06
+BODY699_JCOEF(11) -1.155312580876e-08 +2.886182422314e-08
+BODY699_JCOEF(12) -2.437044743424e-06 -2.332907321960e-06
+BODY699_JCOEF(13) -1.120617107914e-07 -8.423790343048e-08
+BODY699_JCOEF(14) -1.219002171382e-06 -1.172747659727e-06
+BODY699_JCOEF(2) +1.629057491353e-02 +1.629056935466e-02
+BODY699_JCOEF(3) +2.833112343228e-07 +2.965003945711e-07
+BODY699_JCOEF(4) -9.354181192562e-04 -9.353714329544e-04
+BODY699_JCOEF(5) +1.110932646324e-08 +4.685956775618e-09
+BODY699_JCOEF(6) +8.607405457832e-05 +8.610467107942e-05
+BODY699_JCOEF(7) +4.545482178452e-07 +4.738809141506e-07
+BODY699_JCOEF(8) -1.520674082639e-05 -1.511356193045e-05
+BODY699_JCOEF(9) +7.664061761364e-07 +8.047857413151e-07
+BODY699_POLE_DEC(1) +8.353796123271e+01 +8.353796209170e+01
+BODY699_POLE_RA(1) +4.058382745190e+01 +4.058381078301e+01
+BODY6_GM +3.794058443092e+07 +3.794058443092e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2017-Oct-21 (published)
+Automated Process
+
+Applicable current Ephemeris = 171017R_SCPSE_17117_17146.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170608_271GF
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY603_GM +4.120850186975e+01 +4.120850186975e+01
+BODY604_GM +7.311605842130e+01 +7.311605842130e+01
+BODY605_GM +1.539500870013e+02 +1.539500870013e+02
+BODY606_GM +8.978130958559e+03 +8.978130958559e+03
+BODY608_GM +1.204890219402e+02 +1.204890219402e+02
+BODY699_GM +3.793120689736e+07 +3.793120689736e+07
+BODY699_JCOEF(2) +1.629090771061e-02 +1.629057491353e-02
+BODY699_JCOEF(3) +0.000000000000e+00 +2.833112343228e-07
+BODY699_JCOEF(4) -9.338214217045e-04 -9.354181192562e-04
+BODY699_JCOEF(5) +0.000000000000e+00 +1.110932646324e-08
+BODY699_JCOEF(6) +8.325055333031e-05 +8.607405457832e-05
+BODY699_JCOEF(7) +0.000000000000e+00 +4.545482178452e-07
+BODY699_JCOEF(8) +0.000000000000e+00 -1.520674082639e-05
+BODY699_JCOEF(9) +0.000000000000e+00 +7.664061761364e-07
+BODY699_JCOEF(10) +0.000000000000e+00 +3.641907938036e-06
+BODY699_JCOEF(11) +0.000000000000e+00 -1.155312580876e-08
+BODY699_JCOEF(12) +0.000000000000e+00 -2.437044743424e-06
+BODY699_JCOEF(13) +0.000000000000e+00 -1.120617107914e-07
+BODY699_JCOEF(14) +0.000000000000e+00 -1.219002171382e-06
+BODY699_POLE_DEC(1) +8.353795895203e+01 +8.353796123271e+01
+BODY699_POLE_RA(1) +4.058386992768e+01 +4.058382745190e+01
+BODY6_GM +3.794058443092e+07 +3.794058443092e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2017-Aug-14 (published)
+Automated Process
+
+Applicable current Ephemeris = 170811R_SCPSE_17104_17117.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170507_269GF
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY601_GM +2.504168531168e+00 +2.502817739550e+00
+BODY602_GM +7.210642146844e+00 +7.211777492985e+00
+BODY603_GM +4.120886351384e+01 +4.120850186975e+01
+BODY604_GM +7.311578204704e+01 +7.311605842130e+01
+BODY605_GM +1.539457695021e+02 +1.539500870013e+02
+BODY606_GM +8.978136802358e+03 +8.978130958559e+03
+BODY607_GM +3.716779497898e-01 +3.713685396357e-01
+BODY608_GM +1.205406980395e+02 +1.204890219402e+02
+BODY609_GM +5.480161786740e-01 +5.527094668508e-01
+BODY699_GM +3.793120689522e+07 +3.793120689736e+07
+BODY699_JCOEF(2) +1.629055618674e-02 +1.629090771061e-02
+BODY699_JCOEF(4) -9.366851917272e-04 -9.338214217045e-04
+BODY699_JCOEF(6) +8.280896942075e-05 +8.325055333031e-05
+BODY699_POLE_DEC(1) +8.353795234454e+01 +8.353795895203e+01
+BODY699_POLE_RA(1) +4.058613626293e+01 +4.058386992768e+01
+BODY6_GM +3.794058447810e+07 +3.794058443092e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2017-Jul-25 (published)
+Automated Process
+
+Applicable current Ephemeris = 170720R_SCPSE_17061_17104.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170421_264T126
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY601_GM +2.504081870687e+00 +2.504168531168e+00
+BODY602_GM +7.210772616182e+00 +7.210642146844e+00
+BODY603_GM +4.120887177496e+01 +4.120886351384e+01
+BODY604_GM +7.311572411683e+01 +7.311578204704e+01
+BODY605_GM +1.539444655259e+02 +1.539457695021e+02
+BODY606_GM +8.978138039097e+03 +8.978136802358e+03
+BODY607_GM +3.716711120483e-01 +3.716779497898e-01
+BODY608_GM +1.205402752867e+02 +1.205406980395e+02
+BODY609_GM +5.505747898310e-01 +5.480161786740e-01
+BODY699_GM +3.793120741278e+07 +3.793120689522e+07
+BODY699_JCOEF(2) +1.629053435909e-02 +1.629055618674e-02
+BODY699_JCOEF(4) -9.373092086599e-04 -9.366851917272e-04
+BODY699_JCOEF(6) +7.540511809128e-05 +8.280896942075e-05
+BODY699_POLE_DEC(1) +8.353795237942e+01 +8.353795234454e+01
+BODY699_POLE_RA(1) +4.058613580121e+01 +4.058613626293e+01
+BODY6_GM +3.794058499768e+07 +3.794058447810e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2017-May-09 (published)
+Automated Process
+
+Applicable current Ephemeris = 170509R_SCPSE_16363_17061.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170423_254T126
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY601_GM +2.503522356085e+00 +2.504081870687e+00
+BODY602_GM +7.211029015103e+00 +7.210772616182e+00
+BODY603_GM +4.120902759359e+01 +4.120887177496e+01
+BODY604_GM +7.311571724805e+01 +7.311572411683e+01
+BODY605_GM +1.539445703042e+02 +1.539444655259e+02
+BODY606_GM +8.978134397405e+03 +8.978138039097e+03
+BODY607_GM +3.713890479231e-01 +3.716711120483e-01
+BODY608_GM +1.205778163298e+02 +1.205402752867e+02
+BODY609_GM +5.537034401022e-01 +5.505747898310e-01
+BODY699_GM +3.793120714676e+07 +3.793120741278e+07
+BODY699_JCOEF(2) +1.629088427394e-02 +1.629053435909e-02
+BODY699_JCOEF(4) -9.337629884495e-04 -9.373092086599e-04
+BODY699_JCOEF(6) +7.614739101940e-05 +7.540511809128e-05
+BODY699_POLE_DEC(1) +8.353795251735e+01 +8.353795237942e+01
+BODY699_POLE_RA(1) +4.058611775960e+01 +4.058613580121e+01
+BODY6_GM +3.794058476830e+07 +3.794058499768e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2017-Mar-27 (published)
+Automated Process
+
+Applicable current Ephemeris = 170323R_SCPSE_16329_16363.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 170105_251T126
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY601_GM +2.503458199931e+00 +2.503522356085e+00
+BODY602_GM +7.211216857327e+00 +7.211029015103e+00
+BODY603_GM +4.120862437003e+01 +4.120902759359e+01
+BODY604_GM +7.311579178242e+01 +7.311571724805e+01
+BODY605_GM +1.539424333799e+02 +1.539445703042e+02
+BODY606_GM +8.978137827385e+03 +8.978134397405e+03
+BODY607_GM +3.713969352243e-01 +3.713890479231e-01
+BODY608_GM +1.204756561849e+02 +1.205778163298e+02
+BODY609_GM +5.533648326496e-01 +5.537034401022e-01
+BODY699_GM +3.793120704269e+07 +3.793120714676e+07
+BODY699_JCOEF(2) +1.629098177296e-02 +1.629088427394e-02
+BODY699_JCOEF(4) -9.313711046683e-04 -9.337629884495e-04
+BODY699_JCOEF(6) +8.878694316872e-05 +7.614739101940e-05
+BODY699_POLE_DEC(1) +8.353809821829e+01 +8.353795251735e+01
+BODY699_POLE_RA(1) +4.058409635443e+01 +4.058611775960e+01
+BODY6_GM +3.794058456266e+07 +3.794058476830e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2017-Mar-20 (published)
+Automated Process
+
+Applicable current Ephemeris = 170315R_SCPSE_16310_16329.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 161202_1_249T125
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY601_GM +2.503429819565e+00 +2.503458199931e+00
+BODY602_GM +7.211263331665e+00 +7.211216857327e+00
+BODY603_GM +4.120807865783e+01 +4.120862437003e+01
+BODY604_GM +7.311565440283e+01 +7.311579178242e+01
+BODY605_GM +1.539422768490e+02 +1.539424333799e+02
+BODY606_GM +8.978138421746e+03 +8.978137827385e+03
+BODY607_GM +3.713250481181e-01 +3.713969352243e-01
+BODY608_GM +1.205443628610e+02 +1.204756561849e+02
+BODY609_GM +5.541420472080e-01 +5.533648326496e-01
+BODY699_GM +3.793120752586e+07 +3.793120704269e+07
+BODY699_JCOEF(2) +1.629105265841e-02 +1.629098177296e-02
+BODY699_JCOEF(4) -9.307532830389e-04 -9.313711046683e-04
+BODY699_JCOEF(6) +8.821178266851e-05 +8.878694316872e-05
+BODY699_POLE_DEC(1) +8.353813668628e+01 +8.353809821829e+01
+BODY699_POLE_RA(1) +4.058322932675e+01 +4.058409635443e+01
+BODY6_GM +3.794058511503e+07 +3.794058456266e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2017-Mar-01 (published)
+Automated Process
+
+Applicable current Ephemeris = 170301R_SCPSE_16282_16310.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 161116_246T124
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY601_GM +2.503458199931e+00 +2.503429819565e+00
+BODY602_GM +7.211438886407e+00 +7.211263331665e+00
+BODY603_GM +4.120859857122e+01 +4.120807865783e+01
+BODY604_GM +7.311579502939e+01 +7.311565440283e+01
+BODY605_GM +1.539421951727e+02 +1.539422768490e+02
+BODY606_GM +8.978136177723e+03 +8.978138421746e+03
+BODY607_GM +3.713209987014e-01 +3.713250481181e-01
+BODY608_GM +1.205222816678e+02 +1.205443628610e+02
+BODY609_GM +5.540640303818e-01 +5.541420472080e-01
+BODY699_GM +3.793120731501e+07 +3.793120752586e+07
+BODY699_JCOEF(2) +1.629113494099e-02 +1.629105265841e-02
+BODY699_JCOEF(4) -9.300312200208e-04 -9.307532830389e-04
+BODY699_JCOEF(6) +8.990159020464e-05 +8.821178266851e-05
+BODY699_POLE_DEC(1) +8.353813708379e+01 +8.353813668628e+01
+BODY699_POLE_RA(1) +4.058321003407e+01 +4.058322932675e+01
+BODY6_GM +3.794058488055e+07 +3.794058511503e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2017-Feb-28 (published)
+Automated Process
+
+Applicable current Ephemeris = 170228R_SCPSE_16262_16282.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 161019_244T124
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY602_GM +7.211357133168e+00 +7.211438886407e+00
+BODY603_GM +4.120838587263e+01 +4.120859857122e+01
+BODY604_GM +7.311580066353e+01 +7.311579502939e+01
+BODY605_GM +1.539433188040e+02 +1.539421951727e+02
+BODY606_CCOEF(3) +1.029534469634e-05 +1.046258225998e-05
+BODY606_GM +8.978132593546e+03 +8.978136177723e+03
+BODY606_JCOEF(2) +3.546380755853e-05 +3.341349498806e-05
+BODY606_SCOEF(3) +2.322168281218e-07 +3.915574411619e-07
+BODY607_GM +3.714099091721e-01 +3.713209987014e-01
+BODY608_GM +1.204848222541e+02 +1.205222816678e+02
+BODY609_GM +5.553928427732e-01 +5.540640303818e-01
+BODY699_GM +3.793120718935e+07 +3.793120731501e+07
+BODY699_JCOEF(2) +1.629106986990e-02 +1.629113494099e-02
+BODY699_JCOEF(4) -9.307706047161e-04 -9.300312200208e-04
+BODY699_JCOEF(6) +8.839867540967e-05 +8.990159020464e-05
+BODY699_POLE_DEC(1) +8.353812798747e+01 +8.353813708379e+01
+BODY699_POLE_RA(1) +4.058378023140e+01 +4.058321003407e+01
+BODY6_GM +3.794058471609e+07 +3.794058488055e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2016-Dec-15 (published)
+Automated Process
+
+Applicable current Ephemeris = 161214R_SCPSE_16217_16262.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160926_240T123
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY602_GM +7.211402764994e+00 +7.211357133168e+00
+BODY603_GM +4.120828173203e+01 +4.120838587263e+01
+BODY604_GM +7.311578550158e+01 +7.311580066353e+01
+BODY605_GM +1.539427209498e+02 +1.539433188040e+02
+BODY606_CCOEF(3) +1.035135894910e-05 +1.029534469634e-05
+BODY606_GM +8.978131430064e+03 +8.978132593546e+03
+BODY606_JCOEF(2) +3.453993520201e-05 +3.546380755853e-05
+BODY606_SCOEF(3) -1.328779671011e-08 +2.322168281218e-07
+BODY607_GM +3.713269422707e-01 +3.714099091721e-01
+BODY608_GM +1.205497924859e+02 +1.204848222541e+02
+BODY609_GM +5.540358787579e-01 +5.553928427732e-01
+BODY699_GM +3.793120736644e+07 +3.793120718935e+07
+BODY699_JCOEF(2) +1.629111982374e-02 +1.629106986990e-02
+BODY699_JCOEF(4) -9.300983689047e-04 -9.307706047161e-04
+BODY699_JCOEF(6) +9.027570812799e-05 +8.839867540967e-05
+BODY699_POLE_DEC(1) +8.353813363065e+01 +8.353812798747e+01
+BODY699_POLE_RA(1) +4.058357784587e+01 +4.058378023140e+01
+BODY6_GM +3.794058495488e+07 +3.794058471609e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2016-Dec-12 (published)
+Automated Process
+
+Applicable current Ephemeris = 161208R_SCPSE_16201_16217.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160810_1_239T122
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY602_GM +7.211703581579e+00 +7.211402764994e+00
+BODY603_GM +4.120843806343e+01 +4.120828173203e+01
+BODY604_GM +7.311584179385e+01 +7.311578550158e+01
+BODY605_GM +1.539428752140e+02 +1.539427209498e+02
+BODY606_CCOEF(3) +1.046258225998e-05 +1.035135894910e-05
+BODY606_GM +8.978134655522e+03 +8.978131430064e+03
+BODY606_JCOEF(2) +3.341349498806e-05 +3.453993520201e-05
+BODY606_SCOEF(3) +3.915574411619e-07 -1.328779671011e-08
+BODY607_GM +3.713075782150e-01 +3.713269422707e-01
+BODY608_GM +1.204605259223e+02 +1.205497924859e+02
+BODY609_GM +5.527880806141e-01 +5.540358787579e-01
+BODY699_GM +3.793120695506e+07 +3.793120736644e+07
+BODY699_JCOEF(2) +1.629112234313e-02 +1.629111982374e-02
+BODY699_JCOEF(4) -9.297728263461e-04 -9.300983689047e-04
+BODY699_JCOEF(6) +9.114243475253e-05 +9.027570812799e-05
+BODY699_POLE_DEC(1) +8.353815470019e+01 +8.353813363065e+01
+BODY699_POLE_RA(1) +4.058303844662e+01 +4.058357784587e+01
+BODY6_GM +3.794058445686e+07 +3.794058495488e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2016-Nov-17 (published)
+Automated Process
+
+Applicable current Ephemeris = 161117R_SCPSE_16146_16201.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160724_237T121
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY601_GM +2.503448868242e+00 +2.503458199931e+00
+BODY602_GM +7.211325894096e+00 +7.211703581579e+00
+BODY603_GM +4.120847806547e+01 +4.120843806343e+01
+BODY604_GM +7.311570926715e+01 +7.311584179385e+01
+BODY605_GM +1.539423683108e+02 +1.539428752140e+02
+BODY606_GM +8.978134339426e+03 +8.978134655522e+03
+BODY607_GM +3.713244675027e-01 +3.713075782150e-01
+BODY608_GM +1.205322393914e+02 +1.204605259223e+02
+BODY609_GM +5.543646426583e-01 +5.527880806141e-01
+BODY699_GM +3.793120700538e+07 +3.793120695506e+07
+BODY699_JCOEF(2) +1.629108871238e-02 +1.629112234313e-02
+BODY699_JCOEF(4) -9.304882330717e-04 -9.297728263461e-04
+BODY699_JCOEF(6) +8.885094992101e-05 +9.114243475253e-05
+BODY699_POLE_DEC(1) +8.353800243639e+01 +8.353815470019e+01
+BODY699_POLE_RA(1) +4.058439605750e+01 +4.058303844662e+01
+BODY6_GM +3.794058457925e+07 +3.794058445686e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2016-Aug-26 (published)
+Automated Process
+
+Applicable current Ephemeris = 160725R_SCPSE_16115_16146.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160606_236T120
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY601_GM +2.503458199931e+00 +2.503448868242e+00
+BODY602_GM +7.211471999477e+00 +7.211325894096e+00
+BODY603_GM +4.120844755642e+01 +4.120847806547e+01
+BODY604_GM +7.311575497245e+01 +7.311570926715e+01
+BODY605_GM +1.539425188714e+02 +1.539423683108e+02
+BODY606_GM +8.978136440086e+03 +8.978134339426e+03
+BODY607_GM +3.712817316551e-01 +3.713244675027e-01
+BODY608_GM +1.205098029896e+02 +1.205322393914e+02
+BODY609_GM +5.531710748936e-01 +5.543646426583e-01
+BODY699_GM +3.793120705906e+07 +3.793120700538e+07
+BODY699_JCOEF(2) +1.629111447570e-02 +1.629108871238e-02
+BODY699_JCOEF(4) -9.301241563302e-04 -9.304882330717e-04
+BODY699_JCOEF(6) +8.990943846005e-05 +8.885094992101e-05
+BODY699_POLE_DEC(1) +8.353805038622e+01 +8.353800243639e+01
+BODY699_POLE_RA(1) +4.058378246620e+01 +4.058439605750e+01
+BODY6_GM +3.794058461162e+07 +3.794058457925e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2016-Jul-20 (published)
+Automated Process
+
+Applicable current Ephemeris = 160718R_SCPSE_16088_16115.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160504_235T119
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY602_GM +7.211185066510e+00 +7.211471999477e+00
+BODY603_GM +4.120856508659e+01 +4.120844755642e+01
+BODY604_GM +7.311574218947e+01 +7.311575497245e+01
+BODY605_GM +1.539419035933e+02 +1.539425188714e+02
+BODY606_GM +8.978137030984e+03 +8.978136440086e+03
+BODY607_GM +3.712085754472e-01 +3.712817316551e-01
+BODY608_GM +1.205095752389e+02 +1.205098029896e+02
+BODY609_GM +5.532371285376e-01 +5.531710748936e-01
+BODY699_GM +3.793120723494e+07 +3.793120705906e+07
+BODY699_JCOEF(2) +1.629111964057e-02 +1.629111447570e-02
+BODY699_JCOEF(4) -9.305945887740e-04 -9.301241563302e-04
+BODY699_JCOEF(6) +8.872819837009e-05 +8.990943846005e-05
+BODY699_POLE_DEC(1) +8.353776999027e+01 +8.353805038622e+01
+BODY699_POLE_RA(1) +4.058252338374e+01 +4.058378246620e+01
+BODY6_GM +3.794058478705e+07 +3.794058461162e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2016-Jun-08 (published)
+Automated Process
+
+Applicable current Ephemeris = 160608R_SCPSE_16041_16088.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160405_233T118
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY603_GM +4.120856508659e+01 +4.120856508659e+01
+BODY604_GM +7.311574218947e+01 +7.311574218947e+01
+BODY605_GM +1.539419035933e+02 +1.539419035933e+02
+BODY606_GM +8.978137030984e+03 +8.978137030984e+03
+BODY608_GM +1.205095752389e+02 +1.205095752389e+02
+BODY699_GM +3.793120723494e+07 +3.793120723494e+07
+BODY699_POLE_DEC(1) +8.353776999027e+01 +8.353776999027e+01
+BODY699_POLE_RA(1) +4.058252338374e+01 +4.058252338374e+01
+BODY6_GM +3.794058478705e+07 +3.794058478705e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2016-May-20 (published)
+Automated Process
+
+Applicable current Ephemeris = 160519R_SCPSE_16025_16041.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160218_232T117
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY603_GM +4.120856508659e+01 +4.120856508659e+01
+BODY604_GM +7.311574218947e+01 +7.311574218947e+01
+BODY605_GM +1.539419035933e+02 +1.539419035933e+02
+BODY606_GM +8.978137030984e+03 +8.978137030984e+03
+BODY608_GM +1.205095752389e+02 +1.205095752389e+02
+BODY699_GM +3.793120723494e+07 +3.793120723494e+07
+BODY699_POLE_DEC(1) +8.353776999027e+01 +8.353776999027e+01
+BODY699_POLE_RA(1) +4.058252338374e+01 +4.058252338374e+01
+BODY6_GM +3.794058478705e+07 +3.794058478705e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2016-Apr-13 (published)
+Automated Process
+
+Applicable current Ephemeris = 160413R_SCPSE_16007_16025.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160203_231T116
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY603_GM +4.120856508659e+01 +4.120856508659e+01
+BODY604_GM +7.311574218947e+01 +7.311574218947e+01
+BODY605_GM +1.539419035933e+02 +1.539419035933e+02
+BODY606_GM +8.978137030984e+03 +8.978137030984e+03
+BODY608_GM +1.205095752389e+02 +1.205095752389e+02
+BODY699_GM +3.793120723494e+07 +3.793120723494e+07
+BODY699_POLE_DEC(1) +8.353776999027e+01 +8.353776999027e+01
+BODY699_POLE_RA(1) +4.058252338374e+01 +4.058252338374e+01
+BODY6_GM +3.794058478705e+07 +3.794058478705e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2016-Mar-30 (published)
+Automated Process
+
+Applicable current Ephemeris = 160330R_SCPSE_15347_16007.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 160118_229T115
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400419e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800117136e+03 +4.902800117136e+03
+BODY399_GM +3.986004353851e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641334e+08 +1.267127641334e+08
+BODY603_GM +4.120856508659e+01 +4.120856508659e+01
+BODY604_GM +7.311574218947e+01 +7.311574218947e+01
+BODY605_GM +1.539419035933e+02 +1.539419035933e+02
+BODY606_GM +8.978137030984e+03 +8.978137030984e+03
+BODY608_GM +1.205095752389e+02 +1.205095752389e+02
+BODY699_GM +3.793120723494e+07 +3.793120723494e+07
+BODY699_POLE_DEC(1) +8.353776999027e+01 +8.353776999027e+01
+BODY699_POLE_RA(1) +4.058252338374e+01 +4.058252338374e+01
+BODY6_GM +3.794058478705e+07 +3.794058478705e+07
+BODY7_GM +5.794556465752e+06 +5.794556465752e+06
+
+2016-Mar-24 (published)
+Automated Process
+
+Applicable current Ephemeris = 160323R_SCPSE_15310_15347.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 151222_226E22
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327132332639e+11 +1.327124400419e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800117136e+03
+BODY399_GM +3.986004354361e+05 +3.986004353851e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY5_GM +1.267127641000e+08 +1.267127641334e+08
+BODY601_GM +2.503523763302e+00 +2.503458199931e+00
+BODY602_CCOEF(3) +1.229502218138e-03 +1.549800000000e-03
+BODY602_GM +7.211176947682e+00 +7.211185066510e+00
+BODY602_JCOEF(2) +6.055594538600e-03 +5.435200000000e-03
+BODY603_GM +4.121082693902e+01 +4.120856508659e+01
+BODY604_CCOEF(3) +3.858211235156e-04 +3.651494811184e-04
+BODY604_GM +7.311671566552e+01 +7.311574218947e+01
+BODY604_JCOEF(2) +1.294156214342e-03 +1.436865258838e-03
+BODY605_CCOEF(3) +2.548409590520e-04 +2.366835799998e-04
+BODY605_GM +1.539427914458e+02 +1.539419035933e+02
+BODY605_JCOEF(2) +8.496490377952e-04 +9.496088222042e-04
+BODY606_CCOEF(3) +9.968773423301e-06 +1.046258225998e-05
+BODY606_GM +8.978137900462e+03 +8.978137030984e+03
+BODY606_JCOEF(2) +3.267536300237e-05 +3.341349498806e-05
+BODY606_SCOEF(3) +2.617518846598e-07 +3.915574411619e-07
+BODY607_GM +3.718569049967e-01 +3.712085754472e-01
+BODY608_GM +1.205076319121e+02 +1.205095752389e+02
+BODY609_GM +5.529409232812e-01 +5.532371285376e-01
+BODY699_GM +3.793120738834e+07 +3.793120723494e+07
+BODY699_JCOEF(2) +1.629070151853e-02 +1.629111964057e-02
+BODY699_JCOEF(4) -9.340278799551e-04 -9.305945887740e-04
+BODY699_JCOEF(6) +8.929667654105e-05 +8.872819837009e-05
+BODY699_POLE_DEC(1) +8.353760844394e+01 +8.353776999027e+01
+BODY699_POLE_DEC(2) -5.382911302100e-03 -7.584170141686e-03
+BODY699_POLE_RA(1) +4.058262053545e+01 +4.058252338374e+01
+BODY699_POLE_RA(2) -2.715273573990e-02 -3.099714786917e-02
+BODY6_GM +3.794058494370e+07 +3.794058478705e+07
+BODY7_GM +5.794556400000e+06 +5.794556465752e+06
+
+2016-Jan-29 (published)
+Automated Process
+
+Applicable current Ephemeris = 160129R_SCPSE_15295_15310.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 151115_225T114
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY601_GM +2.503524000000e+00 +2.503523763302e+00
+BODY602_GM +7.211140136327e+00 +7.211176947682e+00
+BODY603_GM +4.121081982359e+01 +4.121082693902e+01
+BODY604_GM +7.311672244985e+01 +7.311671566552e+01
+BODY605_GM +1.539427790614e+02 +1.539427914458e+02
+BODY606_GM +8.978137874425e+03 +8.978137900462e+03
+BODY607_GM +3.718562949332e-01 +3.718569049967e-01
+BODY608_GM +1.205073858074e+02 +1.205076319121e+02
+BODY609_GM +5.529278065380e-01 +5.529409232812e-01
+BODY699_GM +3.793120738517e+07 +3.793120738834e+07
+BODY699_JCOEF(2) +1.629070068016e-02 +1.629070151853e-02
+BODY699_JCOEF(4) -9.340207297950e-04 -9.340278799551e-04
+BODY699_JCOEF(6) +8.933577374593e-05 +8.929667654105e-05
+BODY699_POLE_DEC(1) +8.353760430989e+01 +8.353760844394e+01
+BODY699_POLE_RA(1) +4.058259729361e+01 +4.058262053545e+01
+BODY6_GM +3.794058494020e+07 +3.794058494370e+07
+
+2015-Nov-16 (published)
+Automated Process
+
+Applicable current Ephemeris = 151116R_SCPSE_15280_15295.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 151030_224E21
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY604_GM +7.311672244985e+01 +7.311672244985e+01
+BODY605_GM +1.539427790614e+02 +1.539427790614e+02
+BODY606_GM +8.978137874425e+03 +8.978137874425e+03
+BODY608_GM +1.205073858074e+02 +1.205073858074e+02
+BODY699_GM +3.793120738517e+07 +3.793120738517e+07
+BODY699_POLE_DEC(1) +8.353760430989e+01 +8.353760430989e+01
+BODY699_POLE_RA(1) +4.058259729361e+01 +4.058259729361e+01
+BODY6_GM +3.794058494020e+07 +3.794058494020e+07
+
+2015-Nov-13 (published)
+Automated Process
+
+Applicable current Ephemeris = 151112R_SCPSE_15261_15280.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 151018_223E20
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY601_GM +2.503525621473e+00 +2.503524000000e+00
+BODY602_GM +7.211277847563e+00 +7.211140136327e+00
+BODY603_GM +4.121092050918e+01 +4.121081982359e+01
+BODY604_CCOEF(3) +4.096610907190e-04 +3.858211235156e-04
+BODY604_GM +7.311659144214e+01 +7.311672244985e+01
+BODY604_JCOEF(2) +1.158244618125e-03 +1.294156214342e-03
+BODY605_GM +1.539428611851e+02 +1.539427790614e+02
+BODY606_GM +8.978137957021e+03 +8.978137874425e+03
+BODY607_GM +3.718596409938e-01 +3.718562949332e-01
+BODY608_GM +1.205088668399e+02 +1.205073858074e+02
+BODY609_GM +5.529684179873e-01 +5.529278065380e-01
+BODY699_GM +3.793120740439e+07 +3.793120738517e+07
+BODY699_JCOEF(2) +1.629070657850e-02 +1.629070068016e-02
+BODY699_JCOEF(4) -9.340015407952e-04 -9.340207297950e-04
+BODY699_JCOEF(6) +8.967524235871e-05 +8.933577374593e-05
+BODY699_POLE_DEC(1) +8.353763029055e+01 +8.353760430989e+01
+BODY699_POLE_RA(1) +4.058273005421e+01 +4.058259729361e+01
+BODY6_GM +3.794058496122e+07 +3.794058494020e+07
+
+2015-Nov-02 (published)
+Automated Process
+
+Applicable current Ephemeris = 151102R_SCPSE_15222_15261.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 151001_221T113
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY601_GM +2.503526767032e+00 +2.503525621473e+00
+BODY602_GM +7.211670352602e+00 +7.211277847563e+00
+BODY603_GM +4.121092931739e+01 +4.121092050918e+01
+BODY604_CCOEF(3) +4.006810364134e-04 +4.096610907190e-04
+BODY604_GM +7.311657574990e+01 +7.311659144214e+01
+BODY604_JCOEF(2) +1.216580827110e-03 +1.158244618125e-03
+BODY605_GM +1.539427263983e+02 +1.539428611851e+02
+BODY606_GM +8.978138400547e+03 +8.978137957021e+03
+BODY607_GM +3.718604278380e-01 +3.718596409938e-01
+BODY608_GM +1.205086493624e+02 +1.205088668399e+02
+BODY609_GM +5.529652914648e-01 +5.529684179873e-01
+BODY699_GM +3.793120740278e+07 +3.793120740439e+07
+BODY699_JCOEF(2) +1.629070431501e-02 +1.629070657850e-02
+BODY699_JCOEF(4) -9.340751123226e-04 -9.340015407952e-04
+BODY699_JCOEF(6) +9.105902884329e-05 +8.967524235871e-05
+BODY699_POLE_DEC(1) +8.353762187255e+01 +8.353763029055e+01
+BODY699_POLE_RA(1) +4.058273932144e+01 +4.058273005421e+01
+BODY6_GM +3.794058496009e+07 +3.794058496122e+07
+
+2015-Oct-14 (published)
+Automated Process
+
+Applicable current Ephemeris = 151014R_SCPSE_15180_15222.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 150819_219D5
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY601_GM +2.503525907247e+00 +2.503526767032e+00
+BODY602_GM +7.211467207431e+00 +7.211670352602e+00
+BODY603_GM +4.121094716824e+01 +4.121092931739e+01
+BODY604_CCOEF(3) +3.900331957120e-04 +4.006810364134e-04
+BODY604_GM +7.311609968736e+01 +7.311657574990e+01
+BODY604_JCOEF(2) +1.318240936309e-03 +1.216580827110e-03
+BODY605_GM +1.539427595960e+02 +1.539427263983e+02
+BODY606_GM +8.978138174255e+03 +8.978138400547e+03
+BODY607_GM +3.718568794227e-01 +3.718604278380e-01
+BODY608_GM +1.205072126963e+02 +1.205086493624e+02
+BODY609_GM +5.528208458989e-01 +5.529652914648e-01
+BODY699_GM +3.793120738081e+07 +3.793120740278e+07
+BODY699_JCOEF(2) +1.629070068016e-02 +1.629070431501e-02
+BODY699_JCOEF(4) -9.340207297950e-04 -9.340751123226e-04
+BODY699_JCOEF(6) +8.933577374593e-05 +9.105902884329e-05
+BODY699_POLE_DEC(1) +8.353760430989e+01 +8.353762187255e+01
+BODY699_POLE_RA(1) +4.058259729361e+01 +4.058273932144e+01
+BODY6_GM +3.794058493568e+07 +3.794058496009e+07
+
+2015-Oct-13 (published)
+Automated Process
+
+Applicable current Ephemeris = 151013R_SCPSE_15161_15180.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 150709_218T112
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY601_GM +2.503514004827e+00 +2.503525907247e+00
+BODY602_GM +7.211311315180e+00 +7.211467207431e+00
+BODY603_GM +4.121081532906e+01 +4.121094716824e+01
+BODY604_CCOEF(3) +3.858211235156e-04 +3.900331957120e-04
+BODY604_GM +7.311665769360e+01 +7.311609968736e+01
+BODY604_JCOEF(2) +1.294156214342e-03 +1.318240936309e-03
+BODY605_GM +1.539425601163e+02 +1.539427595960e+02
+BODY606_GM +8.978136872551e+03 +8.978138174255e+03
+BODY607_GM +3.718576178624e-01 +3.718568794227e-01
+BODY608_GM +1.205072036005e+02 +1.205072126963e+02
+BODY609_GM +5.524056306757e-01 +5.528208458989e-01
+BODY699_GM +3.793120737315e+07 +3.793120738081e+07
+BODY699_POLE_DEC(1) +8.353760430989e+01 +8.353760430989e+01
+BODY699_POLE_RA(1) +4.058259729361e+01 +4.058259729361e+01
+BODY6_GM +3.794058492635e+07 +3.794058493568e+07
+
+2015-Oct-12 (published)
+Automated Process
+
+Applicable current Ephemeris = 151009R_SCPSE_15116_15161.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 150618_216D4
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY601_GM +2.503524000000e+00 +2.503514004827e+00
+BODY602_GM +7.211140136327e+00 +7.211311315180e+00
+BODY603_GM +4.121081982359e+01 +4.121081532906e+01
+BODY604_GM +7.311672244985e+01 +7.311665769360e+01
+BODY605_GM +1.539427790614e+02 +1.539425601163e+02
+BODY606_CCOEF(3) +1.026987704003e-05 +9.968773423301e-06
+BODY606_GM +8.978137874425e+03 +8.978136872551e+03
+BODY606_JCOEF(2) +2.836955902317e-05 +3.267536300237e-05
+BODY606_SCOEF(3) +1.626257999633e-07 +2.617518846598e-07
+BODY607_GM +3.718562949332e-01 +3.718576178624e-01
+BODY608_GM +1.205073858074e+02 +1.205072036005e+02
+BODY609_GM +5.529278065380e-01 +5.524056306757e-01
+BODY699_GM +3.793120738517e+07 +3.793120737315e+07
+BODY699_POLE_DEC(1) +8.353760430989e+01 +8.353760430989e+01
+BODY699_POLE_RA(1) +4.058259729361e+01 +4.058259729361e+01
+BODY6_GM +3.794058494020e+07 +3.794058492635e+07
+
+2015-Aug-28 (published)
+Automated Process
+
+Applicable current Ephemeris = 150828R_SCPSE_15066_15116.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 150507_214T111
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY601_GM +2.503451908819e+00 +2.503524000000e+00
+BODY602_CCOEF(3) +1.549800000000e-03 +1.229502218138e-03
+BODY602_GM +7.211233789589e+00 +7.211140136327e+00
+BODY602_JCOEF(2) +5.435200000000e-03 +6.055594538600e-03
+BODY603_GM +4.120932250035e+01 +4.121081982359e+01
+BODY604_CCOEF(3) +4.042630633858e-04 +3.858211235156e-04
+BODY604_GM +7.311592012061e+01 +7.311672244985e+01
+BODY604_JCOEF(2) +1.092458014279e-03 +1.294156214342e-03
+BODY605_CCOEF(3) +2.209984559363e-04 +2.548409590520e-04
+BODY605_GM +1.539439497209e+02 +1.539427790614e+02
+BODY605_JCOEF(2) +9.688723938907e-04 +8.496490377952e-04
+BODY606_CCOEF(3) +1.036457861987e-05 +1.026987704003e-05
+BODY606_GM +8.978138015653e+03 +8.978137874425e+03
+BODY606_JCOEF(2) +3.393754680271e-05 +2.836955902317e-05
+BODY606_SCOEF(3) +3.214252359006e-07 +1.626257999633e-07
+BODY607_GM +3.715249700202e-01 +3.718562949332e-01
+BODY608_GM +1.205006955067e+02 +1.205073858074e+02
+BODY609_GM +5.539027499377e-01 +5.529278065380e-01
+BODY699_GM +3.793120683754e+07 +3.793120738517e+07
+BODY699_JCOEF(2) +1.629116884116e-02 +1.629070068016e-02
+BODY699_JCOEF(4) -9.304692658710e-04 -9.340207297950e-04
+BODY699_JCOEF(6) +9.120788665605e-05 +8.933577374593e-05
+BODY699_POLE_DEC(1) +8.353741023979e+01 +8.353760430989e+01
+BODY699_POLE_DEC(2) -3.198913258906e-03 -5.382911302100e-03
+BODY699_POLE_RA(1) +4.058445039396e+01 +4.058259729361e+01
+BODY699_POLE_RA(2) -4.463634918787e-02 -2.715273573990e-02
+BODY6_GM +3.794058438556e+07 +3.794058494020e+07
+
+2015-Aug-03 (published)
+Automated Process
+
+Applicable current Ephemeris = 150803R_SCPSE_15033_15066.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 150318_213T110
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY601_GM +2.503524000000e+00 +2.503451908819e+00
+BODY602_CCOEF(3) +1.229502218138e-03 +1.549800000000e-03
+BODY602_GM +7.211454165826e+00 +7.211233789589e+00
+BODY602_JCOEF(2) +6.055594538600e-03 +5.435200000000e-03
+BODY603_GM +4.121107782641e+01 +4.120932250035e+01
+BODY604_CCOEF(3) +3.858211235156e-04 +4.042630633858e-04
+BODY604_GM +7.311636648732e+01 +7.311592012061e+01
+BODY604_JCOEF(2) +1.294156214342e-03 +1.092458014279e-03
+BODY605_CCOEF(3) +2.548409590520e-04 +2.209984559363e-04
+BODY605_GM +1.539424643535e+02 +1.539439497209e+02
+BODY605_JCOEF(2) +8.496490377952e-04 +9.688723938907e-04
+BODY606_CCOEF(3) +9.968773423301e-06 +1.036457861987e-05
+BODY606_GM +8.978138376543e+03 +8.978138015653e+03
+BODY606_JCOEF(2) +3.267536300237e-05 +3.393754680271e-05
+BODY606_SCOEF(3) +2.617518846598e-07 +3.214252359006e-07
+BODY607_GM +3.718742808951e-01 +3.715249700202e-01
+BODY608_GM +1.205120887033e+02 +1.205006955067e+02
+BODY609_GM +5.528989950538e-01 +5.539027499377e-01
+BODY699_GM +3.793120747608e+07 +3.793120683754e+07
+BODY699_JCOEF(2) +1.629069817036e-02 +1.629116884116e-02
+BODY699_JCOEF(4) -9.343344679290e-04 -9.304692658710e-04
+BODY699_JCOEF(6) +9.003499615840e-05 +9.120788665605e-05
+BODY699_POLE_DEC(1) +8.353763861569e+01 +8.353741023979e+01
+BODY699_POLE_DEC(2) -6.782331809658e-03 -3.198913258906e-03
+BODY699_POLE_RA(1) +4.058271311699e+01 +4.058445039396e+01
+BODY699_POLE_RA(2) -5.744235301067e-02 -4.463634918787e-02
+BODY6_GM +3.794058503620e+07 +3.794058438556e+07
+BODY7_GM +5.794548600000e+06 +5.794556400000e+06
+
+2015-Jun-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 150609R_SCPSE_14365_15033.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 150214_212T109
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY603_GM +4.121107782641e+01 +4.121107782641e+01
+BODY604_GM +7.311636648732e+01 +7.311636648732e+01
+BODY605_GM +1.539424643535e+02 +1.539424643535e+02
+BODY606_GM +8.978138376543e+03 +8.978138376543e+03
+BODY608_GM +1.205120887033e+02 +1.205120887033e+02
+BODY699_GM +3.793120747608e+07 +3.793120747608e+07
+BODY699_POLE_RA(1) +4.058271311699e+01 +4.058271311699e+01
+BODY6_GM +3.794058503620e+07 +3.794058503620e+07
+
+2015-Mar-04 (published)
+Automated Process
+
+Applicable current Ephemeris = 150304R_SCPSE_14283_14327.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 141210_210T107
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY603_GM +4.121107782641e+01 +4.121107782641e+01
+BODY604_GM +7.311636648732e+01 +7.311636648732e+01
+BODY605_GM +1.539424643535e+02 +1.539424643535e+02
+BODY606_GM +8.978138376543e+03 +8.978138376543e+03
+BODY608_GM +1.205120887033e+02 +1.205120887033e+02
+BODY699_GM +3.793120747608e+07 +3.793120747608e+07
+BODY699_POLE_RA(1) +4.058271311699e+01 +4.058271311699e+01
+BODY6_GM +3.794058503620e+07 +3.794058503620e+07
+
+2015-Jan-22 (published)
+Automated Process
+
+Applicable current Ephemeris = 150122R_SCPSE_14251_14283.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 141023_1_209T106
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY603_GM +4.121107782641e+01 +4.121107782641e+01
+BODY604_GM +7.311636648732e+01 +7.311636648732e+01
+BODY605_GM +1.539424643535e+02 +1.539424643535e+02
+BODY606_GM +8.978138376543e+03 +8.978138376543e+03
+BODY608_GM +1.205120887033e+02 +1.205120887033e+02
+BODY699_GM +3.793120747608e+07 +3.793120747608e+07
+BODY699_POLE_RA(1) +4.058271311699e+01 +4.058271311699e+01
+BODY6_GM +3.794058503620e+07 +3.794058503620e+07
+
+2015-Jan-08 (published)
+Automated Process
+
+Applicable current Ephemeris = 150107R_SCPSE_14222_14251.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 140923_1_208T105
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY601_GM +2.503522884662e+00 +2.503524000000e+00
+BODY602_GM +7.211292085480e+00 +7.211454165826e+00
+BODY603_GM +4.121117207701e+01 +4.121107782641e+01
+BODY604_GM +7.311635322923e+01 +7.311636648732e+01
+BODY605_GM +1.539422045545e+02 +1.539424643535e+02
+BODY606_GM +8.978138845307e+03 +8.978138376543e+03
+BODY607_GM +3.718791714192e-01 +3.718742808951e-01
+BODY608_GM +1.205134781724e+02 +1.205120887033e+02
+BODY609_GM +5.531110414633e-01 +5.528989950538e-01
+BODY699_GM +3.793120749865e+07 +3.793120747608e+07
+BODY699_JCOEF(2) +1.629069546360e-02 +1.629069817036e-02
+BODY699_JCOEF(4) -9.343510777890e-04 -9.343344679290e-04
+BODY699_JCOEF(6) +8.959557103495e-05 +9.003499615840e-05
+BODY699_POLE_DEC(1) +8.353764728832e+01 +8.353763861569e+01
+BODY699_POLE_DEC(2) -5.841335281700e-03 -6.782331809658e-03
+BODY699_POLE_RA(1) +4.058270059426e+01 +4.058271311699e+01
+BODY699_POLE_RA(2) -2.896108850840e-02 -5.744235301067e-02
+BODY6_GM +3.794058506051e+07 +3.794058503620e+07
+
+2014-Nov-12 (published)
+Automated Process
+
+Applicable current Ephemeris = 141107R_SCPSE_14187_14222.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 140820_207T104
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY603_GM +4.121117207701e+01 +4.121117207701e+01
+BODY604_GM +7.311635322923e+01 +7.311635322923e+01
+BODY605_GM +1.539422045545e+02 +1.539422045545e+02
+BODY606_GM +8.978138845307e+03 +8.978138845307e+03
+BODY608_GM +1.205134781724e+02 +1.205134781724e+02
+BODY699_GM +3.793120749865e+07 +3.793120749865e+07
+BODY699_POLE_DEC(1) +8.353764728832e+01 +8.353764728832e+01
+BODY699_POLE_RA(1) +4.058270059426e+01 +4.058270059426e+01
+BODY6_GM +3.794058506051e+07 +3.794058506051e+07
+
+2014-Sep-09 (published)
+Automated Process
+
+Applicable current Ephemeris = 140909R_SCPSE_14118_14156.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 140621_205T102
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800066164e+03 +4.902800066164e+03
+BODY399_GM +3.986004354361e+05 +3.986004354361e+05
+BODY3_GM +4.035032355023e+05 +4.035032355023e+05
+BODY603_GM +4.121117207701e+01 +4.121117207701e+01
+BODY604_GM +7.311635322923e+01 +7.311635322923e+01
+BODY605_GM +1.539422045545e+02 +1.539422045545e+02
+BODY606_GM +8.978138845307e+03 +8.978138845307e+03
+BODY608_GM +1.205134781724e+02 +1.205134781724e+02
+BODY699_GM +3.793120749865e+07 +3.793120749865e+07
+BODY699_POLE_DEC(1) +8.353764728832e+01 +8.353764728832e+01
+BODY699_POLE_RA(1) +4.058270059426e+01 +4.058270059426e+01
+BODY6_GM +3.794058506051e+07 +3.794058506051e+07
+
+2014-Sep-08 (published)
+Automated Process
+
+Applicable current Ephemeris = 140907R_SCPSE_14083_14118.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 140520_204T101
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800066164e+03
+BODY399_GM +3.986004362961e+05 +3.986004354361e+05
+BODY3_GM +4.035032417380e+05 +4.035032355023e+05
+BODY603_GM +4.121117207701e+01 +4.121117207701e+01
+BODY604_GM +7.311635322923e+01 +7.311635322923e+01
+BODY605_GM +1.539422045545e+02 +1.539422045545e+02
+BODY606_GM +8.978138845307e+03 +8.978138845307e+03
+BODY608_GM +1.205134781724e+02 +1.205134781724e+02
+BODY699_GM +3.793120749865e+07 +3.793120749865e+07
+BODY699_POLE_DEC(1) +8.353764728832e+01 +8.353764728832e+01
+BODY699_POLE_RA(1) +4.058270059426e+01 +4.058270059426e+01
+BODY6_GM +3.794058506051e+07 +3.794058506051e+07
+
+2014-Jul-30 (published)
+Automated Process
+
+Applicable current Ephemeris = 140730R_SCPSE_14051_14083.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 140406_1_203T100
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327132332630e+11 +1.327132332639e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY5_GM +1.267127648000e+08 +1.267127641000e+08
+BODY601_GM +2.503364720729e+00 +2.503522884662e+00
+BODY602_GM +7.210993899856e+00 +7.211292085480e+00
+BODY603_GM +4.121581541110e+01 +4.121117207701e+01
+BODY604_GM +7.311557283053e+01 +7.311635322923e+01
+BODY605_GM +1.539406284855e+02 +1.539422045545e+02
+BODY606_GM +8.978139578101e+03 +8.978138845307e+03
+BODY607_GM +3.717916399235e-01 +3.718791714192e-01
+BODY608_GM +1.205114136810e+02 +1.205134781724e+02
+BODY609_GM +5.534147464623e-01 +5.531110414633e-01
+BODY699_GM +3.793120752438e+07 +3.793120749865e+07
+BODY699_JCOEF(2) +1.629072646994e-02 +1.629069546360e-02
+BODY699_JCOEF(4) -9.344250974340e-04 -9.343510777890e-04
+BODY699_JCOEF(6) +8.813632975019e-05 +8.959557103495e-05
+BODY699_POLE_DEC(1) +8.353762188214e+01 +8.353764728832e+01
+BODY699_POLE_DEC(2) -5.270052700000e-03 -5.841335281700e-03
+BODY699_POLE_RA(1) +4.058216280703e+01 +4.058270059426e+01
+BODY699_POLE_RA(2) -2.613331560000e-02 -2.896108850840e-02
+BODY6_GM +3.794058508695e+07 +3.794058506051e+07
+
+2014-Apr-16 (published)
+Automated Process
+
+Applicable current Ephemeris = 131212R_SCPSE_13273_13314.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 131203_199T96
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.503364720729e+00 +2.503364720729e+00
+BODY602_GM +7.210993899856e+00 +7.210993899856e+00
+BODY603_GM +4.121581541110e+01 +4.121581541110e+01
+BODY604_GM +7.311557283053e+01 +7.311557283053e+01
+BODY605_GM +1.539406284855e+02 +1.539406284855e+02
+BODY606_GM +8.978139578101e+03 +8.978139578101e+03
+BODY607_GM +3.717916399235e-01 +3.717916399235e-01
+BODY608_GM +1.205114136810e+02 +1.205114136810e+02
+BODY609_GM +5.534147464623e-01 +5.534147464623e-01
+BODY699_GM +3.793120752438e+07 +3.793120752438e+07
+BODY699_POLE_RA(1) +4.058216280703e+01 +4.058216280703e+01
+BODY6_GM +3.794058508695e+07 +3.794058508695e+07
+
+2013-Nov-05 (published)
+Automated Process
+
+Applicable current Ephemeris = 131105R_SCPSE_13241_13273.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 131015_198T95
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.503374984937e+00 +2.503364720729e+00
+BODY602_GM +7.210314573106e+00 +7.210993899856e+00
+BODY603_GM +4.121574151061e+01 +4.121581541110e+01
+BODY604_GM +7.311549677532e+01 +7.311557283053e+01
+BODY605_GM +1.539342977601e+02 +1.539406284855e+02
+BODY606_GM +8.978138842275e+03 +8.978139578101e+03
+BODY607_GM +3.713760834192e-01 +3.717916399235e-01
+BODY608_GM +1.206203311620e+02 +1.205114136810e+02
+BODY609_GM +5.517032680985e-01 +5.534147464623e-01
+BODY699_GM +3.793120685564e+07 +3.793120752438e+07
+BODY699_POLE_RA(1) +4.058216280703e+01 +4.058216280703e+01
+BODY6_GM +3.794058451712e+07 +3.794058508695e+07
+
+2013-Oct-24 (published)
+Automated Process
+
+Applicable current Ephemeris = 131024R_SCPSE_13200_13241.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130911_1_196T94
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.503374776631e+00 +2.503374984937e+00
+BODY602_GM +7.210337723506e+00 +7.210314573106e+00
+BODY603_GM +4.121575887463e+01 +4.121574151061e+01
+BODY604_GM +7.311550199907e+01 +7.311549677532e+01
+BODY605_GM +1.539347521641e+02 +1.539342977601e+02
+BODY606_GM +8.978138821641e+03 +8.978138842275e+03
+BODY607_GM +3.713736540033e-01 +3.713760834192e-01
+BODY608_GM +1.206179856883e+02 +1.206203311620e+02
+BODY609_GM +5.517634486963e-01 +5.517032680985e-01
+BODY699_GM +3.793120686211e+07 +3.793120685564e+07
+BODY699_POLE_RA(1) +4.058216280703e+01 +4.058216280703e+01
+BODY6_GM +3.794058452178e+07 +3.794058451712e+07
+
+2013-Aug-07 (published)
+Automated Process
+
+Applicable current Ephemeris = 130807R_SCPSE_13182_13200.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130728_195T93
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.503429813962e+00 +2.503374776631e+00
+BODY602_GM +7.210840769838e+00 +7.210337723506e+00
+BODY603_GM +4.121595253499e+01 +4.121575887463e+01
+BODY604_GM +7.311551677682e+01 +7.311550199907e+01
+BODY605_GM +1.539413218607e+02 +1.539347521641e+02
+BODY606_GM +8.978138475460e+03 +8.978138821641e+03
+BODY607_GM +3.716489921802e-01 +3.713736540033e-01
+BODY608_GM +1.205296586416e+02 +1.206179856883e+02
+BODY609_GM +5.531893969084e-01 +5.517634486963e-01
+BODY699_GM +3.793120725180e+07 +3.793120686211e+07
+BODY699_POLE_RA(1) +4.058216280703e+01 +4.058216280703e+01
+BODY6_GM +3.794058483184e+07 +3.794058452178e+07
+
+2013-Aug-06 (published)
+Automated Process
+
+Applicable current Ephemeris = 130805R_SCPSE_13137_13182.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130713_191T92
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.503362278258e+00 +2.503429813962e+00
+BODY602_GM +7.211043999269e+00 +7.210840769838e+00
+BODY603_GM +4.121588570561e+01 +4.121595253499e+01
+BODY604_GM +7.311557954726e+01 +7.311551677682e+01
+BODY605_GM +1.539414301615e+02 +1.539413218607e+02
+BODY606_GM +8.978138967275e+03 +8.978138475460e+03
+BODY607_GM +3.718388169205e-01 +3.716489921802e-01
+BODY608_GM +1.205022472133e+02 +1.205296586416e+02
+BODY609_GM +5.535607118676e-01 +5.531893969084e-01
+BODY699_GM +3.793120749789e+07 +3.793120725180e+07
+BODY699_POLE_RA(1) +4.058216280703e+01 +4.058216280703e+01
+BODY6_GM +3.794058505181e+07 +3.794058483184e+07
+
+2013-Jul-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 130710R_SCPSE_13087_13137.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130523_186T91
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.503368098279e+00 +2.503362278258e+00
+BODY602_GM +7.210949360765e+00 +7.211043999269e+00
+BODY603_GM +4.121585654735e+01 +4.121588570561e+01
+BODY604_GM +7.311557703862e+01 +7.311557954726e+01
+BODY605_GM +1.539411472541e+02 +1.539414301615e+02
+BODY606_GM +8.978139224038e+03 +8.978138967275e+03
+BODY607_GM +3.717757415270e-01 +3.718388169205e-01
+BODY608_GM +1.205185887895e+02 +1.205022472133e+02
+BODY609_GM +5.533386917621e-01 +5.535607118676e-01
+BODY699_GM +3.793120742331e+07 +3.793120749789e+07
+BODY699_POLE_RA(1) +4.058216280703e+01 +4.058216280703e+01
+BODY6_GM +3.794058499314e+07 +3.794058505181e+07
+
+2013-Apr-17 (published)
+Automated Process
+
+Applicable current Ephemeris = 130417R_SCPSE_13063_13087.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130408_184T90
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.503389125014e+00 +2.503368098279e+00
+BODY602_GM +7.210824055520e+00 +7.210949360765e+00
+BODY603_GM +4.121646992503e+01 +4.121585654735e+01
+BODY604_GM +7.311567610646e+01 +7.311557703862e+01
+BODY605_GM +1.539423900165e+02 +1.539411472541e+02
+BODY606_GM +8.978137632912e+03 +8.978139224038e+03
+BODY607_GM +3.711283610021e-01 +3.717757415270e-01
+BODY608_GM +1.205659185921e+02 +1.205185887895e+02
+BODY609_GM +5.528757716183e-01 +5.533386917621e-01
+BODY699_GM +3.793120691303e+07 +3.793120742331e+07
+BODY699_POLE_RA(1) +4.058216280703e+01 +4.058216280703e+01
+BODY6_GM +3.794058452933e+07 +3.794058499314e+07
+
+2013-Mar-21 (published)
+Automated Process
+
+Applicable current Ephemeris = 130321R_SCPSE_13038_13063.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130313_182R4
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.502932588485e+00 +2.503389125014e+00
+BODY602_CCOEF(3) +1.176812733860e-03 +1.229502218138e-03
+BODY602_GM +7.210896041606e+00 +7.210824055520e+00
+BODY602_JCOEF(2) +6.162878919072e-03 +6.055594538600e-03
+BODY603_GM +4.121933431551e+01 +4.121646992503e+01
+BODY604_CCOEF(3) +3.855939046889e-04 +3.858211235156e-04
+BODY604_GM +7.311632825840e+01 +7.311567610646e+01
+BODY604_JCOEF(2) +1.293263547580e-03 +1.294156214342e-03
+BODY605_CCOEF(3) +2.571480059012e-04 +2.548409590520e-04
+BODY605_GM +1.539385013507e+02 +1.539423900165e+02
+BODY605_JCOEF(2) +8.573276471275e-04 +8.496490377952e-04
+BODY606_CCOEF(3) +9.903199565258e-06 +9.968773423301e-06
+BODY606_GM +8.978138963512e+03 +8.978137632912e+03
+BODY606_JCOEF(2) +3.134349728982e-05 +3.267536300237e-05
+BODY606_SCOEF(3) +2.488942346963e-07 +2.617518846598e-07
+BODY607_GM +3.718387203243e-01 +3.711283610021e-01
+BODY608_GM +1.205399337324e+02 +1.205659185921e+02
+BODY609_GM +5.542009195944e-01 +5.528757716183e-01
+BODY699_GM +3.793120747903e+07 +3.793120691303e+07
+BODY699_JCOEF(2) +1.629070978718e-02 +1.629072646994e-02
+BODY699_JCOEF(4) -9.345542285460e-04 -9.344250974340e-04
+BODY699_JCOEF(6) +9.038698194879e-05 +8.813632975019e-05
+BODY699_POLE_DEC(1) +8.353763359470e+01 +8.353762188214e+01
+BODY699_POLE_DEC(2) -5.393363540000e-03 -5.270052700000e-03
+BODY699_POLE_RA(1) +4.058220675714e+01 +4.058216280703e+01
+BODY699_POLE_RA(2) -2.674382740000e-02 -2.613331560000e-02
+BODY6_GM +3.794058507196e+07 +3.794058452933e+07
+
+2013-Mar-19 (published)
+Automated Process
+
+Applicable current Ephemeris = 130319R_SCPSE_12328_13038.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 130216_176T89
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.502945581381e+00 +2.502932588485e+00
+BODY602_GM +7.211023433546e+00 +7.210896041606e+00
+BODY603_GM +4.121952415934e+01 +4.121933431551e+01
+BODY604_GM +7.311641175079e+01 +7.311632825840e+01
+BODY605_GM +1.539431652765e+02 +1.539385013507e+02
+BODY606_GM +8.978139479506e+03 +8.978138963512e+03
+BODY607_GM +3.716481784171e-01 +3.718387203243e-01
+BODY608_GM +1.205238623917e+02 +1.205399337324e+02
+BODY609_GM +5.531853006318e-01 +5.542009195944e-01
+BODY699_GM +3.793120733707e+07 +3.793120747903e+07
+BODY699_POLE_DEC(1) +8.353763359470e+01 +8.353763359470e+01
+BODY699_POLE_RA(1) +4.058220675714e+01 +4.058220675714e+01
+BODY6_GM +3.794058491832e+07 +3.794058507196e+07
+
+2013-Mar-18 (published)
+Automated Process
+
+Applicable current Ephemeris = 130318R_SCPSE_12304_12328.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 121201_1_175T88
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.502939495793e+00 +2.502945581381e+00
+BODY602_GM +7.211025890027e+00 +7.211023433546e+00
+BODY603_GM +4.121934071627e+01 +4.121952415934e+01
+BODY604_GM +7.311635183417e+01 +7.311641175079e+01
+BODY605_GM +1.539401771918e+02 +1.539431652765e+02
+BODY606_GM +8.978139786579e+03 +8.978139479506e+03
+BODY607_GM +3.717985592397e-01 +3.716481784171e-01
+BODY608_GM +1.205178807361e+02 +1.205238623917e+02
+BODY609_GM +5.532217008470e-01 +5.531853006318e-01
+BODY699_GM +3.793120749695e+07 +3.793120733707e+07
+BODY699_POLE_DEC(1) +8.353763359470e+01 +8.353763359470e+01
+BODY699_POLE_RA(1) +4.058220675714e+01 +4.058220675714e+01
+BODY6_GM +3.794058506948e+07 +3.794058491832e+07
+
+2013-Jan-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 130109R_SCPSE_12304_12328.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 121201_175T88
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.502940780953e+00 +2.502939495793e+00
+BODY602_GM +7.211029263108e+00 +7.211025890027e+00
+BODY603_GM +4.121939803881e+01 +4.121934071627e+01
+BODY604_GM +7.311638721527e+01 +7.311635183417e+01
+BODY605_GM +1.539412620568e+02 +1.539401771918e+02
+BODY606_GM +8.978139854664e+03 +8.978139786579e+03
+BODY607_GM +3.717873741716e-01 +3.717985592397e-01
+BODY608_GM +1.205176869455e+02 +1.205178807361e+02
+BODY609_GM +5.531786201455e-01 +5.532217008470e-01
+BODY699_GM +3.793120740273e+07 +3.793120749695e+07
+BODY699_POLE_DEC(1) +8.353763359470e+01 +8.353763359470e+01
+BODY699_POLE_RA(1) +4.058220675714e+01 +4.058220675714e+01
+BODY6_GM +3.794058497625e+07 +3.794058506948e+07
+
+2012-Dec-07 (published)
+Automated Process
+
+Applicable current Ephemeris = 121204R_SCPSE_12257_12304.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 121112_173T87
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.502953915374e+00 +2.502940780953e+00
+BODY602_GM +7.210903693776e+00 +7.211029263108e+00
+BODY603_GM +4.121983674110e+01 +4.121939803881e+01
+BODY604_GM +7.311642657552e+01 +7.311638721527e+01
+BODY605_GM +1.539430345777e+02 +1.539412620568e+02
+BODY606_GM +8.978138873141e+03 +8.978139854664e+03
+BODY607_GM +3.718066068942e-01 +3.717873741716e-01
+BODY608_GM +1.205411087412e+02 +1.205176869455e+02
+BODY609_GM +5.534220101256e-01 +5.531786201455e-01
+BODY699_GM +3.793120714779e+07 +3.793120740273e+07
+BODY699_POLE_DEC(1) +8.353763359470e+01 +8.353763359470e+01
+BODY699_POLE_RA(1) +4.058220675714e+01 +4.058220675714e+01
+BODY6_GM +3.794058474615e+07 +3.794058497625e+07
+
+2012-Dec-01 (published)
+Automated Process
+
+Applicable current Ephemeris = 121130R_SCPSE_12199_12257.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120926_170T86
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327132332632e+11 +1.327132332630e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.502896232927e+00 +2.502953915374e+00
+BODY602_CCOEF(3) +1.571853686210e-03 +1.176812733860e-03
+BODY602_GM +7.211586963839e+00 +7.210903693776e+00
+BODY602_JCOEF(2) +5.058062033063e-03 +6.162878919072e-03
+BODY603_GM +4.121708815158e+01 +4.121983674110e+01
+BODY604_CCOEF(3) +3.851393798411e-04 +3.855939046889e-04
+BODY604_GM +7.311722849064e+01 +7.311642657552e+01
+BODY604_JCOEF(2) +1.304894043103e-03 +1.293263547580e-03
+BODY605_CCOEF(3) +2.568688346349e-04 +2.571480059012e-04
+BODY605_GM +1.539395355110e+02 +1.539430345777e+02
+BODY605_JCOEF(2) +8.563886910818e-04 +8.573276471275e-04
+BODY606_CCOEF(3) +9.910925261286e-06 +9.903199565258e-06
+BODY606_GM +8.978142647138e+03 +8.978138873141e+03
+BODY606_JCOEF(2) +3.406863224874e-05 +3.134349728982e-05
+BODY606_SCOEF(3) +6.096328895348e-07 +2.488942346963e-07
+BODY607_GM +3.720941692925e-01 +3.718066068942e-01
+BODY608_GM +1.205067470663e+02 +1.205411087412e+02
+BODY609_GM +5.520151854476e-01 +5.534220101256e-01
+BODY699_GM +3.793120704106e+07 +3.793120714779e+07
+BODY699_JCOEF(2) +1.629085324163e-02 +1.629070978718e-02
+BODY699_JCOEF(4) -9.338162877618e-04 -9.345542285460e-04
+BODY699_JCOEF(6) +9.442465978731e-05 +9.038698194879e-05
+BODY699_POLE_DEC(1) +8.353760495079e+01 +8.353763359470e+01
+BODY699_POLE_DEC(2) -5.720607940000e-03 -5.393363540000e-03
+BODY699_POLE_RA(1) +4.058219911002e+01 +4.058220675714e+01
+BODY699_POLE_RA(2) -2.837023140000e-02 -2.674382740000e-02
+BODY6_GM +3.794058460290e+07 +3.794058474615e+07
+BODY7_GM +5.794557000000e+06 +5.794548600000e+06
+
+2012-Aug-30 (published)
+Automated Process
+
+Applicable current Ephemeris = 120829R_SCPSE_12151_12199.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120723_168T85
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327132332632e+11 +1.327132332632e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.502789688410e+00 +2.502896232927e+00
+BODY602_GM +7.211762869370e+00 +7.211586963839e+00
+BODY603_GM +4.121695168687e+01 +4.121708815158e+01
+BODY604_GM +7.311780375743e+01 +7.311722849064e+01
+BODY605_GM +1.539399400530e+02 +1.539395355110e+02
+BODY606_GM +8.978142779511e+03 +8.978142647138e+03
+BODY607_GM +3.721163085468e-01 +3.720941692925e-01
+BODY608_GM +1.205058816639e+02 +1.205067470663e+02
+BODY609_GM +5.517235059199e-01 +5.520151854476e-01
+BODY699_GM +3.793120704905e+07 +3.793120704106e+07
+BODY699_JCOEF(2) +1.629083792178e-02 +1.629085324163e-02
+BODY699_JCOEF(4) -9.337437981265e-04 -9.338162877618e-04
+BODY699_JCOEF(6) +9.371990144597e-05 +9.442465978731e-05
+BODY699_POLE_DEC(1) +8.353765343003e+01 +8.353760495079e+01
+BODY699_POLE_RA(1) +4.058242679916e+01 +4.058219911002e+01
+BODY6_GM +3.794058461080e+07 +3.794058460290e+07
+
+2012-Jun-29 (published)
+Automated Process
+
+Applicable current Ephemeris = 120628R_SCPSE_12116_12136.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120523_166T83
+
+Parameter Superseded Value New Value
+
+BODY10_GM +1.327124400409e+11 +1.327132332632e+11
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY601_GM +2.502732557135e+00 +2.502789688410e+00
+BODY602_GM +7.212055044568e+00 +7.211762869370e+00
+BODY603_GM +4.121681151664e+01 +4.121695168687e+01
+BODY604_GM +7.311689571825e+01 +7.311780375743e+01
+BODY605_GM +1.539392032247e+02 +1.539399400530e+02
+BODY606_GM +8.978142890321e+03 +8.978142779511e+03
+BODY607_GM +3.720234351039e-01 +3.721163085468e-01
+BODY608_GM +1.205064232644e+02 +1.205058816639e+02
+BODY609_GM +5.515085378325e-01 +5.517235059199e-01
+BODY699_GM +3.793120714983e+07 +3.793120704905e+07
+BODY699_JCOEF(2) +1.629086364882e-02 +1.629083792178e-02
+BODY699_JCOEF(4) -9.337992318066e-04 -9.337437981265e-04
+BODY699_JCOEF(6) +9.596024651605e-05 +9.371990144597e-05
+BODY699_POLE_DEC(1) +8.353757612142e+01 +8.353765343003e+01
+BODY699_POLE_DEC(2) -5.862042770000e-03 -5.720607940000e-03
+BODY699_POLE_RA(1) +4.058203525207e+01 +4.058242679916e+01
+BODY699_POLE_RA(2) -2.976086740000e-02 -2.837023140000e-02
+BODY6_GM +3.794058471037e+07 +3.794058461080e+07
+BODY7_GM +5.794548600000e+06 +5.794557000000e+06
+
+2012-May-23 (published)
+Automated Process
+
+Applicable current Ephemeris = 120523R_SCPSE_12098_12116.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120502_1_165E19
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800013433e+03
+BODY399_GM +3.986004362961e+05 +3.986004362961e+05
+BODY5_GM +1.267127648000e+08 +1.267127648000e+08
+BODY601_GM +2.502757050877e+00 +2.502732557135e+00
+BODY602_GM +7.211707954300e+00 +7.212055044568e+00
+BODY603_GM +4.121671259700e+01 +4.121681151664e+01
+BODY604_GM +7.311712862180e+01 +7.311689571825e+01
+BODY605_GM +1.539390197027e+02 +1.539392032247e+02
+BODY606_GM +8.978142876094e+03 +8.978142890321e+03
+BODY607_GM +3.720107081501e-01 +3.720234351039e-01
+BODY608_GM +1.205077782502e+02 +1.205064232644e+02
+BODY609_GM +5.514776081161e-01 +5.515085378325e-01
+BODY699_GM +3.793120712313e+07 +3.793120714983e+07
+BODY699_JCOEF(2) +1.629087428832e-02 +1.629086364882e-02
+BODY699_JCOEF(4) -9.338877596813e-04 -9.337992318066e-04
+BODY699_JCOEF(6) +9.363764244073e-05 +9.596024651605e-05
+BODY699_POLE_DEC(1) +8.353755491179e+01 +8.353757612142e+01
+BODY699_POLE_DEC(2) -5.720607940000e-03 -5.862042770000e-03
+BODY699_POLE_RA(1) +4.058192715365e+01 +4.058203525207e+01
+BODY699_POLE_RA(2) -2.837023140000e-02 -2.976086740000e-02
+BODY6_GM +3.794058468460e+07 +3.794058471037e+07
+BODY7_GM +5.794548600000e+06 +5.794548600000e+06
+
+2012-Apr-26 (published)
+Automated Process
+
+Applicable current Ephemeris = 120426R_SCPSE_12077_12098.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120416_164E18
+
+Parameter Superseded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800076228e+03 +4.902800013433e+03
+BODY399_GM +3.986004362333e+05 +3.986004362961e+05
+BODY5_GM +1.267127648000e+08 +1.267127648000e+08
+BODY601_GM +2.502781809124e+00 +2.502757050877e+00
+BODY602_GM +7.211929911319e+00 +7.211707954300e+00
+BODY603_GM +4.121700270136e+01 +4.121671259700e+01
+BODY604_GM +7.311735484700e+01 +7.311712862180e+01
+BODY605_GM +1.539394541121e+02 +1.539390197027e+02
+BODY606_GM +8.978142978805e+03 +8.978142876094e+03
+BODY607_GM +3.720046795694e-01 +3.720107081501e-01
+BODY608_GM +1.205116677867e+02 +1.205077782502e+02
+BODY609_GM +5.515442127428e-01 +5.514776081161e-01
+BODY699_GM +3.793120714229e+07 +3.793120712313e+07
+BODY699_JCOEF(2) +1.629083239718e-02 +1.629087428832e-02
+BODY699_JCOEF(4) -9.339199266817e-04 -9.338877596813e-04
+BODY699_JCOEF(6) +9.407948941470e-05 +9.363764244073e-05
+BODY699_POLE_DEC(1) +8.353765707880e+01 +8.353755491179e+01
+BODY699_POLE_RA(1) +4.058232152654e+01 +4.058192715365e+01
+BODY6_GM +3.794058470900e+07 +3.794058468460e+07
+BODY7_GM +5.794557000000e+06 +5.794548600000e+06
+
+2012-Apr-18 (published)
+Automated Process
+
+Applicable current Ephemeris = 120416R_SCPSE_12042_12061.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120329_162E17
+
+Parameter Superceded Value New Value
+
+BODY299_GM +3.248585920000e+05 +3.248585920000e+05
+BODY301_GM +4.902800013433e+03 +4.902800076228e+03
+BODY399_GM +3.986004362961e+05 +3.986004362333e+05
+BODY599_GM +1.266865339033e+08 +1.267127654544e+08
+BODY5_GM +1.267127648000e+08 +1.267127648000e+08
+BODY601_GM +2.502576360130e+00 +2.502781809124e+00
+BODY602_CCOEF(3) +1.401126121569e-03 +1.571853686210e-03
+BODY602_GM +7.211620392608e+00 +7.211929911319e+00
+BODY602_JCOEF(2) +5.180894509760e-03 +5.058062033063e-03
+BODY603_GM +4.121701834062e+01 +4.121700270136e+01
+BODY604_CCOEF(3) +3.792220000000e-04 +3.851393798411e-04
+BODY604_GM +7.311625775155e+01 +7.311735484700e+01
+BODY604_JCOEF(2) +1.262860000000e-03 +1.304894043103e-03
+BODY605_CCOEF(3) +2.193468165357e-04 +2.568688346349e-04
+BODY605_GM +1.539397404411e+02 +1.539394541121e+02
+BODY605_JCOEF(2) +9.541798988345e-04 +8.563886910818e-04
+BODY606_CCOEF(3) +9.955883795748e-06 +9.910925261286e-06
+BODY606_GM +8.978137947298e+03 +8.978142978805e+03
+BODY606_JCOEF(2) +3.346401469529e-05 +3.406863224874e-05
+BODY606_SCOEF(3) +2.817024724065e-07 +6.096328895348e-07
+BODY607_GM +3.717797526598e-01 +3.720046795694e-01
+BODY608_GM +1.205457671731e+02 +1.205116677867e+02
+BODY609_GM +5.530284459514e-01 +5.515442127428e-01
+BODY699_GM +3.793120680764e+07 +3.793120714229e+07
+BODY699_JCOEF(2) +1.629088162435e-02 +1.629083239718e-02
+BODY699_JCOEF(4) -9.341612482702e-04 -9.339199266817e-04
+BODY699_JCOEF(6) +8.936911675694e-05 +9.407948941470e-05
+BODY699_POLE_DEC(1) +8.353758489860e+01 +8.353765707880e+01
+BODY699_POLE_DEC(2) -5.862042770000e-03 -5.720607940000e-03
+BODY699_POLE_RA(1) +4.058274178768e+01 +4.058232152654e+01
+BODY699_POLE_RA(2) -2.976086740000e-02 -2.837023140000e-02
+BODY6_GM +3.794058440338e+07 +3.794058470900e+07
+BODY7_GM +5.794548600000e+06 +5.794557000000e+06
+
+2012-Feb-28 (published)
+Automated Process
+
+Applicable current Ephemeris = 120227R_SCPSE_11357_12016.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120203_160T81
+
+Parameter Superceded Value New Value
+
+BODY299_GM +3.248585988265e+05 +3.248585920000e+05
+BODY301_GM +4.902800076228e+03 +4.902800013433e+03
+BODY399_GM +3.986004362333e+05 +3.986004362961e+05
+BODY3_GM +4.035032363096e+05 +4.035032417380e+05
+BODY601_GM +2.502609373501e+00 +2.502576360130e+00
+BODY602_CCOEF(3) +1.401126100000e-03 +1.401126121569e-03
+BODY602_GM +7.211505727025e+00 +7.211620392608e+00
+BODY602_JCOEF(2) +5.180890000000e-03 +5.180894509760e-03
+BODY603_GM +4.121695859535e+01 +4.121701834062e+01
+BODY604_GM +7.311631631847e+01 +7.311625775155e+01
+BODY605_CCOEF(3) +2.193468000000e-04 +2.193468165357e-04
+BODY605_GM +1.539396945672e+02 +1.539397404411e+02
+BODY605_JCOEF(2) +9.541800000000e-04 +9.541798988345e-04
+BODY606_CCOEF(3) +9.955900000000e-06 +9.955883795748e-06
+BODY606_GM +8.978138479967e+03 +8.978137947298e+03
+BODY606_JCOEF(2) +3.346000000000e-05 +3.346401469529e-05
+BODY606_SCOEF(3) +2.817000000000e-07 +2.817024724065e-07
+BODY607_GM +3.717583184521e-01 +3.717797526598e-01
+BODY608_GM +1.205487491162e+02 +1.205457671731e+02
+BODY609_GM +5.524333193119e-01 +5.530284459514e-01
+BODY699_GM +3.793120690270e+07 +3.793120680764e+07
+BODY699_JCOEF(2) +1.629087423500e-02 +1.629088162435e-02
+BODY699_JCOEF(4) -9.342391790000e-04 -9.341612482702e-04
+BODY699_JCOEF(6) +8.883146500000e-05 +8.936911675694e-05
+BODY699_POLE_DEC(1) +8.353758200000e+01 +8.353758489860e+01
+BODY699_POLE_DEC(2) -5.862000000000e-03 -5.862042770000e-03
+BODY699_POLE_RA(1) +4.058264200000e+01 +4.058274178768e+01
+BODY699_POLE_RA(2) -2.976100000000e-02 -2.976086740000e-02
+BODY6_GM +3.794058450123e+07 +3.794058440338e+07
+
+2012-Jan-19 (published)
+Automated Process
+
+Applicable current Ephemeris = 120119R_SCPSE_11337_11357.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 120105_159T80
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.51701198 37940584.50122525
+BODY699_GM 37931206.9198 37931206.9027
+BODY699_POLE_RA(1) 40.582648 40.582642
+BODY699_POLE_DEC(1) 83.537576 83.537582
+BODY699_JCOEF(2) 0.016290873808 0.016290874235
+BODY699_JCOEF(4) -0.000934271084 -0.000934239179
+BODY699_JCOEF(6) 0.000088937374 0.000088831465
+BODY601_GM 2.502701109172617 2.502609373500557
+BODY602_GM 7.211289386801197 7.211505727024772
+BODY603_GM 41.21702746886321 41.21695859535338
+BODY604_GM 73.11634639889347 73.11631631847311
+BODY604_JCOEF(2) 0.0012 0.00126286
+BODY604_CCOEF(3) 0.000361 0.0003792220
+BODY605_GM 153.9395644216691 153.9396945671801
+BODY606_GM 8978.138517075671 8978.138479966845
+BODY607_GM 0.371740933989066 0.371758318452143
+BODY608_GM 120.5475434022670 120.5487491162408
+BODY609_GM 0.5524404151635458 0.5524333193118883
+
+2012-Jan-17 (published)
+Automated Process
+
+Applicable current Ephemeris = 120117R_SCPSE_11303_11337.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 111216_157T79
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.72898314 37940584.51701198
+BODY699_GM 37931207.1187 37931206.9198
+BODY699_POLE_RA(1) 40.582382 40.582648
+BODY699_POLE_DEC(1) 83.537590 83.537576
+BODY699_JCOEF(2) 0.016290899375 0.016290873808
+BODY699_JCOEF(4) -0.000934474971 -0.000934271084
+BODY699_JCOEF(6) 0.000087083293 0.000088937374
+BODY601_GM 2.502748619543429 2.502701109172617
+BODY602_GM 7.211444887614973 7.211289386801197
+BODY603_GM 41.21721833070302 41.21702746886321
+BODY604_GM 73.11637880800029 73.11634639889347
+BODY605_GM 153.9515313553848 153.9395644216691
+BODY606_GM 8978.140251410228 8978.138517075671
+BODY607_GM 0.371745584012855 0.371740933989066
+BODY608_GM 120.5458907932224 120.5475434022670
+BODY609_GM 0.5531157026177208 0.5524404151635458
+
+2011-Oct-14 (published)
+Automated Process
+
+Applicable current Ephemeris = 111014R_SCPSE_11246_11267.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 111003_154E14
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.48265366 37940584.72898314
+BODY699_GM 37931207.9045 37931207.1187
+BODY699_POLE_RA(1) 40.582396 40.582382
+BODY699_POLE_RA(2) -0.033859 -0.029761
+BODY699_POLE_DEC(1) 83.537615 83.537590
+BODY699_POLE_DEC(2) -0.006348 -0.005862
+BODY699_JCOEF(2) 0.016290821650 0.016290899375
+BODY699_JCOEF(4) -0.000934481091 -0.000934474971
+BODY699_JCOEF(6) 0.000089178356 0.000087083293
+BODY601_GM 2.502709995086387 2.502748619543429
+BODY602_GM 7.211349287191156 7.211444887614973
+BODY602_JCOEF(2) 0.00527772 0.00518089
+BODY602_CCOEF(3) 0.0013095931 0.0014011261
+BODY603_GM 41.21699261797900 41.21721833070302
+BODY604_GM 73.11610656099036 73.11637880800029
+BODY605_GM 153.9403316477660 153.9515313553848
+BODY605_JCOEF(2) 0.00095018 0.00095418
+BODY605_CCOEF(3) 0.0002230468 0.0002193468
+BODY606_GM 8978.142487268824 8978.140251410228
+BODY606_JCOEF(2) 0.00003216 0.00003346
+BODY606_CCOEF(3) 0.0000099392 0.0000099559
+BODY606_SCOEF(3) -0.0000003327 0.0000002817
+BODY607_GM 0.371862776487706 0.371745584012855
+BODY608_GM 120.5236609628246 120.5458907932224
+BODY609_GM 0.5526712667564784 0.5531157026177208
+
+2011-Oct-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 111010R_SCPSE_11150_11246.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 110915_150T78
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.79162857 37940585.48265366
+BODY699_GM 37931207.2153 37931207.9045
+BODY699_POLE_RA(1) 40.582683 40.582396
+BODY699_POLE_DEC(1) 83.537662 83.537615
+BODY699_JCOEF(2) 0.016290924417 0.016290821650
+BODY699_JCOEF(4) -0.000934268461 -0.000934481091
+BODY699_JCOEF(6) 0.000087694639 0.000089178356
+BODY601_GM 2.502718654443902 2.502709995086387
+BODY602_GM 7.211415535267963 7.211349287191156
+BODY603_GM 41.21680348050685 41.21699261797900
+BODY604_GM 73.11620149768477 73.11610656099036
+BODY605_GM 153.9429277851216 153.9403316477660
+BODY606_GM 8978.141512182867 8978.142487268824
+BODY607_GM 0.371559508106878 0.371862776487706
+BODY608_GM 120.5206701212654 120.5236609628246
+BODY609_GM 0.5525429652386353 0.5526712667564784
+
+2011-Aug-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 110721R_SCPSE_11119_11150.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 110623_149T77
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.41564407 37940584.79162857
+BODY699_GM 37931207.8379 37931207.2153
+BODY699_POLE_RA(1) 40.582735 40.582683
+BODY699_POLE_DEC(1) 83.537640 83.537662
+BODY699_JCOEF(2) 0.016290769033 0.016290924417
+BODY699_JCOEF(4) -0.000934828924 -0.000934268461
+BODY699_JCOEF(6) 0.000089541641 0.000087694639
+BODY601_GM 2.502712463799070 2.502718654443902
+BODY602_GM 7.211309707003353 7.211415535267963
+BODY603_GM 41.21694923358992 41.21680348050685
+BODY604_GM 73.11602896866832 73.11620149768477
+BODY605_GM 153.9421876166184 153.9429277851216
+BODY606_GM 8978.141233205604 8978.141512182867
+BODY607_GM 0.371894539491829 0.371559508106878
+BODY608_GM 120.5228618777735 120.5206701212654
+BODY609_GM 0.5525905733729537 0.5525429652386353
+
+2011-May-20 (published)
+Automated Process
+
+Applicable current Ephemeris = 110519R_SCPSE_11093_11119.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 110511_148T76
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.28449907 37940585.41564407
+BODY699_GM 37931207.7016 37931207.8379
+BODY699_POLE_RA(1) 40.583101 40.582735
+BODY699_POLE_DEC(1) 83.537606 83.537640
+BODY699_JCOEF(2) 0.016290745825 0.016290769033
+BODY699_JCOEF(4) -0.000934907419 -0.000934828924
+BODY699_JCOEF(6) 0.000090097813 0.000089541641
+BODY601_GM 2.502684587752144 2.502712463799070
+BODY602_GM 7.211270538055901 7.211309707003353
+BODY602_JCOEF(2) 0.00549329 0.00527772
+BODY602_CCOEF(3) 0.0011903952 0.0013095931
+BODY603_GM 41.21712026405778 41.21694923358992
+BODY604_GM 73.11608291566047 73.11602896866832
+BODY605_GM 153.9428904917647 153.9421876166184
+BODY605_JCOEF(2) 0.00095268 0.00095018
+BODY605_CCOEF(3) 0.0002222901 0.0002230468
+BODY606_GM 8978.141550256330 8978.141233205604
+BODY607_GM 0.372068900451880 0.371894539491829
+BODY608_GM 120.5266601781686 120.5228618777735
+BODY609_GM 0.5525857916664789 0.5525905733729537
+
+2011-Feb-04 (published)
+Automated Process
+
+Applicable current Ephemeris = 110204R_SCPSE_10344_11003.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 110113_143R3
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.37187426 37940585.28449907
+BODY699_GM 37931207.7852 37931207.7016
+BODY699_POLE_RA(1) 40.581500 40.583101
+BODY699_POLE_RA(2) -0.028733 -0.033859
+BODY699_POLE_DEC(1) 83.537730 83.537606
+BODY699_POLE_DEC(2) -0.005948 -0.006348
+BODY699_JCOEF(2) 0.016290633224 0.016290745825
+BODY699_JCOEF(4) -0.000935195652 -0.000934907419
+BODY699_JCOEF(6) 0.000085459485 0.000090097813
+BODY601_GM 2.502626327561335 2.502684587752144
+BODY602_GM 7.210536994915831 7.211270538055901
+BODY602_JCOEF(2) 0.00531842 0.00549329
+BODY602_CCOEF(3) 0.0015976821 0.0011903952
+BODY603_GM 41.22349707074201 41.21712026405778
+BODY604_GM 73.11665319608169 73.11608291566047
+BODY605_GM 153.9442354209173 153.9428904917647
+BODY605_JCOEF(2) 0.00095295 0.00095268
+BODY605_CCOEF(3) 0.0002228052 0.0002222901
+BODY606_GM 8978.139216940886 8978.141550256330
+BODY606_JCOEF(2) 0.00003269 0.00003216
+BODY606_CCOEF(3) 0.0000100419 0.0000099392
+BODY606_SCOEF(3) 0.0000003039 -0.0000003327
+BODY607_GM 0.371282156229949 0.372068900451880
+BODY608_GM 120.5253274797591 120.5266601781686
+BODY609_GM 0.5532663617110715 0.5525857916664789
+
+2011-Jan-19 (published)
+Automated Process
+
+Applicable current Ephemeris = 110119R_SCPSE_10326_10358.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 101223_142E13
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.41238648 37940585.37187426
+BODY699_GM 37931207.8284 37931207.7852
+BODY699_POLE_RA(1) 40.581689 40.581500
+BODY699_POLE_DEC(1) 83.537707 83.537730
+BODY699_JCOEF(2) 0.016290633969 0.016290633224
+BODY699_JCOEF(4) -0.000935277266 -0.000935195652
+BODY699_JCOEF(6) 0.000084635225 0.000085459485
+BODY601_GM 2.502628566850901 2.502626327561335
+BODY602_GM 7.210415677503655 7.210536994915831
+BODY602_JCOEF(2) 0.00523040 0.00531842
+BODY602_CCOEF(3) 0.0015737859 0.0015976821
+BODY603_GM 41.22320902398944 41.22349707074201
+BODY604_GM 73.11651456573139 73.11665319608169
+BODY605_GM 153.9443320892218 153.9442354209173
+BODY606_GM 8978.139152894189 8978.139216940886
+BODY607_GM 0.371399737059410 0.371282156229949
+BODY608_GM 120.5230847276307 120.5253274797591
+BODY609_GM 0.5532448793302067 0.5532663617110715
+
+2010-Dec-17 (published)
+Automated Process
+
+Applicable current Ephemeris = 101215R_SCPSE_10302_10326.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 101201_141E12
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.83653561 37940585.41238648
+BODY699_GM 37931207.2536 37931207.8284
+BODY699_POLE_RA(1) 40.582631 40.581689
+BODY699_POLE_RA(2) -0.032774 -0.028733
+BODY699_POLE_DEC(1) 83.537547 83.537707
+BODY699_POLE_DEC(2) -0.004597 -0.005948
+BODY699_JCOEF(2) 0.016290651320 0.016290633969
+BODY699_JCOEF(4) -0.000935096688 -0.000935277266
+BODY699_JCOEF(6) 0.000085352909 0.000084635225
+BODY601_GM 2.502663111473977 2.502628566850901
+BODY602_GM 7.211324203674568 7.210415677503655
+BODY602_JCOEF(2) 0.00557036 0.00523040
+BODY602_CCOEF(3) 0.0016663335 0.0015737859
+BODY603_GM 41.22170043283749 41.22320902398944
+BODY604_GM 73.11568875704903 73.11651456573139
+BODY605_GM 153.9440126920278 153.9443320892218
+BODY606_GM 8978.138814840953 8978.139152894189
+BODY607_GM 0.371969905643023 0.371399737059410
+BODY608_GM 120.5236408456456 120.5230847276307
+BODY609_GM 0.5531308887862909 0.5532448793302067
+
+2010-Oct-14 (published)
+Automated Process
+
+Applicable current Ephemeris = 101013R_SCPSE_10216_10256.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100927_137T72
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.61433598 37940584.83653561
+BODY699_GM 37931207.0322 37931207.2536
+BODY699_POLE_RA(1) 40.582809 40.582631
+BODY699_POLE_DEC(1) 83.537558 83.537547
+BODY699_JCOEF(2) 0.016290678471 0.016290651320
+BODY699_JCOEF(4) -0.000935178263 -0.000935096688
+BODY699_JCOEF(6) 0.000084369889 0.000085352909
+BODY601_GM 2.502663309378276 2.502663111473977
+BODY602_GM 7.211042948930951 7.211324203674568
+BODY603_GM 41.22306832898998 41.22170043283749
+BODY604_GM 73.11573158578534 73.11568875704903
+BODY605_GM 153.9434257917183 153.9440126920278
+BODY606_GM 8978.138489543775 8978.138814840953
+BODY607_GM 0.372089441130883 0.371969905643023
+BODY608_GM 120.5225430884476 120.5236408456456
+BODY609_GM 0.5530596352942014 0.5531308887862909
+
+2010-Sep-13 (published)
+Automated Process
+
+Applicable current Ephemeris = 100913R_SCPSE_10178_10216.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100816_135E11
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.19103519 37940584.61433598
+BODY699_GM 37931207.6129 37931207.0322
+BODY699_POLE_RA(1) 40.582746 40.582809
+BODY699_POLE_DEC(1) 83.537530 83.537558
+BODY699_JCOEF(2) 0.016290713275 0.016290678471
+BODY699_JCOEF(4) -0.000934907426 -0.000935178263
+BODY699_JCOEF(6) 0.000086813940 0.000084369889
+BODY601_GM 2.502649735590598 2.502663309378276
+BODY602_GM 7.210755807081804 7.211042948930951
+BODY603_GM 41.22385281006390 41.22306832898998
+BODY604_GM 73.11577260830295 73.11573158578534
+BODY605_GM 153.9434705372475 153.9434257917183
+BODY606_GM 8978.138947128351 8978.138489543775
+BODY607_GM 0.372093053243830 0.372089441130883
+BODY608_GM 120.5174460416719 120.5225430884476
+BODY609_GM 0.5531061101745497 0.5530596352942014
+
+2010-Jul-27 (published)
+Automated Process
+
+Applicable current Ephemeris = 100726R_SCPSE_10164_10178.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100709_134T71
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.18590788 37940585.19103519
+BODY699_GM 37931207.6077 37931207.6129
+BODY699_POLE_RA(1) 40.582679 40.582746
+BODY699_POLE_DEC(1) 83.537533 83.537530
+BODY699_JCOEF(2) 0.016290699821 0.016290713275
+BODY699_JCOEF(4) -0.000934908417 -0.000934907426
+BODY699_JCOEF(6) 0.000086154394 0.000086813940
+BODY601_GM 2.502653854130373 2.502649735590598
+BODY602_GM 7.210753192578406 7.210755807081804
+BODY603_GM 41.22399120522562 41.22385281006390
+BODY604_GM 73.11575812534798 73.11577260830295
+BODY605_GM 153.9434658935521 153.9434705372475
+BODY606_GM 8978.138877124944 8978.138947128351
+BODY607_GM 0.372092758433870 0.372093053243830
+BODY608_GM 120.5175109354886 120.5174460416719
+BODY609_GM 0.5531033330031904 0.5531061101745497
+
+2010-Jul-06 (published)
+Automated Process
+
+Applicable current Ephemeris = 100706R_SCPSE_10146_10164.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100623_133T70
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.29031831 37940585.18590788
+BODY699_GM 37931207.7190 37931207.6077
+BODY699_POLE_RA(1) 40.582751 40.582679
+BODY699_POLE_DEC(1) 83.537526 83.537533
+BODY699_JCOEF(2) 0.016290754606 0.016290699821
+BODY699_JCOEF(4) -0.000934784018 -0.000934908417
+BODY699_JCOEF(6) 0.000086160455 0.000086154394
+BODY601_GM 2.502656688609775 2.502653854130373
+BODY602_GM 7.210856063224142 7.210753192578406
+BODY603_GM 41.22385484916347 41.22399120522562
+BODY604_GM 73.11579543141077 73.11575812534798
+BODY605_GM 153.9435729984046 153.9434658935521
+BODY606_GM 8978.138935580162 8978.138877124944
+BODY606_JCOEF(2) 0.00003264 0.00003269
+BODY606_CCOEF(3) 0.0000101074 0.0000100419
+BODY606_SCOEF(3) 0.0000002976 0.0000003039
+BODY607_GM 0.371810410430814 0.372092758433870
+BODY608_GM 120.5108312160242 120.5175109354886
+BODY609_GM 0.5530318826600191 0.5531033330031904
+
+2010-Jun-25 (published)
+Automated Process
+
+Applicable current Ephemeris = 100625R_SCPSE_10132_10146.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100608_132T69
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.37753170 37940585.29031831
+BODY699_GM 37931207.8020 37931207.7190
+BODY699_POLE_RA(1) 40.583044 40.582751
+BODY699_POLE_RA(2) -0.051079 -0.032774
+BODY699_POLE_DEC(1) 83.537392 83.537526
+BODY699_POLE_DEC(2) -0.003848 -0.004597
+BODY699_JCOEF(2) 0.016290743445 0.016290754606
+BODY699_JCOEF(4) -0.000934656136 -0.000934784018
+BODY699_JCOEF(6) 0.000089478120 0.000086160455
+BODY601_GM 2.502671606225361 2.502656688609775
+BODY602_GM 7.215820873505562 7.210856063224142
+BODY603_GM 41.22377302913180 41.22385484916347
+BODY604_GM 73.11608477740288 73.11579543141077
+BODY605_GM 153.9425885951420 153.9435729984046
+BODY606_GM 8978.139647304321 8978.138935580162
+BODY606_JCOEF(2) 0.00003269 0.00003264
+BODY606_CCOEF(3) 0.0000100419 0.0000101074
+BODY606_SCOEF(3) 0.0000003039 0.0000002976
+BODY607_GM 0.371579902841404 0.371810410430814
+BODY608_GM 120.5103570301357 120.5108312160242
+BODY609_GM 0.5530290115183746 0.5530318826600191
+
+2010-Jun-16 (published)
+Automated Process
+
+Applicable current Ephemeris = 100616R_SCPSE_10110_10132.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100523_131T68
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.06567518 37940585.37753170
+BODY699_GM 37931207.5024 37931207.8020
+BODY699_POLE_RA(1) 40.583171 40.583044
+BODY699_POLE_RA(2) -0.049286 -0.051079
+BODY699_POLE_DEC(1) 83.537659 83.537392
+BODY699_POLE_DEC(2) -0.003661 -0.003848
+BODY699_JCOEF(2) 0.016290772029 0.016290743445
+BODY699_JCOEF(4) -0.000934694303 -0.000934656136
+BODY699_JCOEF(6) 0.000089880248 0.000089478120
+BODY601_GM 2.502694107602816 2.502671606225361
+BODY602_GM 7.200063329536838 7.215820873505562
+BODY602_JCOEF(2) 0.00897000 0.00557036
+BODY602_CCOEF(3) 0.0020800000 0.0016663335
+BODY603_GM 41.22407969389818 41.22377302913180
+BODY604_GM 73.11530489083277 73.11608477740288
+BODY605_GM 153.9438092585369 153.9425885951420
+BODY605_JCOEF(2) 0.00094296 0.00095295
+BODY605_CCOEF(3) 0.0002311116 0.0002228052
+BODY606_GM 8978.139811476925 8978.139647304321
+BODY606_JCOEF(2) 0.00003345 0.00003269
+BODY606_CCOEF(3) 0.0000100225 0.0000100419
+BODY606_SCOEF(3) 0.0000002649 0.0000003039
+BODY607_GM 0.371472830275555 0.371579902841404
+BODY608_GM 120.5130217227762 120.5103570301357
+BODY609_GM 0.5530242922746966 0.5530290115183746
+
+2010-Apr-20 (published)
+Automated Process
+
+Applicable current Ephemeris = 100420R_SCPSE_10055_10085.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100409_128T67
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.21575641 37940585.06567518
+BODY699_GM 37931207.6474 37931207.5024
+BODY699_POLE_RA(1) 40.583800 40.583171
+BODY699_POLE_DEC(1) 83.537637 83.537659
+BODY699_JCOEF(2) 0.016290761372 0.016290772029
+BODY699_JCOEF(4) -0.000935041843 -0.000934694303
+BODY699_JCOEF(6) 0.000088218547 0.000089880248
+BODY601_GM 2.502664059914654 2.502694107602816
+BODY602_GM 7.206088184897235 7.200063329536838
+BODY603_GM 41.22395894571505 41.22407969389818
+BODY604_GM 73.11537306097487 73.11530489083277
+BODY605_GM 153.9437119917676 153.9438092585369
+BODY605_JCOEF(2) 0.00094265 0.00094296
+BODY605_CCOEF(3) 0.0002312426 0.0002311116
+BODY606_GM 8978.139838625968 8978.139811476925
+BODY607_GM 0.371514037767062 0.371472830275555
+BODY608_GM 120.5121181800631 120.5130217227762
+BODY609_GM 0.5530860071780509 0.5530242922746966
+
+2010-Mar-25 (published)
+Automated Process
+
+Applicable current Ephemeris = 100325R_SCPSE_10021_10055.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100306_126R2
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.09552705 37940585.21575641
+BODY699_GM 37931207.5284 37931207.6474
+BODY699_POLE_RA(1) 40.585300 40.583800
+BODY699_POLE_RA(2) -0.078714 -0.049286
+BODY699_POLE_DEC(1) 83.537587 83.537637
+BODY699_POLE_DEC(2) -0.002593 -0.003661
+BODY699_JCOEF(2) 0.016290745623 0.016290761372
+BODY699_JCOEF(4) -0.000935314074 -0.000935041843
+BODY699_JCOEF(6) 0.000087992940 0.000088218547
+BODY601_GM 2.502460898333089 2.502664059914654
+BODY602_GM 7.214445984477930 7.206088184897235
+BODY603_GM 41.22381705804884 41.22395894571505
+BODY604_GM 73.11541481976771 73.11537306097487
+BODY605_GM 153.9435622399753 153.9437119917676
+BODY605_JCOEF(2) 0.000941 0.00094265
+BODY605_CCOEF(3) 0.000232 0.0002312426
+BODY606_GM 8978.139471964878 8978.139838625968
+BODY607_GM 0.371794454208596 0.371514037767062
+BODY608_GM 120.5028737124517 120.5121181800631
+BODY609_GM 0.5533175139508248 0.5530860071780509
+
+2010-Feb-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 100209R_SCPSE_10003_10021.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100131_125T66
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.22578886 37940585.09552705
+BODY699_GM 37931207.6569 37931207.5284
+BODY699_POLE_RA(1) 40.585759 40.585300
+BODY699_POLE_DEC(1) 83.537556 83.537587
+BODY699_JCOEF(2) 0.016290741015 0.016290745623
+BODY699_JCOEF(4) -0.000935387473 -0.000935314074
+BODY699_JCOEF(6) 0.000088500228 0.000087992940
+BODY601_GM 2.502446043296527 2.502460898333089
+BODY602_GM 7.215994919166206 7.214445984477930
+BODY603_GM 41.22362671256990 41.22381705804884
+BODY604_GM 73.11544724167149 73.11541481976771
+BODY605_GM 153.9435653494335 153.9435622399753
+BODY606_GM 8978.139773741363 8978.139471964878
+BODY607_GM 0.371704406193575 0.371794454208596
+BODY608_GM 120.5029631980470 120.5028737124517
+BODY609_GM 0.5533689173792706 0.5533175139508248
+
+2010-Jan-14 (published)
+Automated Process
+
+Applicable current Ephemeris = 100114R_SCPSE_09339_09355.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 100103_123T64
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.15858903 37940585.22578886
+BODY699_GM 37931207.5900 37931207.6569
+BODY699_POLE_RA(1) 40.585776 40.585759
+BODY699_POLE_DEC(1) 83.537549 83.537556
+BODY699_JCOEF(2) 0.016290740684 0.016290741015
+BODY699_JCOEF(4) -0.000935384506 -0.000935387473
+BODY699_JCOEF(6) 0.000088616052 0.000088500228
+BODY601_GM 2.502444361443687 2.502446043296527
+BODY602_GM 7.216019322193621 7.215994919166206
+BODY603_GM 41.22364199485792 41.22362671256990
+BODY604_GM 73.11544873759908 73.11544724167149
+BODY605_GM 153.9436018626194 153.9435653494335
+BODY606_GM 8978.139733770831 8978.139773741363
+BODY607_GM 0.371729621214713 0.371704406193575
+BODY608_GM 120.5026255303498 120.5029631980470
+BODY609_GM 0.5533749729146867 0.5533689173792706
+
+2010-Jan-13 (published)
+Automated Process
+
+Applicable current Ephemeris = 100113R_SCPSE_09317_09339.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 091214_122T63
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.16056534 37940585.15858903
+BODY699_GM 37931207.5928 37931207.5900
+BODY699_POLE_RA(1) 40.585833 40.585776
+BODY699_POLE_DEC(1) 83.537546 83.537549
+BODY699_JCOEF(2) 0.016290730583 0.016290740684
+BODY699_JCOEF(4) -0.000935329227 -0.000935384506
+BODY699_JCOEF(6) 0.000089137743 0.000088616052
+BODY601_GM 2.502448263194753 2.502444361443687
+BODY602_GM 7.215373106036623 7.216019322193621
+BODY602_JCOEF(2) 0.00860000 0.00897000
+BODY602_CCOEF(3) 0.0020000000 0.0020800000
+BODY603_GM 41.22365223268523 41.22364199485792
+BODY604_GM 73.11544209566517 73.11544873759908
+BODY605_GM 153.9428691775221 153.9436018626194
+BODY606_GM 8978.139780362366 8978.139733770831
+BODY607_GM 0.371729681348213 0.371729621214713
+BODY608_GM 120.5030146074768 120.5026255303498
+BODY609_GM 0.5534091650364432 0.5533749729146867
+
+2010-Jan-07 (published)
+Automated Process
+
+Applicable current Ephemeris = 100107R_SCPSE_09296_09317.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 091122_121E8
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.09116724 37940585.16056534
+BODY699_GM 37931207.5249 37931207.5928
+BODY699_POLE_RA(1) 40.585508 40.585833
+BODY699_POLE_DEC(1) 83.537554 83.537546
+BODY699_JCOEF(2) 0.016290731107 0.016290730583
+BODY699_JCOEF(4) -0.000935289052 -0.000935329227
+BODY699_JCOEF(6) 0.000089393653 0.000089137743
+BODY601_GM 2.502454613265376 2.502448263194753
+BODY602_GM 7.213717239668965 7.215373106036623
+BODY602_JCOEF(2) 0.00897000 0.00860000
+BODY602_CCOEF(3) 0.0020800000 0.0020000000
+BODY603_GM 41.22368226514975 41.22365223268523
+BODY604_GM 73.11541351216987 73.11544209566517
+BODY605_GM 153.9428287523109 153.9428691775221
+BODY606_GM 8978.139735367682 8978.139780362366
+BODY607_GM 0.371723892177733 0.371729681348213
+BODY608_GM 120.5033436971190 120.5030146074768
+BODY609_GM 0.5534119652050336 0.5534091650364432
+
+2009-Dec-09 (published)
+Automated Process
+
+Applicable current Ephemeris = 091208R_SCPSE_09275_09296.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 091105_120E7
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.03276838 37940585.09116724
+BODY699_GM 37931207.4714 37931207.5249
+BODY699_POLE_RA(1) 40.585279 40.585508
+BODY699_POLE_DEC(1) 83.537547 83.537554
+BODY699_JCOEF(2) 0.016290735072 0.016290731107
+BODY699_JCOEF(4) -0.000935111838 -0.000935289052
+BODY699_JCOEF(6) 0.000090315814 0.000089393653
+BODY601_GM 2.502475635558650 2.502454613265376
+BODY602_GM 7.208253760083588 7.213717239668965
+BODY603_GM 41.22378316253346 41.22368226514975
+BODY604_GM 73.11535293474266 73.11541351216987
+BODY605_GM 153.9428336666086 153.9428287523109
+BODY606_GM 8978.139773285628 8978.139735367682
+BODY607_GM 0.371665390265868 0.371723892177733
+BODY608_GM 120.5038438413984 120.5033436971190
+BODY609_GM 0.5533933559394255 0.5534119652050336
+
+2009-Nov-18 (published)
+Automated Process
+
+Applicable current Ephemeris = 091116R_SCPSE_09231_09275.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 091016_118T62
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.02015772 37940585.03276838
+BODY699_GM 37931207.4585 37931207.4714
+BODY699_POLE_RA(1) 40.585339 40.585279
+BODY699_POLE_DEC(1) 83.537538 83.537547
+BODY699_JCOEF(2) 0.016290728848 0.016290735072
+BODY699_JCOEF(4) -0.000935100646 -0.000935111838
+BODY699_JCOEF(6) 0.000090361294 0.000090315814
+BODY601_GM 2.502473662855939 2.502475635558650
+BODY602_GM 7.207829867198577 7.208253760083588
+BODY603_GM 41.22376135313479 41.22378316253346
+BODY604_GM 73.11534875998363 73.11535293474266
+BODY605_GM 153.9428426421361 153.9428336666086
+BODY606_GM 8978.139712993554 8978.139773285628
+BODY607_GM 0.371706132043968 0.371665390265868
+BODY608_GM 120.5046024195398 120.5038438413984
+BODY609_GM 0.5533978648353445 0.5533933559394255
+
+2009-Oct-07 (published)
+Automated Process
+
+Applicable current Ephemeris = 091005AP_SCPSE_09248_17265.XSP
+Restrictions/Limitations = Used for planning for the duration of the file.
+Reference/Source of new values = 090903_118T62
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.65797564 37940585.02015772
+BODY699_GM 37931207.1063 37931207.4585
+BODY699_POLE_RA(1) 40.584440 40.585339
+BODY699_POLE_RA(2) -0.077682 -0.078714
+BODY699_POLE_DEC(1) 83.537474 83.537538
+BODY699_POLE_DEC(2) -0.002560 -0.002593
+BODY699_JCOEF(2) 0.016290772291 0.016290728848
+BODY699_JCOEF(4) -0.000934349536 -0.000935100646
+BODY699_JCOEF(6) 0.000092641174 0.000090361294
+BODY601_GM 2.502540299154720 2.502473662855939
+BODY602_GM 7.199143776956102 7.207829867198577
+BODY603_GM 41.21630049528812 41.22376135313479
+BODY604_GM 73.11462427344662 73.11534875998363
+BODY605_GM 153.9429961290159 153.9428426421361
+BODY606_GM 8978.139098895999 8978.139712993554
+BODY607_GM 0.371336843250265 0.371706132043968
+BODY608_GM 120.5121366316792 120.5046024195398
+BODY609_GM 0.5535358693227870 0.5533978648353445
+
+2009-Sep-24 (published)
+Automated Process
+
+Applicable current Ephemeris = 090924R_SCPSE_09215_09231.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090828_117T61
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.66693778 37940584.65797564
+BODY699_GM 37931207.1203 37931207.1063
+BODY699_POLE_RA(1) 40.584460 40.584440
+BODY699_POLE_DEC(1) 83.537511 83.537474
+BODY699_JCOEF(2) 0.016290819768 0.016290772291
+BODY699_JCOEF(4) -0.000934423051 -0.000934349536
+BODY699_JCOEF(6) 0.000091378573 0.000092641174
+BODY601_GM 2.502529277804900 2.502540299154720
+BODY602_GM 7.201941809221156 7.199143776956102
+BODY603_GM 41.21647784535888 41.21630049528812
+BODY604_GM 73.11465326768231 73.11462427344662
+BODY605_GM 153.9430787943620 153.9429961290159
+BODY606_GM 8978.139238159505 8978.139098895999
+BODY607_GM 0.371323170984844 0.371336843250265
+BODY608_GM 120.5039064835442 120.5121366316792
+BODY609_GM 0.5534758495938736 0.5535358693227870
+
+2009-Sep-22 (published)
+Automated Process
+
+Applicable current Ephemeris = 090921R_SCPSE_09200_09215.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090810_116T60
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.70866594 37940584.66693778
+BODY699_GM 37931207.1597 37931207.1203
+BODY699_POLE_RA(1) 40.584646 40.584460
+BODY699_POLE_DEC(1) 83.537510 83.537511
+BODY699_JCOEF(2) 0.016290820193 0.016290819768
+BODY699_JCOEF(4) -0.000934488379 -0.000934423051
+BODY699_JCOEF(6) 0.000091048774 0.000091378573
+BODY601_GM 2.502526714253576 2.502529277804900
+BODY602_GM 7.204128393822666 7.201941809221156
+BODY603_GM 41.21643705156555 41.21647784535888
+BODY604_GM 73.11467812476211 73.11465326768231
+BODY605_GM 153.9430863480677 153.9430787943620
+BODY606_GM 8978.139270340744 8978.139238159505
+BODY607_GM 0.371283234316610 0.371323170984844
+BODY608_GM 120.5040974359097 120.5039064835442
+BODY609_GM 0.5534910265088943 0.5534758495938736
+
+2009-Aug-17 (published)
+Automated Process
+
+Applicable current Ephemeris = 090817R_SCPSE_09184_09200.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090727_115T59
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.69981475 37940584.70866594
+BODY699_GM 37931207.1530 37931207.1597
+BODY699_POLE_RA(1) 40.584632 40.584646
+BODY699_POLE_DEC(1) 83.537505 83.537510
+BODY699_JCOEF(2) 0.016290814989 0.016290820193
+BODY699_JCOEF(4) -0.000934442184 -0.000934488379
+BODY699_JCOEF(6) 0.000091417534 0.000091048774
+BODY601_GM 2.502527494064343 2.502526714253576
+BODY602_GM 7.202142639487098 7.204128393822666
+BODY603_GM 41.21646288247825 41.21643705156555
+BODY604_GM 73.11464936300638 73.11467812476211
+BODY605_GM 153.9430565154396 153.9430863480677
+BODY606_GM 8978.139419438765 8978.139270340744
+BODY607_GM 0.371355483637583 0.371283234316610
+BODY608_GM 120.5037677365865 120.5040974359097
+BODY609_GM 0.5534816653469494 0.5534910265088943
+
+2009-Aug-06 (published)
+Automated Process
+
+Applicable current Ephemeris = 090806R_SCPSE_09168_09184.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090710_114T58
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.53093457 37940584.69981475
+BODY699_GM 37931206.9833 37931207.1530
+BODY699_POLE_RA(1) 40.584685 40.584632
+BODY699_POLE_DEC(1) 83.537493 83.537505
+BODY699_JCOEF(2) 0.016290815947 0.016290814989
+BODY699_JCOEF(4) -0.000934359844 -0.000934442184
+BODY699_JCOEF(6) 0.000091606222 0.000091417534
+BODY601_GM 2.502537156770620 2.502527494064343
+BODY602_GM 7.201056306132469 7.202142639487098
+BODY603_GM 41.21648344845686 41.21646288247825
+BODY604_GM 73.11463634344963 73.11464936300638
+BODY605_GM 153.9430477770478 153.9430565154396
+BODY606_GM 8978.139168628506 8978.139419438765
+BODY607_GM 0.371496424973641 0.371355483637583
+BODY608_GM 120.5056888490891 120.5037677365865
+BODY609_GM 0.5534819048142049 0.5534816653469494
+
+2009-Jul-08 (published)
+Automated Process
+
+Applicable current Ephemeris = 090708R_SCPSE_09153_09168.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090626_113T57
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.71483988 37940584.53093457
+BODY699_GM 37931207.1673 37931206.9833
+BODY699_POLE_RA(1) 40.584923 40.584685
+BODY699_POLE_DEC(1) 83.537522 83.537493
+BODY699_JCOEF(2) 0.016290793712 0.016290815947
+BODY699_JCOEF(4) -0.000934709423 -0.000934359844
+BODY699_JCOEF(6) 0.000090908483 0.000091606222
+BODY601_GM 2.502492017198180 2.502537156770620
+BODY602_GM 7.204291351372671 7.201056306132469
+BODY603_GM 41.21637470288032 41.21648344845686
+BODY604_GM 73.11467949836259 73.11463634344963
+BODY605_GM 153.9431111979202 153.9430477770478
+BODY606_GM 8978.139491416670 8978.139168628506
+BODY607_GM 0.370991166709194 0.371496424973641
+BODY608_GM 120.5026713407083 120.5056888490891
+BODY609_GM 0.5534654353131513 0.5534819048142049
+
+2009-Jul-01 (published)
+Automated Process
+
+Applicable current Ephemeris = 090701R_SCPSE_09136_09153.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090609_112T56
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.72257956 37940584.71483988
+BODY699_GM 37931207.1765 37931207.1673
+BODY699_POLE_RA(1) 40.584630 40.584923
+BODY699_POLE_DEC(1) 83.537540 83.537522
+BODY699_JCOEF(2) 0.016290787250 0.016290793712
+BODY699_JCOEF(4) -0.000934733160 -0.000934709423
+BODY699_JCOEF(6) 0.000091418329 0.000090908483
+BODY601_GM 2.502479294868557 2.502492017198180
+BODY602_GM 7.202798775360185 7.204291351372671
+BODY603_GM 41.21624413197247 41.21637470288032
+BODY604_GM 73.11466057947915 73.11467949836259
+BODY605_GM 153.9430434766724 153.9431111979202
+BODY606_GM 8978.139573866585 8978.139491416670
+BODY607_GM 0.370832695912033 0.370991166709194
+BODY608_GM 120.5030445679196 120.5026713407083
+BODY609_GM 0.5534401160635997 0.5534654353131513
+
+2009-Jun-24 (published)
+Automated Process
+
+Applicable current Ephemeris = 090624R_SCPSE_09120_09136.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090526_111T55
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.75892913 37940584.72257956
+BODY699_GM 37931207.2088 37931207.1765
+BODY699_POLE_RA(1) 40.582542 40.584630
+BODY699_POLE_RA(2) -0.037432 -0.077682
+BODY699_POLE_DEC(1) 83.537652 83.537540
+BODY699_POLE_DEC(2) -0.004944 -0.002560
+BODY699_JCOEF(2) 0.016290758527 0.016290787250
+BODY699_JCOEF(4) -0.000935166069 -0.000934733160
+BODY699_JCOEF(6) 0.000089537218 0.000091418329
+BODY601_GM 2.502480071324441 2.502479294868557
+BODY602_GM 7.207489777875368 7.202798775360185
+BODY603_GM 41.21590409811643 41.21624413197247
+BODY604_GM 73.11480925384234 73.11466057947915
+BODY605_GM 153.9430369538330 153.9430434766724
+BODY606_GM 8978.139616255658 8978.139573866585
+BODY607_GM 0.370625094690230 0.370832695912033
+BODY608_GM 120.5027152141226 120.5030445679196
+BODY609_GM 0.5534265033291642 0.5534401160635997
+
+2009-Jun-11 (published)
+Automated Process
+
+Applicable current Ephemeris = 090609R_SCPSE_09104_09120.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090507_110T54
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.79518565 37940584.75892913
+BODY699_GM 37931207.2468 37931207.2088
+BODY699_POLE_RA(1) 40.582443 40.582542
+BODY699_POLE_DEC(1) 83.537663 83.537652
+BODY699_JCOEF(2) 0.016290749081 0.016290758527
+BODY699_JCOEF(4) -0.000935197591 -0.000935166069
+BODY699_JCOEF(6) 0.000089824771 0.000089537218
+BODY601_GM 2.502496382974899 2.502480071324441
+BODY602_GM 7.206671212324381 7.207489777875368
+BODY603_GM 41.21592046942041 41.21590409811643
+BODY604_GM 73.11481317140027 73.11480925384234
+BODY605_GM 153.9429742206838 153.9430369538330
+BODY606_GM 8978.139782617298 8978.139616255658
+BODY607_GM 0.370661213500527 0.370625094690230
+BODY608_GM 120.5016238558722 120.5027152141226
+BODY609_GM 0.5534054527005198 0.5534265033291642
+
+2009-May-21 (published)
+Automated Process
+
+Applicable current Ephemeris = 090520R_SCPSE_09089_09104.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090422_109T53
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940583.83670486 37940584.79518565
+BODY699_GM 37931206.2896 37931207.2468
+BODY699_POLE_RA(1) 40.581567 40.582443
+BODY699_POLE_RA(2) -0.037353 -0.037432
+BODY699_POLE_DEC(1) 83.537702 83.537663
+BODY699_POLE_DEC(2) -0.004933 -0.004944
+BODY699_JCOEF(2) 0.016290750592 0.016290749081
+BODY699_JCOEF(4) -0.000934942751 -0.000935197591
+BODY699_JCOEF(6) 0.000089655803 0.000089824771
+BODY601_GM 2.502375745139359 2.502496382974899
+BODY602_GM 7.200775737205724 7.206671212324381
+BODY603_GM 41.21611289570998 41.21592046942041
+BODY604_GM 73.11472484717956 73.11481317140027
+BODY605_GM 153.9429469769423 153.9429742206838
+BODY606_GM 8978.139106855113 8978.139782617298
+BODY607_GM 0.371190991373805 0.370661213500527
+BODY608_GM 120.5062324337800 120.5016238558722
+BODY609_GM 0.5536043842359156 0.5534054527005198
+
+2009-May-07 (published)
+Automated Process
+
+Applicable current Ephemeris = 090507R_SCPSE_09075_09089.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090407_107T52
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.04339046 37940583.83670486
+BODY699_GM 37931206.4966 37931206.2896
+BODY699_POLE_RA(1) 40.581934 40.581567
+BODY699_POLE_DEC(1) 83.537693 83.537702
+BODY699_JCOEF(2) 0.016290732957 0.016290750592
+BODY699_JCOEF(4) -0.000935091860 -0.000934942751
+BODY699_JCOEF(6) 0.000089451150 0.000089655803
+BODY601_GM 2.502415585318155 2.502375745139359
+BODY602_GM 7.203519438374520 7.200775737205724
+BODY603_GM 41.21599214744679 41.21611289570998
+BODY604_GM 73.11474559066438 73.11472484717956
+BODY605_GM 153.9427553435824 153.9429469769423
+BODY606_GM 8978.138922629163 8978.139106855113
+BODY607_GM 0.371620801197215 0.371190991373805
+BODY608_GM 120.5032558591434 120.5062324337800
+BODY609_GM 0.5535208221133412 0.5536043842359156
+
+2009-Apr-23 (published)
+Automated Process
+
+Applicable current Ephemeris = 090423R_SCPSE_09028_09075.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090328_103T51
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.95180942 37940584.04339046
+BODY699_GM 37931207.3882 37931206.4966
+BODY699_POLE_RA(1) 40.582774 40.581934
+BODY699_POLE_RA(2) -0.036427 -0.037353
+BODY699_POLE_DEC(1) 83.537685 83.537693
+BODY699_POLE_DEC(2) -0.004811 -0.004933
+BODY699_JCOEF(2) 0.016290704214 0.016290732957
+BODY699_JCOEF(4) -0.000935307318 -0.000935091860
+BODY699_JCOEF(6) 0.000090619956 0.000089451150
+BODY601_GM 2.502321711007510 2.502415585318155
+BODY602_GM 7.208313972796445 7.203519438374520
+BODY603_GM 41.21604378398847 41.21599214744679
+BODY604_GM 73.11493826230807 73.11474559066438
+BODY605_GM 153.9431057300922 153.9427553435824
+BODY606_GM 8978.141024766712 8978.138922629163
+BODY607_GM 0.370344781190025 0.371620801197215
+BODY608_GM 120.5141263265947 120.5032558591434
+BODY609_GM 0.5533540349512766 0.5535208221133412
+
+2009-Feb-26 (published)
+Automated Process
+
+Applicable current Ephemeris = 090225R_SCPSE_08350_09028.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 090209_098T50
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.89169871 37940584.95180942
+BODY699_GM 37931207.3416 37931207.3882
+BODY699_POLE_RA(1) 40.582649 40.582774
+BODY699_POLE_DEC(1) 83.537663 83.537685
+BODY699_JCOEF(2) 0.016290684865 0.016290704214
+BODY699_JCOEF(4) -0.000935283514 -0.000935307318
+BODY699_JCOEF(6) 0.000090997196 0.000090619956
+BODY601_GM 2.502352850175356 2.502321711007510
+BODY602_GM 7.207600997452297 7.208313972796445
+BODY603_GM 41.21601112668976 41.21604378398847
+BODY604_GM 73.11488499625567 73.11493826230807
+BODY605_GM 153.9430894153115 153.9431057300922
+BODY606_GM 8978.140680747552 8978.141024766712
+BODY607_GM 0.370996212157831 0.370344781190025
+BODY608_GM 120.5012562767647 120.5141263265947
+BODY609_GM 0.5532629207784916 0.5533540349512766
+
+2009-Feb-02 (published)
+Automated Process
+
+Applicable current Ephemeris = 090202R_SCPSE_08334_08350.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 081228_096T49
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.82205020 37940584.89169871
+BODY699_GM 37931207.2631 37931207.3416
+BODY699_POLE_RA(1) 40.582848 40.582649
+BODY699_POLE_DEC(1) 83.537650 83.537663
+BODY699_JCOEF(2) 0.016290658170 0.016290684865
+BODY699_JCOEF(4) -0.000935427563 -0.000935283514
+BODY699_JCOEF(6) 0.000090378797 0.000090997196
+BODY601_GM 2.502374087988651 2.502352850175356
+BODY602_GM 7.208518568446848 7.207600997452297
+BODY603_GM 41.21613638955037 41.21601112668976
+BODY604_GM 73.11487574250081 73.11488499625567
+BODY605_GM 153.9429874323952 153.9430894153115
+BODY606_GM 8978.140131197120 8978.140680747552
+BODY607_GM 0.371644267058727 0.370996212157831
+BODY608_GM 120.5090171536813 120.5012562767647
+BODY609_GM 0.5532158104637386 0.5532629207784916
+
+2009-Jan-20 (published)
+Automated Process
+
+Applicable current Ephemeris = 090120R_SCPSE_08319_08334.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 081208_094T48
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.81290928 37940584.82205020
+BODY699_GM 37931207.2702 37931207.2631
+BODY699_POLE_RA(1) 40.582892 40.582848
+BODY699_POLE_RA(2) -0.036197 -0.036427
+BODY699_POLE_DEC(1) 83.537692 83.537650
+BODY699_POLE_DEC(2) -0.004781 -0.004811
+BODY699_JCOEF(2) 0.016290683480 0.016290658170
+BODY699_JCOEF(4) -0.000935187071 -0.000935427563
+BODY699_JCOEF(6) 0.000090351241 0.000090378797
+BODY601_GM 2.502553353261852 2.502374087988651
+BODY602_GM 7.198024751397580 7.208518568446848
+BODY603_GM 41.20680547202384 41.21613638955037
+BODY604_GM 73.11493779546134 73.11487574250081
+BODY605_GM 153.9429514952013 153.9429874323952
+BODY606_GM 8978.139760858710 8978.140131197120
+BODY606_JCOEF(2) 0.00003676 0.00003345
+BODY606_CCOEF(3) 0.0000098144 0.0000100225
+BODY606_SCOEF(3) 0.0000000290 0.0000002649
+BODY607_GM 0.371733822034568 0.371644267058727
+BODY608_GM 120.5126935476018 120.5090171536813
+BODY609_GM 0.5532268430393127 0.5532158104637386
+
+2008-Dec-17 (published)
+Automated Process
+
+Applicable current Ephemeris = 081217R_SCPSE_08294_08319.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 081122_091T47
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.75080759 37940584.81290928
+BODY699_GM 37931207.2159 37931207.2702
+BODY699_POLE_RA(1) 40.583018 40.582892
+BODY699_POLE_DEC(1) 83.537706 83.537692
+BODY699_JCOEF(2) 0.016290787300 0.016290683480
+BODY699_JCOEF(4) -0.000935059549 -0.000935187071
+BODY699_JCOEF(6) 0.000088909124 0.000090351241
+BODY601_GM 2.502593891311248 2.502553353261852
+BODY602_GM 7.198495850305284 7.198024751397580
+BODY603_GM 41.20585579154643 41.20680547202384
+BODY604_GM 73.11498772669157 73.11493779546134
+BODY605_GM 153.9427416028387 153.9429514952013
+BODY606_GM 8978.139141085363 8978.139760858710
+BODY607_GM 0.372318766963366 0.371733822034568
+BODY608_GM 120.5055433851675 120.5126935476018
+BODY609_GM 0.5532116571684228 0.5532268430393127
+
+2008-Dec-03 (published)
+Automated Process
+
+Applicable current Ephemeris = 081126R_SCPSE_08272_08294.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 081106_089T46
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.84323245 37940584.75080759
+BODY699_GM 37931207.3105 37931207.2159
+BODY699_POLE_RA(1) 40.583620 40.583018
+BODY699_POLE_DEC(1) 83.537762 83.537706
+BODY699_JCOEF(2) 0.016290692878 0.016290787300
+BODY699_JCOEF(4) -0.000935823729 -0.000935059549
+BODY699_JCOEF(6) 0.000088632421 0.000088909124
+BODY601_GM 2.502623200887248 2.502593891311248
+BODY602_GM 7.205883040951948 7.198495850305284
+BODY603_GM 41.20624377144850 41.20585579154643
+BODY604_GM 73.11470507883155 73.11498772669157
+BODY605_GM 153.9428866862459 153.9427416028387
+BODY606_GM 8978.139092755462 8978.139141085363
+BODY607_GM 0.372242134056882 0.372318766963366
+BODY608_GM 120.4957900045622 120.5055433851675
+BODY609_GM 0.5532380113023578 0.5532116571684228
+
+2008-Oct-31 (published)
+Automated Process
+
+Applicable current Ephemeris = 081031R_SCPSE_08220_08272.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 081011_081E5
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.84137087 37940584.84323245
+BODY699_GM 37931207.2963 37931207.3105
+BODY699_POLE_RA(1) 40.582020 40.583620
+BODY699_POLE_RA(2) -0.032010 -0.036197
+BODY699_POLE_DEC(1) 83.537784 83.537762
+BODY699_POLE_DEC(2) -0.005401 -0.004781
+BODY699_JCOEF(2) 0.016290697495 0.016290692878
+BODY699_JCOEF(4) -0.000935250961 -0.000935823729
+BODY699_JCOEF(6) 0.000091782033 0.000088632421
+BODY601_GM 2.502706597774052 2.502623200887248
+BODY602_GM 7.206763681178778 7.205883040951948
+BODY603_GM 41.20803428037864 41.20624377144850
+BODY604_GM 73.11435544930634 73.11470507883155
+BODY605_GM 153.9427846135544 153.9428866862459
+BODY606_GM 8978.139988036010 8978.139092755462
+BODY606_JCOEF(2) 0.00003495 0.00003676
+BODY606_CCOEF(3) 0.0000098881 0.0000098144
+BODY606_SCOEF(3) 0.0000002774 0.0000000290
+BODY607_GM 0.371532363950584 0.372242134056882
+BODY608_GM 120.5055685912496 120.4957900045622
+BODY609_GM 0.5533328348407409 0.5532380113023578
+
+2008-Sep-16 (published)
+Automated Process
+
+Applicable current Ephemeris = 080916R_SCPSE_08206_08220.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080816_079E4
+
+Parameter Superceded Value New Value
+
+BODY10_GM 132712440044.2083 132712440040.9446
+BODY2_GM 324858.598890645 324858.592000001
+BODY3_GM 403503.2335605171 403503.2363095674
+BODY399_GM 398600.4334392727 398600.4362333397
+BODY5_GM 126712764.8582231 126712764.8000003
+BODY599_GM 126686533.9614931 126686533.9032703
+BODY6_GM 37940584.38475962 37940584.84137087
+BODY699_GM 37931206.8370 37931207.2963
+BODY699_POLE_RA(1) 40.581443 40.582020
+BODY699_POLE_RA(2) -0.027530 -0.032010
+BODY699_POLE_DEC(1) 83.537728 83.537784
+BODY699_POLE_DEC(2) -0.004758 -0.005401
+BODY699_JCOEF(2) 0.016290733302 0.016290697495
+BODY699_JCOEF(4) -0.000935178259 -0.000935250961
+BODY699_JCOEF(6) 0.000095739859 0.000091782033
+BODY7_GM 5794549.008216757 5794548.600000031
+BODY301_GM 4902.800121244415 4902.800076227743
+BODY601_GM 2.502670647164671 2.502706597774052
+BODY602_GM 7.208136538970446 7.206763681178778
+BODY603_GM 41.21476543489587 41.20803428037864
+BODY604_GM 73.11300597304992 73.11435544930634
+BODY605_GM 153.9422805538818 153.9427846135544
+BODY606_GM 8978.139418614695 8978.139988036010
+BODY606_JCOEF(2) 0.00003681 0.00003495
+BODY606_CCOEF(3) 0.0000098158 0.0000098881
+BODY606_SCOEF(3) 0.0000000344 0.0000002774
+BODY607_GM 0.371344544273395 0.371532363950584
+BODY608_GM 120.5027082136875 120.5055685912496
+BODY609_GM 0.5534003114787691 0.5533328348407409
+
+2008-Sep-05 (published)
+Automated Process
+
+Applicable current Ephemeris = 080819R_SCPSE_08141_08206.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080803_070Sa
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.15980972 37940584.38475962
+BODY699_GM 37931206.6163 37931206.8370
+BODY699_POLE_RA(1) 40.581466 40.581443
+BODY699_POLE_DEC(1) 83.537709 83.537728
+BODY699_JCOEF(2) 0.016290704643 0.016290733302
+BODY699_JCOEF(4) -0.000935189240 -0.000935178259
+BODY699_JCOEF(6) 0.000096466048 0.000095739859
+BODY601_GM 2.502881776228512 2.502670647164671
+BODY602_GM 7.208734879056464 7.208136538970446
+BODY603_GM 41.21355138275547 41.21476543489587
+BODY604_GM 73.11290544686008 73.11300597304992
+BODY605_GM 153.9422746808738 153.9422805538818
+BODY606_GM 8978.139081588426 8978.139418614695
+BODY606_JCOEF(2) 0.00003676 0.00003681
+BODY606_CCOEF(3) 0.0000098144 0.0000098158
+BODY606_SCOEF(3) 0.0000000290 0.0000000344
+BODY607_GM 0.371434289398711 0.371344544273395
+BODY608_GM 120.4992477407413 120.5027082136875
+
+2008-Jun-18 (published)
+Automated Process
+
+Applicable current Ephemeris = 080618R_SCPSE_08126_08141.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080602_068T44
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.17743508 37940584.15980972
+BODY699_GM 37931206.6349 37931206.6163
+BODY699_POLE_RA(1) 40.581827 40.581466
+BODY699_POLE_DEC(1) 83.537703 83.537709
+BODY699_JCOEF(2) 0.016290716594 0.016290704643
+BODY699_JCOEF(4) -0.000935672409 -0.000935189240
+BODY699_JCOEF(6) 0.000094389114 0.000096466048
+BODY601_GM 2.502881955220740 2.502881776228512
+BODY602_GM 7.210410824718255 7.208734879056464
+BODY603_GM 41.21262070849623 41.21355138275547
+BODY604_GM 73.11291911924228 73.11290544686008
+BODY605_GM 153.9422199461879 153.9422746808738
+BODY606_GM 8978.138986415834 8978.139081588426
+BODY607_GM 0.371129805972588 0.371434289398711
+BODY608_GM 120.4976975847023 120.4992477407413
+BODY609_GM 0.5537090403439990 0.5534003114787691
+
+2008-Jun-06 (published)
+Automated Process
+
+Applicable current Ephemeris = 080605R_SCPSE_08078_08126.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080516_063T43
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.27667402 37940584.17743508
+BODY699_GM 37931206.7269 37931206.6349
+BODY699_POLE_RA(1) 40.581871 40.581827
+BODY699_POLE_DEC(1) 83.537722 83.537703
+BODY699_JCOEF(2) 0.016290694906 0.016290716594
+BODY699_JCOEF(4) -0.000935647674 -0.000935672409
+BODY699_JCOEF(6) 0.000094680606 0.000094389114
+BODY601_GM 2.502935187158320 2.502881955220740
+BODY602_GM 7.210716312905534 7.210410824718255
+BODY602_JCOEF(2) 0.00880584 0.00897000
+BODY602_CCOEF(3) 0.0014554727 0.0020800000
+BODY603_GM 41.21188522645834 41.21262070849623
+BODY604_GM 73.11293489316252 73.11291911924228
+BODY605_GM 153.9422268415005 153.9422199461879
+BODY606_GM 8978.138927320846 8978.138986415834
+BODY607_GM 0.371120905579017 0.371129805972588
+BODY608_GM 120.5052569914020 120.4976975847023
+BODY609_GM 0.5537536295128821 0.5537090403439990
+
+2008-May-15 (published)
+Automated Process
+
+Applicable current Ephemeris = 080515R_SCPSE_08067_08078.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080331_062T42
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.35143083 37940584.27667402
+BODY699_GM 37931206.8047 37931206.7269
+BODY699_POLE_RA(1) 40.581833 40.581871
+BODY699_POLE_DEC(1) 83.537765 83.537722
+BODY699_JCOEF(2) 0.016290674404 0.016290694906
+BODY699_JCOEF(4) -0.000935829230 -0.000935647674
+BODY699_JCOEF(6) 0.000093971390 0.000094680606
+BODY601_GM 2.502920537306806 2.502935187158320
+BODY602_GM 7.211083813192880 7.210716312905534
+BODY602_JCOEF(2) 0.00877236 0.00880584
+BODY602_CCOEF(3) 0.0014999008 0.0014554727
+BODY603_GM 41.21181926660137 41.21188522645834
+BODY604_GM 73.11292310928664 73.11293489316252
+BODY605_GM 153.9422173029270 153.9422268415005
+BODY606_GM 8978.138994952336 8978.138927320846
+BODY607_GM 0.370895155476839 0.371120905579017
+BODY608_GM 120.5021858690953 120.5052569914020
+BODY609_GM 0.5537337090249409 0.5537536295128821
+
+2008-May-02 (published)
+Automated Process
+
+Applicable current Ephemeris = 080428R_SCPSE_08045_08067.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080313_060E3
+
+Parameter Superceded Value New Value
+
+BODY10_GM 132712440040.0565 132712440044.2083
+BODY2_GM 324858.592000000 324858.598890645
+BODY3_GM 403503.2363068672 403503.2335605171
+BODY399_GM 398600.4362002230 398600.4334392727
+BODY5_GM 126712764.8000000 126712764.8582231
+BODY599_GM 126686533.9032700 126686533.9614931
+BODY6_GM 37940585.27338909 37940584.35143083
+BODY699_GM 37931207.7282 37931206.8047
+BODY699_POLE_RA(1) 40.581505 40.581833
+BODY699_POLE_DEC(1) 83.537689 83.537765
+BODY699_JCOEF(2) 0.016290505727 0.016290674404
+BODY699_JCOEF(4) -0.000936733745 -0.000935829230
+BODY699_JCOEF(6) 0.000086349193 0.000093971390
+BODY7_GM 5794548.600000000 5794549.008216757
+BODY301_GM 4902.800106644209 4902.800121244415
+BODY601_GM 2.503681306799234 2.502920537306806
+BODY602_GM 7.207438711629040 7.211083813192880
+BODY602_JCOEF(2) 0.00897 0.00877236
+BODY602_CCOEF(3) 0.00208 0.0014999008
+BODY603_GM 41.21161107170069 41.21181926660137
+BODY604_GM 73.11303912442641 73.11292310928664
+BODY605_GM 153.9424389694393 153.9422173029270
+BODY606_GM 8978.137465374053 8978.138994952336
+BODY607_GM 0.372290582643009 0.370895155476839
+BODY608_GM 120.5036261119318 120.5021858690953
+BODY609_GM 0.5535544897385243 0.5537337090249409
+
+2008-Mar-28 (published)
+Automated Process
+
+Applicable current Ephemeris = 080327R_SCPSE_07365_08045.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080229_056T41
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.28350117 37940585.27338909
+BODY699_GM 37931207.7391 37931207.7282
+BODY699_POLE_RA(1) 40.582230 40.581505
+BODY699_POLE_DEC(1) 83.537656 83.537689
+BODY699_JCOEF(2) 0.016290539045 0.016290505727
+BODY699_JCOEF(4) -0.000936841920 -0.000936733745
+BODY699_JCOEF(6) 0.000085005705 0.000086349193
+BODY601_GM 2.503804640631195 2.503681306799234
+BODY602_GM 7.208113831972937 7.207438711629040
+BODY603_GM 41.21114295507989 41.21161107170069
+BODY604_GM 73.11294768194610 73.11303912442641
+BODY605_GM 153.9423849400276 153.9424389694393
+BODY606_GM 8978.137388790423 8978.137465374053
+BODY607_GM 0.372389672138376 0.372290582643009
+BODY608_GM 120.5026849890331 120.5036261119318
+BODY609_GM 0.5535191880496334 0.5535544897385243
+
+2008-Mar-10 (published)
+Automated Process
+
+Applicable current Ephemeris = 080307R_SCPSE_07345_07365.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 080108_055T40
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.27527665 37940585.28350117
+BODY699_GM 37931207.7325 37931207.7391
+BODY699_POLE_RA(1) 40.582098 40.582230
+BODY699_POLE_DEC(1) 83.537705 83.537656
+BODY699_JCOEF(2) 0.016290544651 0.016290539045
+BODY699_JCOEF(4) -0.000936905325 -0.000936841920
+BODY699_JCOEF(6) 0.000084843928 0.000085005705
+BODY601_GM 2.503914037088305 2.503804640631195
+BODY602_GM 7.208620862251065 7.208113831972937
+BODY603_GM 41.21095350743407 41.21114295507989
+BODY604_GM 73.11290742978323 73.11294768194610
+BODY605_GM 153.9424010118651 153.9423849400276
+BODY606_GM 8978.137327428010 8978.137388790423
+BODY607_GM 0.372366804799818 0.372389672138376
+BODY608_GM 120.5007708643355 120.5026849890331
+BODY609_GM 0.5535373313434467 0.5535191880496334
+
+2008-Jan-25 (published)
+Automated Process
+
+Applicable current Ephemeris = 080123R_SCPSE_07309_07329.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 071208_053T38
+
+Parameter Superceded Value New Value
+
+BODY10_GM 132712440044.2083 132712440040.0565
+BODY2_GM 324858.598890645 324858.592000000
+BODY3_GM 403503.2335605171 403503.2363068672
+BODY399_GM 398600.4334392727 398600.4362002230
+BODY5_GM 126712764.8582231 126712764.8000000
+BODY599_GM 126686533.9614931 126686533.9032700
+BODY6_GM 37940584.44408617 37940585.27527665
+BODY699_GM 37931206.9073 37931207.7325
+BODY699_POLE_RA(1) 40.581521 40.582098
+BODY699_POLE_DEC(1) 83.537644 83.537705
+BODY699_JCOEF(2) 0.016290556604 0.016290544651
+BODY699_JCOEF(4) -0.000936535883 -0.000936905325
+BODY699_JCOEF(6) 0.000087229074 0.000084843928
+BODY7_GM 5794549.008216757 5794548.600000000
+BODY301_GM 4902.800121244415 4902.800106644209
+BODY601_GM 2.503962504392251 2.503914037088305
+BODY602_GM 7.206462956405896 7.208620862251065
+BODY603_GM 41.21053911096154 41.21095350743407
+BODY604_GM 73.11296178124047 73.11290742978323
+BODY605_GM 153.9420079809344 153.9424010118651
+BODY606_GM 8978.138641652298 8978.137327428010
+BODY606_JCOEF(2) 0.00003300 0.00003676
+BODY606_CCOEF(3) 0.0000111800 0.0000098144
+BODY606_SCOEF(3) -0.0000003700 0.0000000290
+BODY607_GM 0.370879439084761 0.372366804799818
+BODY608_GM 120.4977883563631 120.5007708643355
+BODY609_GM 0.5535009498398994 0.5535373313434467
+
+2008-Jan-22 (published)
+Automated Process
+
+Applicable current Ephemeris = 080117R_SCPSE_07262_07309.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 071121_051T37
+
+
+Parameter Superceded Value New Value
+
+
+BODY6_GM 37940584.33316191 37940584.44408617
+BODY699_GM 37931206.7900 37931206.9073
+BODY699_POLE_RA(1) 40.581634 40.581521
+BODY699_POLE_DEC(1) 83.537653 83.537644
+BODY699_JCOEF(2) 0.016290573664 0.016290556604
+BODY699_JCOEF(4) -0.000936412164 -0.000936535883
+BODY699_JCOEF(6) 0.000087338436 0.000087229074
+BODY601_GM 2.503976507903127 2.503962504392251
+BODY602_GM 7.206823163853062 7.206462956405896
+BODY603_GM 41.21053825232565 41.21053911096154
+BODY604_GM 73.11294390332988 73.11296178124047
+BODY605_GM 153.9420572125665 153.9420079809344
+BODY606_GM 8978.138848070126 8978.138641652298
+BODY607_GM 0.370604084668938 0.370879439084761
+BODY608_GM 120.5039090692674 120.4977883563631
+BODY609_GM 0.5534188875932333 0.5535009498398994
+
+2007-Nov-27 (published)
+Automated Process
+
+Applicable current Ephemeris = 071127R_SCPSE_07221_07262.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 071004_050T36
+
+
+Parameter Superceded Value New Value
+
+
+BODY6_GM 37940584.84186901 37940584.33316191
+BODY699_GM 37931207.2884 37931206.7900
+BODY699_POLE_RA(1) 40.582641 40.581634
+BODY699_POLE_DEC(1) 83.537724 83.537653
+BODY699_JCOEF(2) 0.016290612479 0.016290573664
+BODY699_JCOEF(4) -0.000936294465 -0.000936412164
+BODY699_JCOEF(6) 0.000085698631 0.000087338436
+BODY601_GM 2.504049862130569 2.503976507903127
+BODY602_GM 7.209384148992843 7.206823163853062
+BODY603_GM 41.21155584587244 41.21053825232565
+BODY604_GM 73.11290828235806 73.11294390332988
+BODY605_GM 153.9424774264240 153.9420572125665
+BODY606_GM 8978.141570596494 8978.138848070126
+BODY607_GM 0.370570713135802 0.370604084668938
+BODY608_GM 120.5076093230218 120.5039090692674
+BODY609_GM 0.5533871680420684 0.5534188875932333
+
+2007-Oct-18 (published)
+Automated Process
+
+Applicable current Ephemeris = 071017R_SCPSE_07191_07221.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070902_049T35
+
+
+Parameter Superceded Value New Value
+
+
+BODY6_GM 37940584.84332670 37940584.84186901
+BODY699_GM 37931207.2932 37931207.2884
+BODY699_POLE_RA(1) 40.582430 40.582641
+BODY699_POLE_DEC(1) 83.537699 83.537724
+BODY699_JCOEF(2) 0.016290600706 0.016290612479
+BODY699_JCOEF(4) -0.000936283456 -0.000936294465
+BODY601_GM 2.504061092290415 2.504049862130569
+BODY602_GM 7.208392748901111 7.209384148992843
+BODY603_GM 41.21123661827443 41.21155584587244
+BODY604_GM 73.11288907130644 73.11290828235806
+BODY605_GM 153.9424024154587 153.9424774264240
+BODY606_GM 8978.141410813654 8978.141570596494
+BODY606_JCOEF(2) 0.00003601 0.00003300
+BODY606_CCOEF(3) 0.0000090887 0.0000111800
+BODY606_SCOEF(3) 0.0000006522 -0.0000003700
+BODY607_GM 0.370732118387213 0.370570713135802
+BODY608_GM 120.5055725066606 120.5076093230218
+BODY609_GM 0.5534083195746095 0.5533871680420684
+
+2007 August 23 (published)
+E. Martinez - modified by automated process
+
+Applicable current Ephemeris = 070822R_SCPSE_07170_07191.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070722_048T34
+
+
+Parameter Superceded Value New Value
+
+
+BODY6_GM 37940585.21293911 37940584.84332670
+BODY699_GM 37931207.6624 37931207.2932
+BODY699_POLE_RA(1) 40.582203 40.582430
+BODY699_POLE_DEC(1) 83.537758 83.537699
+BODY699_JCOEF(2) 0.016290558106 0.016290600706
+BODY699_JCOEF(4) -0.000936543536 -0.000936283456
+BODY601_GM 2.504123199124006 2.504061092290415
+BODY602_GM 7.208710372016743 7.208392748901111
+BODY603_GM 41.21112748400978 41.21123661827443
+BODY604_GM 73.11287036205675 73.11288907130644
+BODY605_GM 153.9423057334808 153.9424024154587
+BODY606_GM 8978.140644218034 8978.141410813654
+BODY606_JCOEF(2) 0.00003886 0.00003601
+BODY606_CCOEF(3) 0.0000090424 0.0000090887
+BODY606_SCOEF(3) 0.0000006837 0.0000006522
+BODY607_GM 0.371284081096715 0.370732118387213
+BODY608_GM 120.5060708891759 120.5055725066606
+BODY609_GM 0.5534250308405290 0.5534083195746095
+
+
+
+2007 July 30 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070727R_SCPSE_07155_07170.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070703_047T33
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.17856981 37940585.21293911
+BODY699_GM 37931207.6234 37931207.6624
+BODY699_POLE_RA(1) 40.581027 40.582203
+BODY699_POLE_DEC(1) 83.537733 83.537758
+BODY699_JCOEF(2) 0.016290499156 0.016290558106
+BODY699_JCOEF(4) -0.000936368414 -0.000936543536
+BODY699_JCOEF(6) 0.000085387817 0.000085698631
+BODY601_GM 2.504414142228290 2.504123199124006
+BODY602_GM 7.205528919131223 7.208710372016743
+BODY603_GM 41.21396906165625 41.21112748400978
+BODY604_GM 73.11211150967007 73.11287036205675
+BODY605_GM 153.9421896011184 153.9423057334808
+BODY606_GM 8978.144236041977 8978.140644218034
+BODY606_JCOEF(2) 0.00003300 0.00003886
+BODY606_CCOEF(3) 0.0000111800 0.0000090424
+BODY606_SCOEF(3) -0.0000003700 0.0000006837
+BODY607_GM 0.370612570883980 0.371284081096715
+BODY608_GM 120.5086247632435 120.5060708891759
+BODY609_GM 0.5535133733207492 0.5534250308405290
+
+
+2007 July 9 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070705R_SCPSE_07140_07155.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070616_046T32
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.08048513 37940585.17856981
+BODY699_GM 37931207.5251 37931207.6234
+BODY699_POLE_RA(1) 40.581004 40.581027
+BODY699_JCOEF(2) 0.016290501183 0.016290499156
+BODY699_JCOEF(4) -0.000936480581 -0.000936368414
+BODY601_GM 2.504411459582265 2.504414142228290
+BODY602_GM 7.205523796006839 7.205528919131223
+BODY603_GM 41.21397120396249 41.21396906165625
+BODY604_GM 73.11210641361994 73.11211150967007
+BODY605_GM 153.9421682125904 153.9421896011184
+BODY606_GM 8978.144146129685 8978.144236041977
+BODY607_GM 0.370679269434110 0.370612570883980
+BODY608_GM 120.5088834664148 120.5086247632435
+BODY609_GM 0.5535141277727101 0.5535133733207492
+
+
+
+2007 June 25 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070625R_SCPSE_07125_07140.XSP
+ Restrictions/Limitations = Use for analysis for period of file.
+ Reference/Source of new values = 070531_045T31
+ PCK Produced by NAVT (070531_045T31) = CASSINI_PCK_VERSION = ( '2007-JUN-25' )
+
+
+ Parameter Superceded Value New Value
+
+ BODY6_GM 37940585.40297550 37940585.08048513
+ BODY699_GM 37931207.8468 37931207.5251
+ BODY699_POLE_RA(1) 40.581249 40.581004
+ BODY699_POLE_DEC(1) 83.537722 83.537733
+ BODY699_JCOEF(2) 0.016290482169 0.016290501183
+ BODY699_JCOEF(4) -0.000936661780 -0.000936480581
+ BODY601_GM 2.504418526540353 2.504411459582265
+ BODY602_GM 7.205822825717696 7.205523796006839
+ BODY603_GM 41.21391693524110 41.21397120396249
+ BODY604_GM 73.11210744224974 73.11210641361994
+ BODY605_GM 153.9421724973921 153.9421682125904
+ BODY606_GM 8978.144706785964 8978.144146129685
+ BODY607_GM 0.370826890400237 0.370679269434110
+ BODY608_GM 120.5086965046577 120.5088834664148
+ BODY609_GM 0.5535193168614742 0.5535141277727101
+
+
+
+
+2007 June 06 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070605R_SCPSE_07106_07125.BSP
+Restrictions/Limitations =
+Reference/Source of new values = 070516_044T30
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.38628557 37940585.40297550
+BODY699_GM 37931207.8310 37931207.8468
+BODY699_POLE_RA(1) 40.581289 40.581249
+BODY699_POLE_DEC(1) 83.537733 83.537722
+BODY699_JCOEF(2) 0.016290481702 0.016290482169
+BODY699_JCOEF(4) -0.000936637437 -0.000936661780
+BODY601_GM 2.504419042580414 2.504418526540353
+BODY602_GM 7.205961922976411 7.205822825717696
+BODY603_GM 41.21392252150596 41.21391693524110
+BODY604_GM 73.11208204909212 73.11210744224974
+BODY605_GM 153.9421763278791 153.9421724973921
+BODY606_GM 8978.144552352178 8978.144706785964
+BODY607_GM 0.370847384392641 0.370826890400237
+BODY608_GM 120.5078146418220 120.5086965046577
+BODY609_GM 0.5535279925596653 0.5535193168614742
+
+
+
+2007 May 17 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070517R_SCPSE_07094_07106.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070429_043T29
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.09724870 37940585.38628557
+BODY699_GM 37931207.5551 37931207.8310
+BODY699_POLE_RA(1) 40.580883 40.581289
+BODY699_POLE_RA(2) -0.028212 -0.027530
+BODY699_POLE_DEC(1) 83.537754 83.537733
+BODY699_POLE_DEC(2) -0.005007 -0.004758
+BODY699_JCOEF(2) 0.016290487287 0.016290481702
+BODY699_JCOEF(4) -0.000936319857 -0.000936637437
+BODY699_JCOEF(6) 0.000085603492 0.000085387817
+BODY601_GM 2.503836439067691 2.504419042580414
+BODY602_GM 7.205091159985646 7.205961922976411
+BODY603_GM 41.21366740556955 41.21392252150596
+BODY604_GM 73.11206406733254 73.11208204909212
+BODY605_GM 153.9421167266536 153.9421763278791
+BODY606_GM 8978.139180360749 8978.144552352178
+BODY607_GM 0.370390019371346 0.370847384392641
+BODY608_GM 120.5021384592211 120.5078146418220
+BODY609_GM 0.5537054261288668 0.5535279925596653
+
+
+
+
+2007 May 8 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070507R_SCPSE_07077_07094.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070412_042T28
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.08153445 37940585.09724870
+BODY699_GM 37931207.5393 37931207.5551
+BODY699_POLE_RA(1) 40.580887 40.580883
+BODY699_POLE_DEC(1) 83.537760 83.537754
+BODY699_JCOEF(2) 0.016290487158 0.016290487287
+BODY699_JCOEF(4) -0.000936645013 -0.000936319857
+BODY601_GM 2.503862387407351 2.503836439067691
+BODY602_GM 7.204709334179276 7.205091159985646
+BODY603_GM 41.21356636921946 41.21366740556955
+BODY604_GM 73.11207388515732 73.11206406733254
+BODY605_GM 153.9421590940140 153.9421167266536
+BODY606_GM 8978.139228648140 8978.139180360749
+BODY607_GM 0.370175811007482 0.370390019371346
+BODY608_GM 120.5026966204559 120.5021384592211
+BODY609_GM 0.5537453110625723 0.5537054261288668
+
+
+
+
+
+2007 May 1 (published)
+E.Martinez
+
+Applicable current Ephemeris = 070430R_SCPSE_07062_07077.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070328_041T27
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.17276487 37940585.08153445
+BODY699_GM 37931207.6257 37931207.5393
+BODY699_POLE_RA(1) 40.581183 40.580887
+BODY699_POLE_DEC(1) 83.537742 83.537760
+BODY699_JCOEF(2) 0.016290515129 0.016290487158
+BODY699_JCOEF(4) -0.000936635353 -0.000936645013
+BODY601_GM 2.503852026860320 2.503862387407351
+BODY602_GM 7.204735734158900 7.204709334179276
+BODY603_GM 41.21342237725444 41.21356636921946
+BODY604_GM 73.11204651203829 73.11207388515732
+BODY605_GM 153.9422097818796 153.9421590940140
+BODY606_GM 8978.139349010102 8978.139228648140
+BODY607_GM 0.370710830099663 0.370175811007482
+BODY608_GM 120.5069073152362 120.5026966204559
+BODY609_GM 0.5537953815668963 0.5537453110625723
+
+
+
+2007 Apr. 5 (published)
+E.Martinez
+
+Applicable current Ephemeris = 070405R_SCPSE_07042_07062.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070311_040T26
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.33700632 37940585.17276487
+BODY699_GM 37931207.7897 37931207.6257
+BODY699_POLE_RA(1) 40.582138 40.581183
+BODY699_POLE_RA(2) -0.042290 -0.028212
+BODY699_POLE_DEC(1) 83.537654 83.537742
+BODY699_POLE_DEC(2) -0.004440 -0.005007
+BODY699_JCOEF(2) 0.016290641945 0.016290515129
+BODY699_JCOEF(4) -0.000935668041 -0.000936635353
+BODY699_JCOEF(6) 0.000086164269 0.000085603492
+BODY601_GM 2.503876883191547 2.503852026860320
+BODY602_GM 7.204408649790674 7.204735734158900
+BODY603_GM 41.21355379903252 41.21342237725444
+BODY604_GM 73.11217921621768 73.11204651203829
+BODY605_GM 153.9423800317704 153.9422097818796
+BODY606_GM 8978.136240566020 8978.139349010102
+BODY607_GM 0.371098539685749 0.370710830099663
+BODY608_GM 120.5099185698973 120.5069073152362
+BODY609_GM 0.5536470952086257 0.5537953815668963
+
+
+
+2007 Mar. 12 (published)
+A. Tinio
+
+Applicable current Ephemeris = 070312R_SCPSE_07023_07042.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070227_039T25
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.33807337 37940585.33700632
+BODY699_GM 37931207.7915 37931207.7897
+BODY699_POLE_RA(1) 40.582215 40.582138
+BODY699_POLE_DEC(1) 83.537654 83.537655
+BODY699_JCOEF(2) 0.016290659210 0.016290641945
+BODY699_JCOEF(4) -0.000935527451 -0.000935668041
+BODY601_GM 2.503837919690110 2.503876883191547
+BODY602_GM 7.204366436582808 7.204408649790674
+BODY603_GM 41.21350165765106 41.21355379903252
+BODY604_GM 73.11214683578255 73.11217921621768
+BODY605_GM 153.9423654046796 153.9423800317704
+BODY606_GM 8978.136205102190 8978.136240566020
+BODY607_GM 0.371098868424698 0.371098539685749
+BODY608_GM 120.5093717224557 120.5099185698973
+BODY609_GM 0.5536729212172495 0.5536470952086257
+
+
+2007 Feb. 14 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070213R_SCPSE_07008_07023.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 070131_038T24
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.37672914 37940585.33807337
+BODY699_GM 37931207.8307 37931207.7915
+BODY699_POLE_RA(1) 40.582442 40.582215
+BODY699_POLE_DEC(1) 83.537638 83.537654
+BODY699_JCOEF(2) 0.016290689119 0.016290659210
+BODY699_JCOEF(4) -0.000935639203 -0.000935527451
+BODY601_GM 2.503846655611214 2.503837919690110
+BODY602_GM 7.204437093644860 7.204366436582808
+BODY603_GM 41.21355196667208 41.21350165765106
+BODY604_GM 73.11210070783861 73.11214683578255
+BODY605_GM 153.9424390527431 153.9423654046796
+BODY606_GM 8978.134670303732 8978.136205102190
+BODY607_GM 0.372265820288520 0.371098868424698
+BODY608_GM 120.5089822796373 120.5093717224557
+BODY609_GM 0.5537139855259471 0.5536729212172495
+
+
+
+2007 Feb. 10 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070209AP_SK_06356_08222.BSP
+Restrictions/Limitations = Use for planning for span of file.
+Reference/Source of new values = 061122_034Sa
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.43553244 37940585.37672914
+BODY699_GM 37931207.8926 37931207.8307
+BODY699_POLE_RA(1) 40.582332 40.582442
+BODY699_POLE_DEC(1) 83.537646 83.537638
+BODY699_JCOEF(2) 0.016290673275 0.016290689119
+BODY699_JCOEF(4) -0.000935553602 -0.000935639203
+BODY601_GM 2.503839997455295 2.503846655611214
+BODY602_GM 7.204479017295238 7.204437093644860
+BODY603_GM 41.21348039992097 41.21355196667208
+BODY604_GM 73.11210988012873 73.11210070783861
+BODY605_GM 153.9424056799695 153.9424390527431
+BODY606_GM 8978.134379445051 8978.134670303732
+BODY606_JCOEF(2) 0.00003174 0.00003300
+BODY606_CCOEF(3) 0.0000092806 0.0000111800
+BODY606_SCOEF(3) 0.0000000000 -0.0000003700
+BODY607_GM 0.370859756936743 0.372265820288520
+BODY608_GM 120.5077275524120 120.5089822796373
+BODY609_GM 0.5536709288276324 0.5537139855259471
+
+
+
+2007 Jan. 26 (published)2007 Jan. 26 (published)
+E. Martinez
+
+Applicable current Ephemeris = 070125R_SCPSE_06342_06356.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061231a_036T22
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.47883564 37940585.43553244
+BODY699_GM 37931207.9327 37931207.8926
+BODY699_POLE_RA(1) 40.582379 40.582332
+BODY699_POLE_DEC(1) 83.537643 83.537646
+BODY699_JCOEF(2) 0.016290679648 0.016290673275
+BODY699_JCOEF(4) -0.000935644640 -0.000935553602
+BODY601_GM 2.503831680306900 2.503839997455295
+BODY602_GM 7.204371760563005 7.204479017295238
+BODY603_GM 41.21355129362405 41.21348039992097
+BODY604_GM 73.11211256265864 73.11210988012873
+BODY605_GM 153.9423945784529 153.9424056799695
+BODY606_GM 8978.134682483926 8978.134379445051
+BODY606_JCOEF(2) 0.00003300 0.00003174
+BODY606_CCOEF(3) 0.0000111800 0.0000092806
+BODY606_SCOEF(3) -0.0000003700 0.0000000000
+BODY607_GM 0.371995143043160 0.370859756936743
+BODY608_GM 120.5094986156859 120.5077275524120
+BODY609_GM 0.5537065233590567 0.5536709288276324
+
+
+
+2007 Jan. 17 ( published )
+E. Martinez
+
+Applicable current Ephemeris = 070117R_SCPSE_06332_06342.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061214_035T21
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.40103932 37940585.47883564
+BODY699_GM 37931207.8546 37931207.9327
+BODY699_POLE_RA(1) 40.582415 40.582379
+BODY699_POLE_DEC(1) 83.537640 83.537643
+BODY699_JCOEF(2) 0.016290697390 0.016290679648
+BODY699_JCOEF(4) -0.000935496137 -0.000935644640
+BODY601_GM 2.503829742547669 2.503831680306900
+BODY602_GM 7.204465583009808 7.204371760563005
+BODY603_GM 41.21349540009213 41.21355129362405
+BODY604_GM 73.11214005633310 73.11211256265864
+BODY605_GM 153.9423658347898 153.9423945784529
+BODY606_GM 8978.134661912558 8978.134682483926
+BODY607_GM 0.372269207385233 0.371995143043160
+BODY608_GM 120.5094670844839 120.5094986156859
+BODY609_GM 0.5537061797030824 0.5537065233590567
+
+
+2007 Jan. 10 ( published )
+E. Martinez
+
+Applicable current Ephemeris = 070109R_SCPSE_06318_06332.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061211_034Sa
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.32441469 37940585.40103932
+BODY699_GM 37931207.7782 37931207.8546
+BODY699_POLE_RA(1) 40.582617 40.582415
+BODY699_POLE_DEC(1) 83.537610 83.537640
+BODY699_JCOEF(2) 0.016290678494 0.016290697390
+BODY699_JCOEF(4) -0.000935768820 -0.000935496137
+BODY601_GM 2.503836592945681 2.503829742547669
+BODY602_GM 7.204644742649264 7.204465583009808
+BODY603_GM 41.21354261332835 41.21349540009213
+BODY604_GM 73.11209408451387 73.11214005633310
+BODY605_GM 153.9424492343117 153.9423658347898
+BODY606_GM 8978.134681720063 8978.134661912558
+BODY607_GM 0.372280925349763 0.372269207385233
+BODY608_GM 120.5090050942508 120.5094670844839
+BODY609_GM 0.5537188622437070 0.5537061797030824
+
+
+2006 Dec. 14 ( published )
+E. Martinez
+
+Applicable current Ephemeris = 061213R_SCPSE_06308_06318.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061127a_033Sa
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.29559930 37940585.32441469
+BODY699_GM 37931207.7534 37931207.7782
+BODY699_POLE_RA(1) 40.582407 40.582617
+BODY699_POLE_DEC(1) 83.537630 83.537610
+BODY699_JCOEF(2) 0.016290705447 0.016290678494
+BODY699_JCOEF(4) -0.000935475070 -0.000935768820
+BODY601_GM 2.503858603857476 2.503836592945681
+BODY602_GM 7.204382802668946 7.204644742649264
+BODY603_GM 41.21362206412197 41.21354261332835
+BODY604_GM 73.11209645069110 73.11209408451387
+BODY605_GM 153.9424779310557 153.9424492343117
+BODY606_GM 8978.134414593294 8978.134681720063
+BODY607_GM 0.371810775100716 0.372280925349763
+BODY608_GM 120.5058167650734 120.5090050942508
+BODY609_GM 0.5537093920200542 0.5537188622437070
+
+
+
+2006 Dec. 01 ( published )
+E. Martinez
+
+Applicable current Ephemeris = 061129R_SCPSE_06292_06307.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061114_032Sa
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.24138311 37940585.29559930
+BODY699_GM 37931207.6992 37931207.7534
+BODY699_POLE_RA(1) 40.582380 40.582407
+BODY699_POLE_DEC(1) 83.537628 83.537630
+BODY699_JCOEF(2) 0.016290694538 0.016290705447
+BODY699_JCOEF(4) -0.000935172730 -0.000935475070
+BODY699_JCOEF(6) 0.000086032043 0.000086164269
+BODY601_GM 2.504045173937001 2.503858603857476
+BODY602_GM 7.204489862685024 7.204382802668946
+BODY603_GM 41.21355396165882 41.21362206412197
+BODY604_GM 73.11209017356970 73.11209645069110
+BODY605_GM 153.9424477351946 153.9424779310557
+BODY606_GM 8978.134479689157 8978.134414593294
+BODY607_GM 0.372161757032882 0.371810775100716
+BODY608_GM 120.5055622185648 120.5058167650734
+BODY609_GM 0.5533481483735110 0.5537093920200542
+
+
+
+2006 Nov. 16 ( published )
+E. Martinez
+
+Applicable current Ephemeris = 061116R_SCPSE_06276_06292.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061029_031T20
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.28556997 37940585.24138311
+BODY699_GM 37931207.7383 37931207.6992
+BODY699_POLE_RA(1) 40.582563 40.582380
+BODY699_POLE_DEC(1) 83.537609 83.537628
+BODY699_JCOEF(2) 0.016290723281 0.016290694538
+BODY699_JCOEF(4) -0.000934943222 -0.000935172730
+BODY601_GM 2.504039758351044 2.504045173937001
+BODY602_GM 7.204635369705422 7.204489862685024
+BODY603_GM 41.21351788474261 41.21355396165882
+BODY604_GM 73.11206102463274 73.11209017356970
+BODY605_GM 153.9424093566678 153.9424477351946
+BODY606_GM 8978.134640768996 8978.134479689157
+BODY607_GM 0.372257378997563 0.372161757032882
+BODY608_GM 120.5103787968222 120.5055622185648
+BODY609_GM 0.5533513566819516 0.5533481483735110
+
+
+2006 Nov. 08 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 061108R_SCPSE_06260_06276.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 061013_030T19
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.20804367 37940585.28556997
+BODY699_GM 37931207.6506 37931207.7383
+BODY699_POLE_RA(1) 40.582917 40.582563
+BODY699_POLE_DEC(1) 83.537562 83.537609
+BODY699_JCOEF(2) 0.016290681360 0.016290723281
+BODY699_JCOEF(4) -0.000935220317 -0.000934943222
+BODY601_GM 2.504056364254555 2.504039758351044
+BODY602_GM 7.205444446422798 7.204635369705422
+BODY603_GM 41.21340329716050 41.21351788474261
+BODY604_GM 73.11208185666693 73.11206102463274
+BODY605_GM 153.9423994589908 153.9424093566678
+BODY606_GM 8978.134885749399 8978.134640768996
+BODY607_GM 0.372103146260205 0.372257378997563
+BODY608_GM 120.5197010249014 120.5103787968222
+BODY609_GM 0.5533956626324310 0.5533513566819516
+
+2006 Oct. 16 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 061013R_SCPSE_06240_06260.BSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060926_029T18
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.30041119 37940585.20804367
+BODY699_GM 37931207.7563 37931207.6506
+BODY699_POLE_RA(1) 40.582624 40.582917
+BODY699_POLE_DEC(1) 83.537604 83.537562
+BODY699_JCOEF(2) 0.016290700509 0.016290681360
+BODY699_JCOEF(4) -0.000935268588 -0.000935220317
+BODY699_JCOEF(6) 0.000086306565 0.000086032043
+BODY601_GM 2.503234184380379 2.504056364254555
+BODY602_GM 7.205788388974169 7.205444446422798
+BODY603_GM 41.20921386093631 41.21340329716050
+BODY604_GM 73.11256958878700 73.11208185666693
+BODY605_GM 153.9427794181101 153.9423994589908
+BODY606_GM 8978.134842412568 8978.134885749399
+BODY607_GM 0.371655593766023 0.372103146260205
+BODY608_GM 120.5107561184160 120.5197010249014
+BODY609_GM 0.5533087871633449 0.5533956626324310
+
+2006 Sep. 26 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060925R_SCPSE_06217_06240.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060910_028T17
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.37202547 37940585.30041119
+BODY699_GM 37931207.8298 37931207.7563
+BODY699_POLE_RA(1) 40.582733 40.582624
+BODY699_POLE_DEC(1) 83.537616 83.537604
+BODY699_JCOEF(2) 0.016290681525 0.016290700509
+BODY699_JCOEF(4) -0.000935830959 -0.000935268588
+BODY601_GM 2.503237817457834 2.503234184380379
+BODY602_GM 7.205571530617301 7.205788388974169
+BODY603_GM 41.20912316700146 41.20921386093631
+BODY604_GM 73.11254700746446 73.11256958878700
+BODY605_GM 153.9427536730286 153.9427794181101
+BODY606_GM 8978.134866382321 8978.134842412568
+BODY607_GM 0.372358845972800 0.371655593766023
+BODY608_GM 120.5084733163531 120.5107561184160
+BODY609_GM 0.5532645857684702 0.5533087871633449
+
+2006 Sep. 07 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060907R_SCPSE_06193_06228.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060815_027Sa
+
+Parameter Superceded Value New Value
+
+BODY10_GM 132712440017.9870 132712440044.2083
+BODY2_GM 324858.598826460 324858.598890645
+BODY3_GM 403503.233479087 403503.2335605171
+BODY399_GM 398600.4328969392 398600.4334392727
+BODY5_GM 126712767.8577960 126712764.8582231
+BODY599_GM 126686536.9610660 126686533.9614931
+BODY6_GM 37940585.21804788 37940585.37202547
+BODY699_GM 37931207.6691 37931207.8298
+BODY699_POLE_RA(1) 40.582843 40.582733
+BODY699_POLE_DEC(1) 83.537599 83.537616
+BODY699_JCOEF(2) 0.016290708626 0.016290681525
+BODY699_JCOEF(4) -0.000935838573 -0.000935830959
+BODY699_JCOEF(6) 0.000086144219 0.000086306565
+BODY7_GM 5794549.007071874 5794549.008216757
+BODY301_GM 4902.800582147764 4902.800121244415
+BODY601_GM 2.502372648309949 2.503237817457834
+BODY602_GM 7.209633248592259 7.205571530617301
+BODY603_GM 41.20971288406673 41.20912316700146
+BODY604_GM 73.11266255598086 73.11254700746446
+BODY605_GM 153.9415996603182 153.9427536730286
+BODY606_GM 8978.135697583817 8978.134866382321
+BODY607_GM 0.371269445627224 0.372358845972800
+BODY608_GM 120.5126041600149 120.5084733163531
+BODY609_GM 0.5534414535788157 0.5532645857684702
+
+
+
+2006 AUG 11 ( published )
+E. Martinez, A. Tinio
+
+Applicable current Ephemeris = 060810R_SCPSE_06162_06193.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060723_026T16
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.19817787 37940585.21804788
+BODY699_GM 37931207.6481 37931207.6691
+BODY699_POLE_RA(1) 40.582804 40.582843
+BODY699_POLE_DEC(1) 83.537620 83.537599
+BODY699_JCOEF(2) 0.016290723295 0.016290708626
+BODY699_JCOEF(4) -0.000935636528 -0.000935838573
+BODY601_GM 2.502337374431450 2.502372648309949
+BODY602_GM 7.209594537754957 7.209633248592259
+BODY603_GM 41.20980224942576 41.20971288406673
+BODY604_GM 73.11265768420897 73.11266255598086
+BODY605_GM 153.9415837936022 153.9415996603182
+BODY606_GM 8978.135361988159 8978.135697583817
+BODY607_GM 0.372568723578752 0.371269445627224
+BODY608_GM 120.5127058469105 120.5126041600149
+BODY609_GM 0.5534333052090450 0.5534414535788157
+
+
+
+2006 July 20 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060719R_SCPSE_06130_06162.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060705a_025T15
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.02377836 37940585.19817787
+BODY699_GM 37931207.4828 37931207.6481
+BODY699_POLE_RA(1) 40.582022 40.582804
+BODY699_POLE_DEC(1) 83.537664 83.537620
+BODY699_JCOEF(2) 0.016290719439 0.016290723295
+BODY699_JCOEF(4) -0.000934406276 -0.000935636528
+BODY699_JCOEF(6) 0.000086620067 0.000086144219
+BODY601_GM 2.503149740351328 2.502337374431450
+BODY602_GM 7.208872923723865 7.209594537754957
+BODY603_GM 41.20029810761654 41.20980224942576
+BODY604_GM 73.11284780426027 73.11265768420897
+BODY605_GM 153.9402009786583 153.9415837936022
+BODY606_GM 8978.137295144839 8978.135361988159
+BODY607_GM 0.372172625164198 0.372568723578752
+BODY608_GM 120.5128842735845 120.5127058469105
+BODY609_GM 0.5532749466908186 0.5534333052090450
+
+2006 June 14 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060614R_SCPSE_06099_06130.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060521_024T14
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.00869015 37940585.02377836
+BODY699_GM 37931207.4702 37931207.4828
+BODY699_POLE_RA(1) 40.581940 40.582022
+BODY699_POLE_DEC(1) 83.537665 83.537664
+BODY699_JCOEF(2) 0.016290720625 0.016290719439
+BODY699_JCOEF(4) -0.000934485800 -0.000934406276
+BODY601_GM 2.503155504246730 2.503149740351328
+BODY602_GM 7.208672940445637 7.208872923723865
+BODY603_GM 41.20030999725930 41.20029810761654
+BODY604_GM 73.11284902953261 73.11284780426027
+BODY605_GM 153.9401720253013 153.9402009786583
+BODY606_GM 8978.137600869284 8978.137295144839
+BODY607_GM 0.372187991611717 0.372172625164198
+BODY608_GM 120.5102865422368 120.5128842735845
+BODY609_GM 0.5532644770436360 0.5532749466908186
+
+
+
+2006 MAY 15 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060515R_SCPSE_06068_06099.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060503_023T13
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.82178953 37940585.00869015
+BODY699_GM 37931207.2824 37931207.4702
+BODY699_POLE_RA(1) 40.580240 40.581940
+BODY699_POLE_DEC(1) 83.537779 83.537665
+BODY699_JCOEF(2) 0.016290675629 0.016290720625
+BODY699_JCOEF(4) -0.000935190949 -0.000934485800
+BODY699_JCOEF(6) 0.000086898078 0.000086620067
+BODY601_GM 2.503244068708538 2.503155504246730
+BODY602_GM 7.208175153748505 7.208672940445637
+BODY603_GM 41.20088341434613 41.20030999725930
+BODY604_GM 73.11295205736538 73.11284902953261
+BODY605_GM 153.9401465123193 153.9401720253013
+BODY606_GM 8978.135422689342 8978.137600869284
+BODY606_JCOEF(2) 0.00003301 0.00003300
+BODY606_CCOEF(3) 0.0000111790 0.0000111800
+BODY606_SCOEF(3) -0.0000003683 -0.0000003700
+BODY607_GM 0.372225170143269 0.372187991611717
+BODY608_GM 120.5131683419617 120.5102865422368
+BODY609_GM 0.5532134715796430 0.5532644770436360
+
+2006 Apr 18 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060417R_SCPSE_06036_06068.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060320_022T12
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.02189582 37940584.82178953
+BODY699_GM 37931207.4768 37931207.2824
+BODY699_POLE_RA(1) 40.582939 40.580240
+BODY699_POLE_DEC(1) 83.537574 83.537779
+BODY699_JCOEF(2) 0.016290752164 0.016290675629
+BODY699_JCOEF(4) -0.000935531632 -0.000935190949
+BODY699_JCOEF(6) 0.000086130696 0.000086898078
+BODY601_GM 2.503196140438530 2.503244068708538
+BODY602_GM 7.209302177761134 7.208175153748505
+BODY603_GM 41.19976930418225 41.20088341434613
+BODY604_GM 73.11284795021615 73.11295205736538
+BODY605_GM 153.9400292807456 153.9401465123193
+BODY606_GM 8978.135208156255 8978.135422689342
+BODY606_JCOEF(2) 0.00003349 0.00003301
+BODY606_CCOEF(3) 0.0000110747 0.0000111790
+BODY606_SCOEF(3) -0.0000003502 -0.0000003683
+BODY607_GM 0.373150368272270 0.372225170143269
+BODY608_GM 120.5182054679503 120.5131683419617
+BODY609_GM 0.5533715466786809 0.5532134715796430
+
+2006 Mar 21 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060321_SCPSE_06005_06036.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060301_021T11
+
+Parameter Superceded Value New Value
+BODY6_GM 37940584.95359504 37940585.02189582
+BODY699_GM 37931207.4118 37931207.4768
+BODY699_POLE_RA(1) 40.582515 40.582939
+BODY699_POLE_DEC(1) 83.537604 83.537574
+BODY699_JCOEF(2) 0.016290685585 0.016290752164
+BODY699_JCOEF(4) -0.000935841110 -0.000935531632
+BODY601_GM 2.503209168287056 2.503196140438530
+BODY602_GM 7.208811870736135 7.209302177761134
+BODY603_GM 41.19992642786966 41.19976930418225
+BODY604_GM 73.11284728090631 73.11284795021615
+BODY605_GM 153.9399206434808 153.9400292807456
+BODY606_GM 8978.134804759919 8978.135208156255
+BODY606_JCOEF(2) 0.00003320 0.00003349
+BODY606_CCOEF(3) 0.0000111862 0.0000110747
+BODY606_SCOEF(3) -0.0000003715220 -0.0000003502
+BODY607_GM 0.372786047857714 0.373150368272270
+BODY608_GM 120.5161788220962 120.5182054679503
+BODY609_GM 0.5533583156478464 0.5533715466786809
+
+
+2006 Mar 15 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060323AP_SK_06082_08222.XSP
+Restrictions/Limitations = Use for Ref. Traj. planning for period of file
+Reference/Source of new values = 060301_022T12
+
+
+
+Parameter Superceded Value New Value
+
+
+BODY6_GM 37940584.97838498 37940584.95359504
+BODY699_GM 37931207.4218 37931207.4118
+BODY699_POLE_RA(1) 40.582375 40.582515
+BODY699_POLE_DEC(1) 83.537622 83.537604
+BODY699_JCOEF(2) 0.016290660391 0.016290685585
+BODY699_JCOEF(4) -0.000935797472 -0.000935841110
+BODY601_GM 2.503255490608568 2.503209168287056
+BODY602_GM 7.208151961640861 7.208811870736135
+BODY603_GM 41.19986045608409 41.19992642786966
+BODY604_GM 73.11282801626780 73.11284728090631
+BODY605_GM 153.9400039367874 153.9399206434808
+BODY606_GM 8978.145353251261 8978.134804759919
+BODY606_JCOEF(2) 0.00002640 0.00003320
+BODY606_CCOEF(3) 0.0000079 0.0000111862
+BODY606_SCOEF(3) -0.0000003715220 *
+BODY607_GM 0.372587254705434 0.372786047857714
+BODY608_GM 120.5211143157129 120.5161788220962
+BODY609_GM 0.5533806776787945 0.5533583156478464
+
+
+* Note: Titan tesseral harmonic, BODY606_SCOEF(3), is included with this
+ delivery:
+ BODY606_SCOEF = ( 0.0, 0.0, -0.0000003715220 )
+
+
+2006 Feb 14 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060213R_SCPSE_05348_06005.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 060121_020T10
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.15649380 37940584.97838498
+BODY699_GM 37931207.5978 37931207.4218
+BODY699_POLE_RA(1) 40.582823 40.582375
+BODY699_POLE_DEC(1) 83.537575 83.537622
+BODY699_JCOEF(2) 0.016290651631 0.016290660391
+BODY699_JCOEF(4) -0.000935923828 -0.000935797472
+BODY699_JCOEF(6) 0.000086273874 0.000086130696
+BODY601_GM 2.503473438509435 2.503255490608568
+BODY602_GM 7.208482454021635 7.208151961640861
+BODY603_GM 41.20142512691800 41.19986045608409
+BODY604_GM 73.11291388000183 73.11282801626780
+BODY605_GM 153.9397981709559 153.9400039367874
+BODY606_GM 8978.155502709762 8978.145353251261
+BODY607_GM 0.372499954808899 0.372587254705434
+BODY608_GM 120.5112356389298 120.5211143157129
+BODY609_GM 0.5533569886802691 0.5533806776787945
+
+Additionally, as provided in "Cassini Planetary Constants Usage Policy,
+Contents, and Update Process" (Rev. E, 16-Apr-2003) and OIA IO-043, the
+Cassini Navigation Team will be estimating some satellite values for
+J2 and C22. The keywords for these coefficients will be of the forms:
+ BODY<nnn>_JCOEF where <nnn> would be 601, 602, etc.
+ BODY<nnn>_CCOEF
+and the pck values would be:
+ ( 0.0, <J2> ) for J2 gravitational coefficients
+and ( 0.0, 0.0, <C22> ) for C22 gravitational coefficients
+
+These current unnormalized values are available with this reconstruction:
+
+BODY602_JCOEF = ( 0.0, 0.00897 )
+BODY602_CCOEF = ( 0.0, 0.0, 0.00208 )
+
+BODY604_JCOEF = ( 0.0, 0.0012 )
+BODY604_CCOEF = ( 0.0, 0.0, 0.000361 )
+
+BODY605_JCOEF = ( 0.0, 0.000941 )
+BODY605_CCOEF = ( 0.0, 0.0, 0.000232 )
+
+BODY606_JCOEF = ( 0.0, 0.0000264 )
+BODY606_CCOEF = ( 0.0, 0.0, 0.0000079 )
+
+
+2006 Jan 12 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 060111R_SCPSE_05320_05348.BSP
+Restrictions/Limitations = Use for period of file.
+Reference/Source of new values = 051230_019T9
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.17590274 37940585.15649380
+BODY699_GM 37931207.6326 37931207.5978
+BODY699_POLE_RA(1) 40.583157 40.582823
+BODY699_POLE_DEC(1) 83.537570 83.537575
+BODY699_JCOEF(2) 0.016290685708 0.016290651631
+BODY699_JCOEF(4) -0.000935953100 -0.000935923828
+BODY601_GM 2.503462470043706 2.503473438509435
+BODY602_GM 7.208374326151627 7.208482454021635
+BODY603_GM 41.20155898244365 41.20142512691800
+BODY604_GM 73.11290821305468 73.11291388000183
+BODY605_GM 153.9375651420232 153.9397981709559
+BODY606_GM 8978.161222465345 8978.155502709762
+BODY607_GM 0.372677926980588 0.372499954808899
+BODY608_GM 120.4921877511916 120.5112356389298
+BODY609_GM 0.5533233423151438 0.5533569886802691
+
+
+2005 Dec 13 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 051213R_SCPSE_05293_05320.XSP
+Restrictions/Limitations = Use for the period of this file
+Reference/Source of new values = 051128_018R1
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.24828158 37940585.17590274
+BODY699_GM 37931207.6394 37931207.6326
+BODY699_POLE_RA(1) 40.583441 40.583157
+BODY699_POLE_DEC(1) 83.537544 83.537570
+BODY699_JCOEF(2) 0.016290736784 0.016290685708
+BODY699_JCOEF(4) -0.000935509628 -0.000935953100
+BODY601_GM 2.503432899195495 2.503462470043706
+BODY602_GM 7.208135453630815 7.208374326151627
+BODY603_GM 41.20196588064624 41.20155898244365
+BODY604_GM 73.11281403854379 73.11290821305468
+BODY605_GM 153.9961391059971 153.9375651420232
+BODY606_GM 8978.161488269006 8978.161222465345
+BODY607_GM 0.372813948978216 0.372677926980588
+BODY608_GM 120.4987924024436 120.4921877511916
+BODY609_GM 0.5533036326727672 0.5533233423151438
+
+
+2005 Nov 15 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 051114R_SCPSE_05275_05293.XSP
+Restrictions/Limitations = Use for tour analysis for period of file.
+Reference/Source of new values = 051031_017T8
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.30229028 37940585.24828158
+BODY699_GM 37931207.6574 37931207.6394
+BODY699_POLE_RA(1) 40.581524 40.583441
+BODY699_POLE_DEC(1) 83.537351 83.537544
+BODY699_JCOEF(2) 0.016290658643 0.016290736784
+BODY699_JCOEF(4) -0.000935977180 -0.000935509628
+BODY699_JCOEF(6) 0.000085916004 0.000086273874
+BODY601_GM 2.521377772727696 2.503432899195495
+BODY602_GM 7.203310617192614 7.208135453630815
+BODY603_GM 41.20404503620523 41.20196588064624
+BODY604_GM 73.11270278320977 73.11281403854379
+BODY605_GM 154.0177629113878 153.9961391059971
+BODY606_GM 8978.157972403947 8978.161488269006
+BODY607_GM 0.371499507966020 0.372813948978216
+BODY608_GM 120.5028956594414 120.4987924024436
+BODY609_GM 0.5532983200668332 0.5533036326727672
+
+2005 Oct 21 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 051021R_SCPSE_05257_05275.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 051012_016D1
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.34349760 37940585.30229028
+BODY699_GM 37931207.6943 37931207.6574
+BODY699_POLE_RA(1) 40.582979 40.581524
+BODY699_POLE_DEC(1) 83.537892 83.537351
+BODY699_JCOEF(2) 0.016290717890 0.016290658643
+BODY699_JCOEF(4) -0.000935625703 -0.000935977180
+BODY699_JCOEF(6) 0.000086359935 0.000085916004
+BODY601_GM 2.526812031114878 2.521377772727696
+BODY602_GM 7.209128567822218 7.203310617192614
+BODY603_GM 41.20938175350662 41.20404503620523
+BODY604_GM 73.11311455024394 73.11270278320977
+BODY605_GM 153.9760788846642 154.0177629113878
+BODY606_GM 8978.189785708180 8978.157972403947
+BODY607_GM 0.371309980105878 0.371499507966020
+BODY608_GM 120.5004502021633 120.5028956594414
+BODY609_GM 0.5531785509595187 0.5532983200668332
+
+2005 Oct 11 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 051011R_SCPSE_05245_05257.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 050927_015H1
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.31875592 37940585.34349760
+BODY699_GM 37931207.6724 37931207.6943
+BODY699_POLE_RA(1) 40.582875 40.582979
+BODY699_POLE_DEC(1) 83.537914 83.537892
+BODY699_JCOEF(2) 0.016290698730 0.016290717890
+BODY699_JCOEF(4) -0.000935658433 -0.000935625703
+BODY601_GM 2.527676231780819 2.526812031114878
+BODY602_GM 7.208873373966934 7.209128567822218
+BODY603_GM 41.20956001485827 41.20938175350662
+BODY604_GM 73.11311058244327 73.11311455024394
+BODY605_GM 153.9761508783966 153.9760788846642
+BODY606_GM 8978.186036934201 8978.189785708180
+BODY607_GM 0.372357313080731 0.371309980105878
+BODY608_GM 120.4994492669644 120.5004502021633
+BODY609_GM 0.5531399174985459 0.5531785509595187
+
+
+2005 Sep 23 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 050922R_SCPSE_05225_05245.XSP
+Restrictions/Limitations = Use for analysis for period of file.
+Reference/Source of new values = 050911_014T7
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.41646386 37940585.31875592
+BODY699_GM 37931207.7502 37931207.6724
+BODY699_POLE_RA(1) 40.583323 40.582875
+BODY699_POLE_DEC(1) 83.537945 83.537914
+BODY699_JCOEF(2) 0.016290703868 0.016290698730
+BODY699_JCOEF(4) -0.000935636535 -0.000935658433
+BODY601_GM 2.527433358438375 2.527676231780819
+BODY602_GM 7.209550965627096 7.208873373966934
+BODY603_GM 41.20955753634430 41.20956001485827
+BODY604_GM 73.11310547668840 73.11311058244327
+BODY605_GM 153.9913950111069 153.9761508783966
+BODY606_GM 8978.185336761786 8978.186036934201
+BODY607_GM 0.375014936981534 0.372357313080731
+BODY608_GM 120.5017530353315 120.4994492669644
+BODY609_GM 0.5530820911204722 0.5531399174985459
+
+
+
+2005 Sep 08 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 050907R_SCPSE_05205_05225.XSP
+Restrictions/Limitations = Use for period of this file.
+Reference/Source of new values = 050824_013T6
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.61194924 37940585.41646386
+BODY699_GM 37931207.9363 37931207.7502
+BODY699_POLE_RA(1) 40.583019 40.583323
+BODY699_POLE_DEC(1) 83.537961 83.537945
+BODY699_JCOEF(2) 0.016290685394 0.016290703868
+BODY699_JCOEF(4) -0.000935967005 -0.000935636535
+BODY601_GM 2.529211216189956 2.527433358438375
+BODY602_GM 7.212376404520326 7.209550965627096
+BODY603_GM 41.20963906707048 41.20955753634430
+BODY604_GM 73.11308526750042 73.11310547668840
+BODY605_GM 153.9923043182035 153.9913950111069
+BODY606_GM 8978.187230684733 8978.185336761786
+BODY607_GM 0.374716668929412 0.375014936981534
+BODY608_GM 120.5039579116963 120.5017530353315
+BODY609_GM 0.5530851646858529 0.5530820911204722
+
+
+
+2005 Aug 26 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 050825R_SCPSE_05186_05205.XSP
+Restrictions/Limitations = Use for data analysis for period of file.
+Reference/Source of new values = 050802_012Sa
+
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940585.41331755 37940585.61194924
+BODY699_GM 37931207.8002 37931207.9363
+BODY699_POLE_RA(1) 40.584385 40.583019
+BODY699_POLE_DEC(1) 83.537627 83.537961
+BODY699_JCOEF(2) 0.016290804116 0.016290685394
+BODY699_JCOEF(4) -0.000933504702 -0.000935967005
+BODY699_JCOEF(6) 0.000092477088 0.000086359935
+BODY601_GM 2.526772990931723 2.529211216189956
+BODY602_GM 7.208888578402212 7.212376404520326
+BODY603_GM 41.20493245127680 41.20963906707048
+BODY604_GM 73.11277252343461 73.11308526750042
+BODY605_GM 153.9672076132773 153.9923043182035
+BODY606_GM 8978.166527318963 8978.187230684733
+BODY607_GM 0.378337733413031 0.374716668929412
+BODY608_GM 120.4944120884058 120.5039579116963
+BODY609_GM 0.5532264432054191 0.5530851646858529
+
+
+2005 Aug 02 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 050802R_SCPSE_05169_05186.XSP
+Restrictions/Limitations = Use for period of file.
+Reference/Source of new values = 050718_011E2
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940584.32393724 37940585.41331755
+BODY699_GM 37931206.6260 37931207.8002
+BODY699_POLE_RA(1) 40.582524 40.584385
+BODY699_POLE_DEC(1) 83.537645 83.537627
+BODY699_JCOEF(2) 0.016290795528 0.016290804116
+BODY699_JCOEF(4) -0.000932738706 -0.000933504702
+BODY601_GM 2.530120927277264 2.526772990931723
+BODY602_GM 7.210665451438561 7.208888578402212
+BODY603_GM 41.20659404333172 41.20493245127680
+BODY604_GM 73.11260446242133 73.11277252343461
+BODY605_GM 154.0186476847478 153.9672076132773
+BODY606_GM 8978.179855914042 8978.166527318963
+BODY607_GM 0.378215663233720 0.378337733413031
+BODY608_GM 120.5079215829297 120.4944120884058
+BODY609_GM 0.5532635543008535 0.5532264432054191
+
+
+2005 Jul 11 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 050708R_SCPSE_05150_05169.XSP
+Restrictions/Limitations = Use for period of file.
+Reference/Source of new values = 050707_010Sa
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940571.43290575 37940584.32393724
+BODY699_GM 37931193.7263 37931206.6260
+BODY699_POLE_RA(1) 40.58051 40.582524
+BODY699_POLE_DEC(1) 83.537912 83.537645
+BODY699_JCOEF(2) 0.016290989185 0.016290795528
+BODY699_JCOEF(4) -0.000931564786 -0.000932738706
+BODY601_GM 2.538987472063466 2.530120927277264
+BODY602_GM 7.209467692177664 7.210665451438561
+BODY603_GM 41.20833951087783 41.20659404333172
+BODY604_GM 73.11259945289306 73.11260446242133
+BODY605_GM 154.0294413273712 154.0186476847478
+BODY606_GM 8978.160024110673 8978.179855914042
+BODY607_GM 0.379051300989386 0.378215663233720
+BODY608_GM 120.5154106017876 120.5079215829297
+BODY609_GM 0.5532537713007321 0.5532635543008535
+
+2005 Jul 05 ( published )
+A. Tinio
+
+Applicable current Ephemeris = 050623R_SCPSE_05132_05150
+
+Restrictions/Limitations = Use for tour analysis for period of file.
+
+Reference/Source of new values = 050613_009Sa
+
+Parameter Superceded Value New Value
+
+
+BODY6_GM 37940570.36454137 37940571.43290575
+BODY699_GM 37931192.6617 37931193.7263
+BODY699_POLE_RA(1) 40.581077 40.580518
+BODY699_POLE_DEC(1) 83.538043 83.537912
+BODY699_JCOEF(2) 0.016290903873 0.016290989185
+BODY699_JCOEF(4) -0.000933053169 -0.000931564786
+BODY601_GM 2.539649757406880 2.538987472063466
+BODY602_GM 7.207150581927309 7.209467692177664
+BODY603_GM 41.20796800520257 41.20833951087783
+BODY604_GM 73.11254942698964 73.11259945289306
+BODY605_GM 154.0258089104270 154.0294413273712
+BODY606_GM 8978.156565061139 8978.160024110673
+BODY607_GM 0.379403816124753 0.379051300989386
+BODY608_GM 120.5204864031117 120.5154106017876
+BODY609_GM 0.5532476180130315 0.5532537713007321
+
+2005 Jun 09 ( published )
+D. Conner
+
+Applicable Ephemeris SPK File:
+ 050606R_SCPSE_05114_05132
+Restrictions/Limitations = Use for timespan of file.
+
+Reference/Source of new values = 050606_008Sa
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940560.63663255 37940570.36454137
+BODY699_GM 37931182.9332 37931192.6617
+BODY699_POLE_RA(1) 40.580644 40.581077
+BODY699_POLE_DEC(1) 83.538056 83.538043
+BODY699_JCOEF(2) 0.016291055854 0.016290903873
+BODY699_JCOEF(4) -0.000931733527 -0.000933053169
+BODY601_GM 2.540653252053214 2.539649757406880
+BODY602_GM 7.205425461485284 7.207150581927309
+BODY603_GM 41.20782889316963 41.20796800520257
+BODY604_GM 73.11252681773537 73.11254942698964
+BODY605_GM 154.0324679857708 154.0258089104270
+BODY606_GM 8978.152308074805 8978.156565061139
+BODY607_GM 0.379158979334525 0.379403816124753
+BODY608_GM 120.5197925170135 120.5204864031117
+BODY609_GM 0.5532510109715066 0.5532476180130315
+
+
+2005 May 19 ( published )
+A. Tinio
+
+Applicable Ephemeris SPK File:
+ 050513R_SCPSE_05097_05114
+Restrictions/Limitations = Use for timespan of file.
+
+Reference/Source of new values = 050513_007Sa
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940486.41643649 37940560.63663255
+BODY699_GM 37931108.7402 37931182.9332
+BODY699_POLE_RA(1) 40.578897 40.580644
+BODY699_POLE_DEC(1) 83.537936 83.538056
+BODY699_JCOEF(2) 0.016291230650 0.016291055854
+BODY699_JCOEF(4) -0.000931186978 -0.000931733527
+BODY699_JCOEF(6) 0.000091862764 0.000092477088
+BODY601_GM 2.541872652365942 2.540653252053214
+BODY602_GM 7.203042868002126 7.205425461485284
+BODY603_GM 41.20826146236565 41.20782889316963
+BODY604_GM 73.11229775557260 73.11252681773537
+BODY605_GM 154.0200209194596 154.0324679857708
+BODY606_GM 8978.142297854909 8978.152308074805
+BODY607_GM 0.374580947348313 0.379158979334525
+BODY608_GM 120.5206235708291 120.5197925170135
+BODY609_GM 0.5532316617014716 0.5532510109715066
+
+
+
+
+2005 May 05 ( published )
+D. Conner
+
+Applicable Ephemeris SPK File:
+ 050506R_SCPSE_05081_05097
+Restrictions/Limitations = Use for period of this file.
+
+Reference/Source of new values = 050502_006T5
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940491.60216828 37940486.41643649
+BODY699_GM 37931113.8322 37931108.7402
+BODY699_POLE_RA(1) 40.577216 40.578897
+BODY699_POLE_DEC(1) 83.537833 83.537936
+BODY699_JCOEF(2) 0.016291419485 0.016291230650
+BODY699_JCOEF(4) -0.000930059692 -0.000931186978
+BODY699_JCOEF(6) 0.000092794848 0.000091862764
+BODY601_GM 2.541204859609778 2.541872652365942
+BODY602_GM 7.208563270001138 7.203042868002126
+BODY603_GM 41.20878136449268 41.20826146236565
+BODY604_GM 73.11206772081295 73.11229775557260
+BODY605_GM 154.1075398995426 154.0200209194596
+BODY606_GM 8978.138361913190 8978.142297854909
+BODY607_GM 0.372850585561523 0.374580947348313
+BODY608_GM 120.5278582301508 120.5206235708291
+BODY609_GM 0.5526937087918932 0.5532316617014716
+
+
+
+2005 Apr 29 ( published )
+D. Conner
+
+Applicable Ephemeris SPK File:
+ 050426AP_SCPSE_05116_05216
+Restrictions/Limitations = Use for period of this file.
+
+Reference/Source of new values = 050425_007Sa
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940502.18556380 37940491.60216828
+BODY699_GM 37931124.7142 37931113.8322
+BODY699_POLE_RA(1) 40.576012 40.577216
+BODY699_POLE_DEC(1) 83.537850 83.537833
+BODY699_JCOEF(2) 0.016291065583 0.016291419485
+BODY699_JCOEF(4) -0.000932322006 -0.000930059692
+BODY699_JCOEF(6) 0.000091137816 0.000092794848
+BODY601_GM 2.540934363643657 2.541204859609778
+BODY602_GM 7.205763658107196 7.208563270001138
+BODY603_GM 41.20992788910005 41.20878136449268
+BODY604_GM 73.11190061154372 73.11206772081295
+BODY605_GM 153.8210020695582 154.1075398995426
+BODY606_GM 8978.126641404288 8978.138361913190
+BODY607_GM 0.379166152072442 0.372850585561523
+BODY608_GM 120.5233558989635 120.5278582301508
+BODY609_GM 0.5526908562645090 0.5526937087918932
+
+
+2005 Apr 21 ( published )
+D. Conner
+
+Applicable Ephemeris SPK File:
+ 050414R_SCPSE_05034_05060 (s/c=-82, planets, satellites)
+
+Restrictions/Limitations = Use for tour analysis for period of this file.
+
+Reference/Source of new values = 050312_004E1
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940496.33673127 37940502.18556380
+BODY699_GM 37931118.8405 37931124.7142
+BODY699_POLE_RA(1) 40.576463 40.576012
+BODY699_POLE_DEC(1) 83.537851 83.537850
+BODY699_JCOEF(2) 0.016290828142 0.016291065583
+BODY699_JCOEF(4) -0.000933491306 -0.000932322006
+BODY699_JCOEF(6) 0.000090898497 0.000091137816
+BODY601_GM 2.541473321497260 2.540934363643657
+BODY602_GM 7.209619039344632 7.205763658107196
+BODY603_GM 41.21072942926893 41.20992788910005
+BODY604_GM 73.11206095252155 73.11190061154372
+BODY605_GM 153.8604802758120 153.8210020695582
+BODY606_GM 8978.112734019802 8978.126641404288
+BODY607_GM 0.379253012301593 0.379166152072442
+BODY608_GM 120.5170740119231 120.5233558989635
+BODY609_GM 0.5528058513249935 0.5526908562645090
+
+
+
+2005 Apr 12 ( published )
+D. Conner
+
+Applicable Ephemeris SPK File:
+ 050411R_SCPSE_05015_05034 (s/c=-82, planets, satellites)
+
+Restrictions/Limitations = Use for Tour analysis for period of SPK file.
+
+Reference/Source of new values = 050218_003T3
+
+5rameter Superceded Value New Value
+
+BODY6_GM 37940515.88181417 37940496.33673127
+BODY699_GM 37931137.6508 37931118.8405
+BODY699_POLE_RA(1) 40.575513 40.576463
+BODY699_POLE_DEC(1) 83.537853 83.537851
+BODY699_JCOEF(2) 0.016290958191 0.016290828142
+BODY699_JCOEF(4) -0.000932286762 -0.000933491306
+BODY601_GM 2.543473865943931 2.541473321497260
+BODY602_GM 7.689375056656368 7.209619039344632
+BODY603_GM 41.21109406519917 41.21072942926893
+BODY604_GM 73.11102520071464 73.11206095252155
+BODY605_GM 154.0395402008101 153.8604802758120
+BODY606_GM 8978.169116863904 8978.112734019802
+BODY607_GM 0.372672948245801 0.379253012301593
+BODY608_GM 120.5420141732170 120.5170740119231
+BODY609_GM 0.5526971060144958 0.5528058513249935
+
+
+
+2005 Mar 01 ( published )
+A. Tinio
+
+Applicable Ephemeris SPK File:
+ 050214R_SCPSE_04336_05015 (s/c=-82, planets, satellites)
+
+Restrictions/Limitations = Use only for timespan of current Ephemeris
+
+Reference/Source of new values = 050214_00cTc
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940575.96714743 37940515.88181417
+BODY699_GM 37931197.4166 37931137.6508
+BODY699_POLE_RA(1) 40.584988 40.575513
+BODY699_POLE_DEC(1) 83.537357 83.537853
+BODY699_JCOEF(2) 0.016291386368 0.016290958191
+BODY699_JCOEF(4) -0.000930863753 -0.000932286762
+BODY699_JCOEF(6) 0.000089007261 0.000090898497
+BODY601_GM 2.543221623761831 2.543473865943931
+BODY602_GM 7.680749472948529 7.689375056656368
+BODY603_GM 41.20953772443173 41.21109406519917
+BODY604_GM 73.11013294006862 73.11102520071464
+BODY605_GM 154.0976429614129 154.0395402008101
+BODY606_GM 8978.252049389006 8978.169116863904
+BODY607_GM 0.379196699024020 0.372672948245801
+BODY608_GM 120.7250175986224 120.5420141732170
+BODY609_GM 0.5529492368788559 0.5526971060144958
+
+
+2005 Feb 28 ( published )
+A. Tinio
+
+Applicable Ephemeris SPK File:
+ 050105R_SCPSE_04247_04336 (s/c=-82, planets, satellites)
+
+Restrictions/Limitations = Use for Tour Analysis for period of SPK file.
+
+Reference/Source of new values = 050105_00bTb
+
+Parameter Superceded Value New Value
+
+BODY2_GM 324858.598826460 324858.598826460
+BODY6_GM 37940594.58466490 37940575.96714743
+BODY699_GM 37931216.9052 37931197.4166
+BODY699_POLE_RA(1) 40.585770 40.584988
+BODY699_POLE_DEC(1) 83.537290 83.537357
+BODY699_JCOEF(2) 0.016290382080 0.016291386368
+BODY699_JCOEF(4) -0.000934342762 -0.000930863753
+BODY601_GM 2.543886999046834 2.543221623761831
+BODY602_GM 7.896235619817622 7.680749472948529
+BODY603_GM 41.21020363352076 41.20953772443173
+BODY604_GM 73.10970856734933 73.11013294006862
+BODY605_GM 153.4403813617471 154.0976429614129
+BODY606_GM 8978.060680624023 8978.252049389006
+BODY607_GM 0.521670363874684 0.379196699024020
+BODY608_GM 120.3437832637150 120.7250175986224
+BODY609_GM* 120.7250175986224 0.5529492368788559
+
+*BODY609_GM value was inadvertently updated with the value for
+ BODY608_GM in the "2005 Jan 10" pck file. This delivery
+ corrects this error. The new value for BODY609_GM is the previous
+ correct value which appears in the "2004 Dec 9" pck file.
+ BODY608_GM is also correctly updated in this delivery.
+
+2005 Jan 10 ( published )
+D. Conner
+
+Applicable Ephemeris SPK File:
+ 050105R_SCPSE_04247_04336 (s/c=-82, planets, satellites)
+
+Restrictions/Limitations = Use for Tour Analysis for period of SPK file.
+
+Reference/Source of new values = 050105_00bTb
+
+Parameter Superceded Value New Value
+
+BODY2_GM 324858.598826460 324858.598826460
+BODY6_GM 37940594.58466490 37940575.96714743
+BODY699_GM 37931216.9052 37931197.4166
+BODY699_POLE_RA(1) 40.585770 40.584988
+BODY699_POLE_DEC(1) 83.537290 83.537357
+BODY699_JCOEF(2) 0.016290382080 0.016291386368
+BODY699_JCOEF(4) -0.000934342762 -0.000930863753
+BODY601_GM 2.543886999046834 2.543221623761831
+BODY602_GM 7.896235619817622 7.680749472948529
+BODY603_GM 41.21020363352076 41.20953772443173
+BODY604_GM 73.10970856734933 73.11013294006862
+BODY605_GM 153.4403813617471 154.0976429614129
+BODY606_GM 8978.060680624023 8978.252049389006
+BODY607_GM 0.521670363874684 0.379196699024020
+BODY608_GM 120.3437832637150 120.7250175986224
+
+
+2004 Dec 9 ( published )
+D. Conner
+
+This file was created from cpck29Sep2004.tpc.
+Removed keywords controlled by PSG, including
+Jupiter satellites, to a separate file
+which is concatenated to this file. Only NAVT affected keywords
+appear above.
+
+Minor satellites and rocks keywords have been moved to the rocks
+PCK in a separate file cpck_rock....
+
+BODY799_GM keyword removed. NAVT only provides a System GM.
+
+Applicable current Ephemeris = 041210AP_SCPSE_04329_08189
+Restrictions/Limitations = None
+Reference/Source of new values = 041207_00cTc (OD Solution)
+
+Parameter Superceded Value New Value
+
+BODY10_GM 132712440035.0199 132712440017.9870
+BODY2_GM 324858.592000000 324858.598826460
+BODY3_GM 403503.241738000 403503.233479087
+BODY399_GM 398600.4415000001 398600.4328969392
+BODY5_GM 126712765.4543717 126712767.8577960
+BODY599_GM 126686534.5576417 126686536.9610660
+BODY6_GM 37940630.56986377 37940594.58466490
+BODY699_GM 37931248.2650 37931216.9052
+BODY699_POLE_RA(1) 40.578921 40.585770
+BODY699_POLE_DEC(1) 83.537507 83.537290
+BODY699_JCOEF(2) 0.016292234642 0.016290382080
+BODY699_JCOEF(4) -0.000927651602 -0.000934342762
+BODY699_JCOEF(6) 0.000096989418 0.000089007261
+BODY7_GM 5794549.007815570 5794549.007071874
+BODY301_GM 4902.800238000001 4902.800582147764
+BODY601_GM 2.520135918453203 2.543886999046834
+BODY602_GM 7.266915346837596 7.896235619817622
+BODY603_GM 41.21004576075436 41.21020363352076
+BODY604_GM 73.11466506841310 73.10970856734933
+BODY605_GM 155.8320579960241 153.4403813617471
+BODY606_GM 8977.930889955829 8978.060680624023
+BODY607_GM 0.720000000000000 0.521670363874684
+BODY608_GM 123.1583788283249 120.3437832637150
+BODY609_GM 0.5517732425959611 0.5529492368788559
+
+
+2004 Sep 29 (published)
+
+Applicable current Ephemeris:
+041001AP_SCPSE_04275_08222.XSP (s/c=-82, planets, satellites)
+
+Restrictions/Limitations = None
+
+Reference/Source of new values = 040927_00aTa (OD solution)
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940690.7690100 37940630.56986377
+BODY699_GM 37931300.4040 37931248.2650
+BODY699_POLE_RA(1) 40.584666 40.578921
+BODY699_POLE_DEC(1) 83.537319 83.537507
+BODY699_JCOEF(2) 0.016293483929 0.016292234642
+BODY699_JCOEF(4) -0.000921635401 -0.000927651602
+BODY699_JCOEF(6) 0.000088726120 0.000096989418
+BODY601_GM 2.521560245529253 2.520135918453203
+BODY602_GM 7.127481554948487 7.266915346837596
+BODY603_GM 41.20541310412448 41.21004576075436
+BODY604_GM 73.11977199413563 73.11466506841310
+BODY605_GM 154.4787324900041 155.8320579960241
+BODY606_GM 8977.981454369899 8977.930889955829
+BODY608_GM 132.6589941798197 123.1583788283249
+BODY609_GM 0.5515856703994798 0.5517732425959611
+
+2004 Jun 21 (published)
+
+Applicable current Ephemeris:
+040622AP_SCPSE_04002_09011.BSP (s/c=-82, planets, satellites)
+040622AP_SK_04122_08222.BSP (spacecraft ephemeris, scid=-82)
+040622AP_PE_04002_09011.BSP (planetary ephemeris)
+040622AP_SE_04002_09011.BSP (satellite ephemeris)
+
+Reference/Source of new values = 040615_00Sa (OD solution)
+
+Parameter Superceded Value New Value
+
+BODY6_GM 37940679.45741954 37940690.76901004
+BODY699_GM 37931289.4836 37931300.4040
+BODY699_POLE_RA(1) 40.586420 40.584666
+BODY699_POLE_DEC(1) 83.537291 83.537319
+BODY699_JCOEF(2) 0.016292243237 0.016293483929
+BODY699_JCOEF(4) -0.000928716077 -0.000921635401
+BODY699_JCOEF(6) 0.000088845313 0.000088726120
+BODY601_GM 2.539908238874431 2.521560245529253
+BODY602_GM 6.980134096218938 7.127481554948487
+BODY603_GM 41.21066708236702 41.20541310412448
+BODY604_GM 73.12382308588424 73.11977199413563
+BODY605_GM 154.6927779454911 154.4787324900041
+BODY606_GM 8978.009444641593 8977.981454369899
+BODY608_GM 132.2117925658847 132.6589941798197
+BODY609_GM 0.4852416379406062 0.5515856703994798 *
+
+* Reference for new Phoebe GM: IOM 312.0-024-04 "Navigation Results
+from the Phoebe flyby", J.B. Jones, 16 June 2004.
+
+
+2004 May 05 (published)
+
+BODY299_GM was set equal to the BODY2_GM.
+BODY799_GM was calculated based on the new BODY7_GM.
+
+Applicable Ephemeris Files:
+ 040506AP_SCPSE_04122_08222.XSP (s/c=-82, planets, satellites)
+ 040506AP_SK_04122_08222.XSP (spacecraft ephemeris, scid=-82)
+ 040506AP_OPK_04122_08222.XSP (s/c & probe, scids=-82,-150)
+ 040506AP_PE_94328_16357.XSP (planetary ephemeris)
+ 040506AP_SE_04002_09011.XSP (satellite ephemeris)
+
+Reference/Source of new values is NAV OD Solution: 040409_00Sa
+
+Parameter Superceded Value New Value
+
+BODY10_GM 132712440017.9870 132712440035.0199
+BODY2_GM 324858.5988264598 324858.592000000
+BODY3_GM 403503.2334790870 403503.241738000
+BODY399_GM 398600.4328969392 398600.4415000001
+BODY5_GM 126712767.8577960 126712765.4543717
+BODY599_GM 126686536.9637693 126686534.5576417
+BODY6_GM 37940629.764 37940679.45741954
+BODY699_GM 37931267.73 37931289.4836
+BODY699_POLE_RA(1) 40.589 40.586420
+BODY699_POLE_RA(2) -0.036 -0.042290
+BODY699_POLE_DEC(1) 83.537 83.537291
+BODY699_POLE_DEC(2) -0.004 -0.004440
+BODY699_JCOEF(2) 0.016298 0.016292243237
+BODY699_JCOEF(4) -0.000915 -0.000928716077
+BODY699_JCOEF(6) 0.000103 0.000088845313
+BODY699_CCOEF(3) 0.00000070 0.0000000000000
+BODY699_SCOEF(3) -0.00000020 0.00000000
+BODY7_GM 5794549.007071874 5794549.007815570
+BODY301_GM 4902.800582147764 4902.800238000001
+BODY601_GM 2.5 2.539908238874431
+BODY602_GM 4.9 6.980134096218938
+BODY603_GM 41.808 41.21066708236702
+BODY604_GM 73.156 73.12382308588424
+BODY605_GM 154.000 154.6927779454911
+BODY606_GM 8978.2 8978.009444641593
+BODY607_GM 0.99 0.720000000000000
+BODY608_GM 106.0 132.2117925658847
+BODY609_GM 0.48 0.4852416379406062
+
+
+
+-------- REFERENCES
+
+ 1. Cassini NAV OD solution 040615_00Sa.
+ 2. Cassini NAV OD solution 040927_00aTa.
+ 3. Cassini NAV OD solution 041207_00cTc.
+ 4. Cassini NAV OD solution 050105_00bTb.
+ 5. Cassini Nav OD solution 050214_00cTc.
+ 6. Cassini Nav OD solution 050218_003T3.
+ 7. Cassini Nav OD solution 050312_004E1.
+ 8. Cassini Nav OD solution 050425_007Sa.
+ 9. Cassini Nav OD solution 050502_006T5.
+ 10. Cassini Nav OD solution 050513_007Sa.
+ 11. Cassini Nav OD solution 050606_008Sa.
+ 12. Cassini Nav OD solution 050613_009Sa.
+ 13. Cassini Nav OD solution 050707_010Sa.
+ 14. Cassini Nav OD solution 050718_011E2.
+ 15. Cassini Nav OD solution 050802_012Sa.
+ 16. Cassini Nav OD solution 050824_013T6.
+ 17. Cassini Nav OD solution 050911_014T7.
+ 18. Cassini Nav OD solution 050927_015H1.
+ 19. Cassini Nav OD solution 051012_016D1.
+ 20. Cassini Nav OD solution 051031_017T8.
+ 21. Cassini Nav OD solution 051128_018R1.
+ 22. Cassini Nav OD solution 051230_019T9.
+ 23. Cassini NAV OD solution 060121_020T10.
+ 24. Cassini NAV OD solution 060301_022T12.
+ 25. Cassini NAV OD solution 060301_021T11.
+ 26. Cassini NAV OD solution 060320_022T12.
+ 27. Cassini NAV OD solution 060503_023T13.
+ 28. Cassini NAV OD solution 060521_024T14.
+ 29. Cassini NAV OD solution 060705a_025T15.
+ 30. Cassini NAV OD solution 060723_026T16.
+ 31. Cassini NAV OD solution 060815_027Sa.
+ 32. Cassini NAV OD solution 060910_028T17.
+ 33. Cassini NAV OD solution 060926_029T18.
+ 34. Cassini NAV OD solution 061013_030T19.
+ 35. Cassini NAV OD solution 061029_031T20.
+ 36. Cassini NAV OD solution 061114_032Sa.
+ 37. Cassini NAV OD solution 061127a_033Sa.
+ 38. Cassini NAV OD solution 061211_034Sa.
+ 39. Cassini NAV OD solution 061214_035T21.
+ 40. Cassini NAV OD solution 061231a_036T22.
+ 41. Cassini NAV OD solution 061122_034Sa.
+ 42. Cassini NAV OD solution 070131_038T24.
+ 43. Cassini NAV OD solution 070227_039T25.
+ 44. Cassini NAV OD solution 070311_040T26.
+ 45. Cassini NAV OD solution 070328_041T27.
+ 46. Cassini NAV OD solution 070412_042T28.
+ 47. Cassini NAV OD solution 070429_043T29.
+ 48. Cassini NAV OD solution 070516_044T30.
+ 49. Cassini NAV OD solution 070531_045T31.
+ 50. Cassini NAV OD solution 070616_046T32.
+ 51. Cassini NAV OD solution 070703_047T33.
+ 52. Cassini NAV OD solution 070722_048T34.
+ 53. Cassini NAV OD solution 070902_049T35.
+
+ 54. Cassini NAV OD solution 071004_050T36.
+ 55. Cassini NAV OD solution 071121_051T37.
+ 56. Cassini NAV OD solution 071208_053T38.
+ 57. Cassini NAV OD solution 080108_055T40.
+ 58. Cassini NAV OD solution 080229_056T41.
+ 59. Cassini NAV OD solution 080313_060E3.
+ 60. Cassini NAV OD solution 080331_062T42.
+ 61. Cassini NAV OD solution 080516_063T43.
+ 62. Cassini NAV OD solution 080602_068T44.
+ 63. Cassini NAV OD solution 080803_070Sa.
+ 64. Cassini NAV OD solution 080816_079E4.
+ 65. Cassini NAV OD solution 081011_081E5.
+ 66. Cassini NAV OD solution 081106_089T46.
+ 67. Cassini NAV OD solution 081122_091T47.
+ 68. Cassini NAV OD solution 081208_094T48.
+ 69. Cassini NAV OD solution 081228_096T49.
+ 70. Cassini NAV OD solution 090209_098T50.
+ 71. Cassini NAV OD solution 090328_103T51.
+ 72. Cassini NAV OD solution 090407_107T52.
+ 73. Cassini NAV OD solution 090422_109T53.
+ 74. Cassini NAV OD solution 090507_110T54.
+ 75. Cassini NAV OD solution 090526_111T55.
+ 76. Cassini NAV OD solution 090609_112T56.
+ 77. Cassini NAV OD solution 090626_113T57.
+ 78. Cassini NAV OD solution 090710_114T58.
+ 79. Cassini NAV OD solution 090727_115T59.
+ 80. Cassini NAV OD solution 090810_116T60.
+ 81. Cassini NAV OD solution 090828_117T61.
+ 82. Cassini NAV OD solution 090903_118T62.
+ 83. Cassini NAV OD solution 091016_118T62.
+ 84. Cassini NAV OD solution 091105_120E7.
+ 85. Cassini NAV OD solution 091122_121E8.
+ 86. Cassini NAV OD solution 091214_122T63.
+ 87. Cassini NAV OD solution 100103_123T64.
+ 88. Cassini NAV OD solution 100131_125T66.
+ 89. Cassini NAV OD solution 100306_126R2.
+ 90. Cassini NAV OD solution 100409_128T67.
+ 91. Cassini NAV OD solution 100523_131T68.
+ 92. Cassini NAV OD solution 100608_132T69.
+ 93. Cassini NAV OD solution 100623_133T70.
+ 94. Cassini NAV OD solution 100709_134T71.
+ 95. Cassini NAV OD solution 100816_135E11.
+ 96. Cassini NAV OD solution 100927_137T72.
+ 97. Cassini NAV OD solution 101201_141E12.
+ 98. Cassini NAV OD solution 101223_142E13.
+ 99. Cassini NAV OD solution 110113_143R3.
+ 100. Cassini NAV OD solution 110511_148T76.
+ 101. Cassini NAV OD solution 110623_149T77.
+ 102. Cassini NAV OD solution 110915_150T78.
+ 103. Cassini NAV OD solution 111003_154E14.
+ 104. Cassini NAV OD solution 111216_157T79.
+ 105. Cassini NAV OD solution 120105_159T80.
+ 106. Cassini NAV OD solution 120203_160T81.
+ 107. Cassini NAV OD solution 120329_162E17.
+ 108. Cassini NAV OD solution 120416_164E18.
+ 109. Cassini NAV OD solution 120502_1_165E19.
+ 110. Cassini NAV OD solution 120523_166T83.
+ 111. Cassini NAV OD solution 120723_168T85.
+ 112. Cassini NAV OD solution 120926_170T86.
+ 113. Cassini NAV OD solution 121112_173T87.
+ 114. Cassini NAV OD solution 121201_175T88.
+ 115. Cassini NAV OD solution 121201_1_175T88.
+ 116. Cassini NAV OD solution 130216_176T89.
+ 117. Cassini NAV OD solution 130313_182R4.
+ 118. Cassini NAV OD solution 130408_184T90.
+ 119. Cassini NAV OD solution 130523_186T91.
+ 120. Cassini NAV OD solution 130713_191T92.
+ 121. Cassini NAV OD solution 130728_195T93.
+ 122. Cassini NAV OD solution 130911_1_196T94.
+ 123. Cassini NAV OD solution 131015_198T95.
+ 124. Cassini NAV OD solution 131203_199T96.
+ 125. Cassini NAV OD solution 140406_1_203T100.
+ 126. Cassini NAV OD solution 140520_204T101.
+ 127. Cassini NAV OD solution 140621_205T102.
+ 128. Cassini NAV OD solution 140820_207T104.
+ 129. Cassini NAV OD solution 140923_1_208T105.
+ 130. Cassini NAV OD solution 141023_1_209T106.
+ 131. Cassini NAV OD solution 141210_210T107.
+ 132. Cassini NAV OD solution 150214_212T109.
+ 133. Cassini NAV OD solution 150318_213T110.
+ 134. Cassini NAV OD solution 150507_214T111.
+ 135. Cassini NAV OD solution 150618_216D4.
+ 136. Cassini NAV OD solution 150709_218T112.
+ 137. Cassini NAV OD solution 150819_219D5.
+ 138. Cassini NAV OD solution 151001_221T113.
+ 139. Cassini NAV OD solution 151018_223E20.
+ 140. Cassini NAV OD solution 151030_224E21.
+ 141. Cassini NAV OD solution 151115_225T114.
+ 142. Cassini NAV OD solution 151222_226E22.
+ 143. Cassini NAV OD solution 160118_229T115.
+ 144. Cassini NAV OD solution 160203_231T116.
+ 145. Cassini NAV OD solution 160218_232T117.
+ 146. Cassini NAV OD solution 160405_233T118.
+ 147. Cassini NAV OD solution 160504_235T119.
+ 148. Cassini NAV OD solution 160606_236T120.
+ 149. Cassini NAV OD solution 160724_237T121.
+ 150. Cassini NAV OD solution 160810_1_239T122.
+ 151. Cassini NAV OD solution 160926_240T123.
+ 152. Cassini NAV OD solution 161019_244T124.
+ 153. Cassini NAV OD solution 161116_246T124.
+ 154. Cassini NAV OD solution 161202_1_249T125.
+ 155. Cassini NAV OD solution 170105_251T126.
+ 156. Cassini NAV OD solution 170423_254T126.
+ 157. Cassini NAV OD solution 170421_264T126.
+ 158. Cassini NAV OD solution 170507_269GF.
+ 159. Cassini NAV OD solution 170608_271GF.
+ 160. Cassini NAV OD solution 170714_276GF.
+ 161. Cassini NAV OD solution 170813_281GF.
+ 162. Cassini NAV OD solution 170915_1_288GF.
+
+KPL/PCK
+
+\begindata
+ CASSINI_PCK_VERSION = ( '2010-SEP-02' )
+\begintext
+
+
+P_constants (PcK) SPICE kernel file
+
+Refer to the notes at the bottom of the file for help, contacts,
+version history, references, and Cassini-specific parameter descriptions.
+All radii and orientation values are from reference [1] unless
+otherwise noted.
+
+This file was created by separating science controlled values from NAVT
+controlled values for ease of file maintenance. References to GMs provided
+by the NAVT, Saturn Pole RA and DEC, and JCOEFF and SCOEFF have been removed.
+
+-------- SUN
+
+ Value for the Sun radii is from [2], page K7.
+
+ \begindata
+ BODY10_RADII = ( 696000. 696000. 696000. )
+ BODY10_POLE_RA = ( 286.13 0. 0. )
+ BODY10_POLE_DEC = ( 63.87 0. 0. )
+ BODY10_PM = ( 84.10 +14.18440 0. )
+ BODY10_LONG_AXIS = ( 0. )
+ \begintext
+
+
+-------- VENUS
+
+ \begindata
+
+ BODY299_RADII = ( 6051.8 6051.8 6051.8 )
+ BODY299_POLE_RA = ( 272.76 0. 0. )
+ BODY299_POLE_DEC = ( +67.16 0. 0. )
+ BODY299_PM = ( 160.20 -1.4813688 0. )
+ BODY299_LONG_AXIS = ( 0. )
+ \begintext
+
+
+-------- EARTH
+
+
+ Northern hemisphere projection of the Earth's magnetic dipole:
+ coordinates are planetocentric, values are from [3].
+
+ \begindata
+ BODY399_RADII = ( 6378.140 6378.140 6356.75 )
+ BODY399_POLE_RA = ( 0. -0.641 0. )
+ BODY399_POLE_DEC = ( +90. -0.557 0. )
+ BODY399_PM = ( 190.147 +360.9856235 0. )
+ BODY399_LONG_AXIS = ( 0. )
+ BODY3_NUT_PREC_ANGLES = ( 125.045 -1935.5364525000
+ 250.089 -3871.0729050000
+ 260.008 475263.3328725000
+ 176.625 487269.6299850000
+ 357.529 35999.0509575000
+ 311.589 964468.4993100001
+ 134.963 477198.8693250000
+ 276.617 12006.3007650000
+ 34.226 63863.5132425000
+ 15.134 -5806.6093575000
+ 119.743 131.8406400000
+ 239.961 6003.1503825000
+ 25.053 473327.7964200000 )
+ BODY399_MAG_NORTH_POLE_LON = ( -69.761 )
+ BODY399_MAG_NORTH_POLE_LAT = ( 78.565 )
+ \begintext
+
+
+-------- JUPITER
+
+
+ \begindata
+ BODY599_RADII = ( 71492. 71492. 66854. )
+ BODY599_POLE_RA = ( 268.05 -0.009 0. )
+ BODY599_POLE_DEC = ( +64.49 +0.003 0. )
+ BODY599_PM = ( 284.95 +870.5366420 0. )
+ BODY599_LONG_AXIS = ( 0. )
+ BODY5_NUT_PREC_ANGLES = ( 73.32 91472.9
+ 24.62 45137.2
+ 283.90 4850.7
+ 355.80 1191.3
+ 119.90 262.1
+ 229.80 64.3
+ 352.35 2382.6
+ 113.35 6070.0
+ 146.64 182945.8
+ 49.24 90274.4 )
+
+ \begintext
+
+
+-------- SATURN
+
+ The first seven angles given in NUT_PREC are the angles S1
+ through S7 from the 2000 IAU report; the eighth and ninth
+ angles are 2*S1 and 2*S2, respectively.
+
+ Ring models are from [4], [19], [20]. They are also documented in
+ [11] and [12].
+ F Ring Data are from [8].
+ MIMI zone reflects the old flight rule
+ for MIMI INCA, +/- 30000 km thickness inside of 8.74 Rs.
+
+ BODY699_RADII_OPTICAL is for PDT to determine at what altitude
+ that Saturn first starts to cast a discernible shadow.
+
+ BODY699_RADII_RS models Saturn as a sphere and corresponds to a 100
+ mbar surface. BODY699_RADII and BODY699_RADII_1BAR correspond to a
+ 1 bar surface. BODY699_RADII contains IAU values. BODY699_RADII_1BAR
+ currently contains IAU values but will likely be updated during the
+ mission. It is generally agreed that 60330.0 is the Saturn reference radius.
+ This value in stored later in the file under the keyword RS.
+
+ Eventually three different magnetospheric models will be provided. This
+ section currently serves as a placeholder.
+
+ BODY699_MAG_NORTH_POLE_LON = ( 0.0 )
+ BODY699_MAG_NORTH_POLE_LAT = ( +90.0 )
+ BODY699_M1COEF = ( 0.0 0.0 0.0 0.0)
+ BODY699_G1COEF = ( 0.0 0.0 0.0 0.0)
+ BODY699_H1COEF = ( 0.0 0.0 0.0 0.0)
+ BODY699_M2COEF = ( 0.0 0.0 0.0 0.0)
+ BODY699_G2COEF = ( 0.0 0.0 0.0 0.0)
+ BODY699_H2COEF = ( 0.0 0.0 0.0 0.0)
+ BODY699_M3COEF = ( 0.0 0.0 0.0 0.0)
+ BODY699_G3COEF = ( 0.0 0.0 0.0 0.0)
+ BODY699_H3COEF = ( 0.0 0.0 0.0 0.0)
+
+
+ \begindata
+ BODY699_RADII = ( 60268. 60268. 54364. )
+ BODY699_RADII_1BAR = ( 60268. 60268. 54364. )
+ BODY699_RADII_OPTICAL = ( 60430. 60430. 54508. )
+ BODY699_RADII_RS = ( 60330. 60330. 60330. )
+ BODY699_PM = ( 38.90 +810.7939024 0. )
+ BODY699_LONG_AXIS = ( 0. )
+ BODY6_NUT_PREC_ANGLES = ( 353.32 75706.7
+ 28.72 75706.7
+ 177.40 -36505.5
+ 300.00 -7225.9
+ 316.45 506.2
+ 345.20 -1016.3
+ 29.80 -52.1
+ 706.64 151413.4
+ 57.44 151413.4 )
+ BODY699_RING1_NAME = 'A Ring'
+ BODY699_RING1 = (122170.0 136780.0 0.1 0.1 0.5)
+ BODY699_RING1_1_NAME = 'Encke Gap'
+ BODY699_RING1_1 = (133405.0 133730.0 0.0 0.0 0.0)
+ BODY699_RING2_NAME = 'Cassini Division'
+ BODY699_RING2 = (117580.0 122170.0 0.0 0.0 0.0)
+ BODY699_RING3_NAME = 'B Ring'
+ BODY699_RING3 = (92000.0 117580.0 0.1 0.1 1.5)
+ BODY699_RING4_NAME = 'C Ring'
+ BODY699_RING4 = (74510.0 92000.0 0.1 0.1 0.1)
+ BODY699_RING5_NAME = 'D Ring'
+ BODY699_RING5 = (66970.0 74510.0 0.1 0.1 0.00001)
+ BODY699_RING6_NAME = 'E ring'
+ BODY699_RING6_A = (189870.0 256900.0 9000.0 9000.0 0.000003)
+ BODY699_RING6_B = (256900.0 420000.0 9000.0 17000.0 0.000003)
+ BODY699_RING7_NAME = 'F Ring'
+ BODY699_RING7 = (140180.0 140270.0 6.5 6.5 0.1)
+ BODY699_RING7_FCENTER = (140223.7, 0.00254, 24.1, 2.7001, 0.0065, 16.1, -2.6876)
+ BODY699_RING8_NAME = 'G Ring'
+ BODY699_RING8 = (165000.0 176000.0 280.0 280.0 0.000001)
+ BODY699_MIMI_DUST_ZONE = ( 0.0 527284.2 60000.0 60000.0 )
+ \begintext
+
+
+-------- URANUS
+
+
+ \begindata
+ BODY799_RADII = ( 25559. 25559. 24973. )
+ BODY799_POLE_RA = ( 257.311 0. 0. )
+ BODY799_POLE_DEC = ( -15.175 0. 0. )
+ BODY799_PM = ( 203.81 -501.1600928 0. )
+ BODY799_LONG_AXIS = ( 0. )
+ \begintext
+
+
+-------- MOON
+
+
+ \begindata
+ BODY301_RADII = ( 1737.4 1737.4 1737.4 )
+ BODY301_POLE_RA = ( 269.9949 0.0031 0. )
+ BODY301_POLE_DEC = ( 66.5392 0.0130 0. )
+ BODY301_PM = ( 38.3213 13.17635815 -1.4D-12 )
+ BODY301_LONG_AXIS = ( 0. )
+ BODY301_NUT_PREC_RA = ( -3.8787 -0.1204 +0.0700 -0.0172
+ 0. +0.0072 0. 0.
+ 0. -0.0052 0. 0.
+ +0.0043 )
+ BODY301_NUT_PREC_DEC = ( 1.5419 0.0239 -0.0278 +0.0068
+ 0. -0.0029 +0.0009 0.
+ 0. +0.0008 0. 0.
+ -0.0009 )
+ BODY301_NUT_PREC_PM = ( 3.5610 +0.1208 -0.0642 +0.0158
+ +0.0252 -0.0066 -0.0047 -0.0046
+ +0.0028 +0.0052 +0.0040 +0.0019
+ -0.0044 )
+ \begintext
+
+
+Satellites of Jupiter
+-------------------------------------------------------
+
+-------- IO
+
+
+ BODY501_GM value from [5].
+
+ \begindata
+ BODY501_GM = ( 5959.916 )
+ BODY501_RADII = ( 1829.4 1819.3 1815.7 )
+ BODY501_POLE_RA = ( 268.05 -0.009 0. )
+ BODY501_POLE_DEC = ( +64.50 +0.003 0. )
+ BODY501_PM = ( 200.39 +203.4889538 0. )
+ BODY501_LONG_AXIS = ( 0. )
+ BODY501_NUT_PREC_RA = ( 0. 0. +0.094 +0.024 )
+ BODY501_NUT_PREC_DEC = ( 0. 0. +0.040 +0.011 )
+ BODY501_NUT_PREC_PM = ( 0. 0. -0.085 -0.022 )
+ \begintext
+
+
+-------- EUROPA
+
+
+ BODY502_GM value from [5].
+
+ \begindata
+ BODY502_GM = ( 3202.739 )
+ BODY502_RADII = ( 1564.13 1561.23 1560.93 )
+ BODY502_POLE_RA = ( 268.08 -0.009 0. )
+ BODY502_POLE_DEC = ( +64.51 +0.003 0. )
+ BODY502_PM = ( 36.022 +101.3747235 0. )
+ BODY502_LONG_AXIS = ( 0. )
+ BODY502_NUT_PREC_RA = ( 0. 0. 0. +1.086 +0.060 +0.015 +0.009 )
+ BODY502_NUT_PREC_DEC = ( 0. 0. 0. +0.468 +0.026 +0.007 +0.002 )
+ BODY502_NUT_PREC_PM = ( 0. 0. 0. -0.980 -0.054 -0.014 -0.008 )
+ \begintext
+
+
+-------- GANYMEDE
+
+
+ BODY503_GM value from [5].
+
+
+ \begindata
+ BODY503_GM = ( 9887.834 )
+ BODY503_RADII = ( 2632.4 2632.29 2632.35 )
+ BODY503_POLE_RA = ( 268.20 -0.009 0. )
+ BODY503_POLE_DEC = ( +64.57 +0.003 0. )
+ BODY503_PM = ( 44.064 +50.3176081 0. )
+ BODY503_LONG_AXIS = ( 0. )
+ BODY503_NUT_PREC_RA = ( 0. 0. 0. -0.037 +0.431 +0.091 )
+ BODY503_NUT_PREC_DEC = ( 0. 0. 0. -0.016 +0.186 +0.039 )
+ BODY503_NUT_PREC_PM = ( 0. 0. 0. +0.033 -0.389 -0.082 )
+ \begintext
+
+
+-------- CALLISTO
+
+
+ BODY504_GM value from [5].
+
+ \begindata
+ BODY504_GM = ( 7179.289 )
+ BODY504_RADII = ( 2409.4 2409.2 2409.3 )
+ BODY504_POLE_RA = ( 268.72 -0.009 0. )
+ BODY504_POLE_DEC = ( +64.83 +0.003 0. )
+ BODY504_PM = ( 259.51 +21.5710715 0. )
+ BODY504_LONG_AXIS = ( 0. )
+ BODY504_NUT_PREC_RA = ( 0. 0. 0. 0. -0.068 +0.590 0. +0.010 )
+ BODY504_NUT_PREC_DEC = ( 0. 0. 0. 0. -0.029 +0.254 0. -0.004 )
+ BODY504_NUT_PREC_PM = ( 0. 0. 0. 0. +0.061 -0.533 0. -0.009 )
+ \begintext
+
+
+-------- HIMALIA
+
+
+ BODY506_GM values from [21].
+
+ \begindata
+ BODY506_GM = ( 0.45 )
+ BODY506_RADII = ( 85 85 85 )
+ BODY506_POLE_RA = ( 268.72 -0.009 0. )
+ BODY506_POLE_DEC = ( +64.83 +0.003 0. )
+ BODY506_PM = ( 259.51 +21.5710715 0. )
+ BODY506_LONG_AXIS = ( 0. )
+ \begintext
+
+
+Satellites of Saturn
+-----------------------------------------------------------
+
+-------- MIMAS
+
+
+ BODY601_RADII values from [22].
+ BODY601_PM values from [24].
+
+ \begindata
+ BODY601_RADII = ( 207.4 196.8 190.6 )
+ BODY601_POLE_RA = ( 40.66 -0.036 0. )
+ BODY601_POLE_DEC = ( +83.52 -0.004 0. )
+ BODY601_PM = ( 333.46 +381.9945550 0. )
+ BODY601_LONG_AXIS = ( 0. )
+ BODY601_NUT_PREC_RA = ( 0. 0. +13.56 0. 0. 0. 0. 0. 0. )
+ BODY601_NUT_PREC_DEC = ( 0. 0. -1.53 0. 0. 0. 0. 0. 0. )
+ BODY601_NUT_PREC_PM = ( 0. 0. -13.48 0. -44.85 0. 0. 0. 0. )
+ \begintext
+
+
+-------- ENCELADUS
+
+
+ BODY602_RADII values from [22].
+ BODY602_PM values from [24].
+
+ \begindata
+ BODY602_RADII = ( 256.6 251.4 248.3 )
+ BODY602_POLE_RA = ( 40.66 -0.036 0. )
+ BODY602_POLE_DEC = ( +83.52 -0.004 0. )
+ BODY602_PM = ( 6.32 +262.7318996 0. )
+ BODY602_LONG_AXIS = ( 0. )
+ \begintext
+
+
+-------- TETHYS
+
+ BODY603_RADII values from [22].
+ BODY603_PM values from [24].
+
+ \begindata
+ BODY603_RADII = ( 540.4 531.1 527.5 )
+ BODY603_POLE_RA = ( 40.66 -0.036 0. )
+ BODY603_POLE_DEC = ( +83.52 -0.004 0. )
+ BODY603_PM = ( 8.95 +190.6979085 0. )
+ BODY603_LONG_AXIS = ( 0. )
+ BODY603_NUT_PREC_RA = ( 0. 0. 0. +9.66 0. 0. 0. 0. 0. )
+ BODY603_NUT_PREC_DEC = ( 0. 0. 0. -1.09 0. 0. 0. 0. 0. )
+ BODY603_NUT_PREC_PM = ( 0. 0. 0. -9.60 +2.23 0. 0. 0. 0. )
+ \begintext
+
+
+-------- DIONE
+
+ BODY604_RADII values from [22].
+ BODY604_PM values from [24].
+
+ \begindata
+ BODY604_RADII = ( 563.8 561.0 560.3 )
+ BODY604_POLE_RA = ( 40.66 -0.036 0. )
+ BODY604_POLE_DEC = ( +83.52 -0.004 0. )
+ BODY604_PM = ( 357.60 +131.5349316 0. )
+ BODY604_LONG_AXIS = ( 0. )
+ \begintext
+
+
+-------- RHEA
+
+ BODY605_RADII values from [22].
+ BODY605_PM values from [24].
+
+ \begindata
+ BODY605_RADII = ( 767.2 762.5 763.1 )
+ BODY605_POLE_RA = ( 40.38 -0.036 0. )
+ BODY605_POLE_DEC = ( +83.55 -0.004 0. )
+ BODY605_PM = ( 235.16 +79.6900478 0. )
+ BODY605_LONG_AXIS = ( 0. )
+ BODY605_NUT_PREC_RA = ( 0. 0. 0. 0. 0. +3.10 0. 0. 0. )
+ BODY605_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. -0.35 0. 0. 0. )
+ BODY605_NUT_PREC_PM = ( 0. 0. 0. 0. 0. -3.08 0. 0. 0. )
+ \begintext
+
+
+-------- TITAN
+
+ Titan Pole Use restriction:
+
+ The proposed new PCK Titan pole model incorporates a new pole position
+ (RA, Dec) with Titan's synchronous spin rate. This model reduces
+ mislocation errors for RADAR passes between TA and T30 from 30km to
+ about 2.5km. The new model contains no rate or nutation terms.
+ Nominal values of these terms would cause changes of less than about 2km
+ in the position of surface features over the period 2000-2020.
+
+ BODY606_POLE_RA, BODY606_POLE_DEC, BODY606_PM, BODY606_NUT_PREC_RA
+ BODY606_NUT_PREC_DEC, BODY606_NUT_PREC_PM values from [23].
+
+ \begindata
+ BODY606_RADII = ( 2575. 2575. 2575. )
+ BODY606_POLE_RA = ( +39.4827 0. 0. )
+ BODY606_POLE_DEC = ( +83.4279 0. 0. )
+ BODY606_PM = ( 186.5855 22.5769768 0. )
+ BODY606_LONG_AXIS = ( 0. )
+ BODY606_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. )
+ BODY606_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. )
+ BODY606_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. )
+ BODY606_ATMOSPHERE = ( 175.0 10.0
+ 0.000006350 11400.0 76.0
+ 0.000000513 8030.0 -429.0
+ 0.000073500 15000.0 44.0 )
+ \begintext
+
+
+-------- HYPERION
+
+
+ While Hyperion's spin state is chaotic, Voyager and ground-based
+ observations suggest some states are common (Thomas et al 1995,
+ Icarus 117, 128-148). The spin pole orientation is from the
+ Voyager observations; both the spin pole orientation and spin rate
+ will probably differ during Cassini's mission. Hyperion radii and
+ orientation from Peter Thomas @ Cornell
+
+
+ \begindata
+ BODY607_RADII = ( 164. 130. 107. )
+ BODY607_POLE_RA = ( 226. 0 0 )
+ BODY607_POLE_DEC = ( 35. 0 0 )
+ BODY607_PM = ( 20.02 72.0 0 )
+ BODY607_LONG_AXIS = ( 0. )
+ \begintext
+
+
+-------- IAPETUS
+
+ BODY608_RADII values from [22].
+ BODY608_PM values from [24].
+
+ \begindata
+ BODY608_RADII = ( 747.4 747.4 712.4 )
+ BODY608_POLE_RA = ( 318.16 -3.949 0. )
+ BODY608_POLE_DEC = ( +75.03 -1.143 0. )
+ BODY608_PM = ( 355.20 +4.5379572 0. )
+ BODY608_LONG_AXIS = ( 0. )
+ \begintext
+
+
+-------- PHOEBE
+
+
+ BODY609_PM from [13].
+
+
+ \begindata
+ BODY609_RADII = ( 115. 110. 105. )
+ BODY609_POLE_RA = ( 355.00 0. 0. )
+ BODY609_POLE_DEC = ( +68.70 0. 0. )
+ BODY609_PM = ( 178.58 +931.639 0. )
+ BODY609_LONG_AXIS = ( 0. )
+ \begintext
+
+-------- CONSTANTS AND NOTES FOR PDT USERS
+
+
+ The astronomical unit AU, given in kilometers.
+
+ \begindata
+ AU = ( 149597870.7 )
+ \begintext
+
+
+ Saturn reference radius (Rs) is the base for measuring body
+ distances and ring radial distances in mulitples of saturn radius.
+
+
+ \begindata
+ RS = ( 60330.0 )
+ \begintext
+
+
+
+ Note that GM values >= 1.0 are packaged as is into 7CONIC_VEC
+ commands for AACS to propagate the body's ephemeris.
+ For GM values < 1.0, the value in the G_MASS parameter
+ of the 7CONIC_VEC command is set to 1.0. One is the minimum
+ value for the G_MASS parameter. The resetting of the G_MASS
+ parameter to the minimum acceptable where the actual
+ GM is < 1.0 is acceptable since CAS will not pass close enough
+ to any of the affected bodies for the gravitational mass
+ to have an effect.
+
+-------- OBLATE SPHEROIDS VERSUS TRIAXIAL ELLIPSOIDS
+
+
+ Some Cassini software cannot model triaxial ellipsoids, where the
+ RADII are all different. Instead, they model bodies as oblate
+ spheroids, where the equatorial RADII values (the first two) must
+ be identical. In cases here where the equatorial radii are not
+ identical, the average of the two should be used when constructing
+ an oblate spheroid. The polar radius (the third RADII) can be used
+ as given in both cases.
+
+
+-------- CONSTANTS AND NOTES FOR CASPER USERS
+
+
+ \begindata
+ BODY601_GM/PRIMARY = ( 6.59087D-08 )
+ BODY602_GM/PRIMARY = ( 1.29181D-07 )
+ BODY603_GM/PRIMARY = ( 1.1022D-06 )
+ BODY604_GM/PRIMARY = ( 1.92865D-06 )
+ BODY605_GM/PRIMARY = ( 4.05998D-06 )
+ BODY606_GM/PRIMARY = ( 2.36697D-04 )
+ BODY607_GM/PRIMARY = ( 2.60998D-08 )
+ BODY608_GM/PRIMARY = ( 2.79453D-06 )
+ BODY609_GM/PRIMARY = ( 1.26545D-08 )
+ BODY610_GM/PRIMARY = ( 3.38507D-09 )
+ BODY611_GM/PRIMARY = ( 9.41176D-10 )
+ BODY612_GM/PRIMARY = ( 4.48179D-11 )
+ BODY613_GM/PRIMARY = ( 1.26545D-11 )
+ BODY614_GM/PRIMARY = ( 6.32723D-12 )
+ BODY615_GM/PRIMARY = ( 1.89817D-11 )
+ BODY616_GM/PRIMARY = ( 5.79996D-10 )
+ BODY617_GM/PRIMARY = ( 3.42725D-10 )
+ BODY618_GM/PRIMARY = ( 4.74543D-12 )
+ \begintext
+
+-------- URLS AND CONTACTS
+
+
+Description of PCK format and contents can be found in NAIF's PCK "required
+reading" document, at:
+
+ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/ascii/individual_docs/pck.req
+
+
+NAIF tutorial on PCK formatting and use at:
+
+ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/Tutorials/office/individual_docs/16_pck.ppt
+ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/Tutorials/office/packages/
+SPICE_Tutorials_Office.zip
+
+
+The Cassini PCK & ephemeris files can be found on the DOM, and at:
+
+ftp://naif.jpl.nasa.gov/pub/naif/CASSINI/kernels/
+
+
+Questions regarding this file can be directed to:
+
+Diane Conner (818)354-8586 Diane.Conner@jpl.nasa.gov
+Adrian Tinio (818)354-7511 Adrian.Tinio@jpl.nasa.gov
+David Seal (818)354-2707 David.Seal@jpl.nasa.gov
+
+
+-------- VERSION HISTORY
+
+The noted versions were officially published; the others were
+created and circulated for internal review only.
+
+2010 Sep 02 (published)
+A. Tinio
+
+ECR-110654 Implementation
+
+Update the rotation parameter W0 to IAU 2009 values
+
+NEW VALUES:
+ BODY601_PM = ( 333.46 +381.9945550 0. )
+ BODY602_PM = ( 6.32 +262.7318996 0. )
+ BODY603_PM = ( 8.95 +190.6979085 0. )
+ BODY604_PM = ( 357.60 +131.5349316 0. )
+ BODY605_PM = ( 235.16 +79.6900478 0. )
+ BODY608_PM = ( 355.20 +4.5379572 0. )
+
+OLD VALUES:
+ BODY601_PM = ( 337.46 +381.9945550 0. )
+ BODY602_PM = ( 2.82 +262.7318996 0. )
+ BODY603_PM = ( 10.45 +190.6979085 0. )
+ BODY604_PM = ( 357.00 +131.5349316 0. )
+ BODY605_PM = ( 235.16 +79.6900478 0. )
+ BODY608_PM = ( 350.20 +4.5379572 0. )
+
+2008 Apr 16 (published)
+A. Tinio
+
+ECR-107847 Implementation
+
+1. Update radii values for Mimas, Enceladus, Tethys, Dione, Rhea, and Iapetus.
+
+NEW VALUES:
+ BODY601_RADII = ( 207.4 196.8 190.6 ) MIMAS
+ BODY602_RADII = ( 256.6 251.4 248.3 ) ENCELADUS
+ BODY603_RADII = ( 540.4 531.1 527.5 ) TETHYS
+ BODY604_RADII = ( 563.8 561.0 560.3 ) DIONE
+ BODY605_RADII = ( 767.2 762.5 763.1 ) RHEA
+ BODY608_RADII = ( 747.4 747.4 712.4 ) IAPETUS
+
+SUPERCEDED VALUES:
+ BODY601_RADII = ( 209.1 196.2 191.4 ) MIMAS
+ BODY602_RADII = ( 256.3 247.3 244.6 ) ENCELADUS
+ BODY603_RADII = ( 535.6 528.2 525.8 ) TETHYS
+ BODY604_RADII = ( 560. 560. 560. ) DIONE
+ BODY605_RADII = ( 764. 764. 764. ) RHEA
+ BODY608_RADII = ( 718. 718. 718. ) IAPETUS
+
+Radii values are from:
+
+Porco, C.C., Thomas, P.C., Weiss, J.W., Richardson, D.C. 2007. Saturns Small Inner Satellites: Clues to Their Origins. Science 318, 1602.
+
+Thomas, P.C., and 12 colleagues 2007. Shapes of the saturnian icy satellites and their significance. Icarus 190, 573-584.
+
+
+2. Update Titan pole position -
+
+NEW VALUES:
+ BODY606_POLE_RA = ( +39.4827 0. 0. )
+ BODY606_POLE_DEC = ( +83.4279 0. 0. )
+ BODY606_PM = ( 186.5855 22.5769768 0. )
+ BODY606_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 0.0 0. 0. )
+ BODY606_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0.0 0. 0. )
+ BODY606_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. 0.0 0. 0. )
+
+SUPERCEDED VALUES:
+ BODY606_POLE_RA = ( 36.41 -0.036 0. )
+ BODY606_POLE_DEC = ( +83.94 -0.004 0. )
+ BODY606_PM = ( 189.64 +22.5769768 0. )
+ BODY606_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. +2.66 0. 0. )
+ BODY606_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. -0.30 0. 0. )
+ BODY606_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. -2.64 0. 0. )
+
+Titan PCK values from: Bryan Stiles
+
+
+2004 Dec 09 (published)
+D. Conner
+
+This file was created from file cpck14Oct2004.tpc.
+It contains keywords that will be maintained by the PSG. NAVT maintained
+keywords have been moved in a separate file.
+
+Minor satellites and rocks keywords have been moved to the rocks
+PCK.
+
+
+2004 Oct 14 (published)
+
+Documentation was added to clarify the different radii defined for Saturn.
+Additional references that are publicly available were added for Saturn's
+rings model. Jupiter's nutation precession angles, and
+Ganymede's W0 value were corrected to agree with the IAU 2000 report.
+
+2004 Jun 21 (published)
+
+* Reference for new Phoebe GM: IOM 312.0-024-04 "Navigation Results
+from the Phoebe flyby", J.B. Jones, 16 June 2004.
+
+
+2004 Mar 05 (published)
+
+ Updated descriptive text preceeding RS keyword.
+ Updated contact information and verified URLs.
+
+ Updates per ECR 103313:
+ Change 1: Update the values for Phoebe Prime Meridian
+ TO:
+ BODY609_PM = ( 178.58 +931.639 0. )
+
+ Reference: Bauer, Simonelli, Buratti, IAU Circular 8279,
+ 1/30/2004; re-reduced by Owen 2/5/2004
+
+ Change 2: Saturn Reference Radius
+ ADD:
+ BODY699_RADII_RS = ( 60330. 60330. 60330. )
+ This radius models saturn as a sphere at 100 mbar.
+
+ Date: Tue, 25 Nov 2003 16:22:41 -0700
+ From: Carolyn Porco <carolyn@ciclops.org>
+
+2002 Oct 01 (published)
+ Changed BODY699_RADII_OPTICAL to be consistent with recommendation of Phil
+ Nicholson dated 24 Sep. Added notes in the version history as to which
+ versions were published to the DOM, as opposed to the versions that were
+ intermediate for review.
+
+
+
+
+-------- FORMATTING FOR SPECIAL PARAMETERS
+
+
+BODYNNN_GM
+ GM in km^3/s^2
+
+BODYNNN_RADII_OPTICAL
+BOYDNNN_RADII_RS
+BOYDNNN_RADII
+BODYNNN_RADII_1BAR
+
+ BODY699_RADII_OPTICAL is for PDT to determine at what altitude
+ that Saturn first starts to cast a discernible shadow.
+
+ BODY699_RADII_RS models Saturn as a sphere and corresponds to a 100
+ mbar surface.
+
+ BODY699_RADII and BODY699_RADII_1BAR correspond to a
+ 1 bar surface. BODY699_RADII contains IAU values. BODY699_RADII_1BAR
+ currently contains IAU values but will likely be updated during the
+ mission.
+
+
+BODYNNN_ATMOSPHERE
+ Exponential atmospheric model in the form of one set of
+ two values To, f, followed by any number of sets of
+ three numbers Do, K, Zo. The atmospheric density in g/cm3
+ can be calculated as follows:
+ Z = height above surface (km)
+ R = radius of body (km)
+ T = thermospheric temperature (K) = To + f * sigma, where
+ sigma is the number of standard deviations (conservatism)
+ desired. If f > 0, positive sigma will result in a hotter
+ thermosphere and higher density.
+ H = scale height of atmosphere (km) = T * ( R + Z ) / K
+ (K is a curve-fit parameter with units of degrees K)
+ D = density (g/cm3) = Do * exp( - ( Z - Zo ) / H )
+ If there are more than one set of Do, K, Zo, sum each
+ value to get the total atmospheric density.
+
+
+BODYNNN_RING*
+ The ring identification scheme is numeric with keyword-associated names.
+ The defnition of a ring is in a set of keywords. The BODYNNN_RING...
+ keyword set includes
+
+
+ 1) a required NAME keyword (BODYNNN_RING<n>_NAME),
+ 2) either a complete ring keyword (BODYNNN_RING<n>) or a set of segmented
+ ring keywords (BODYNNN_RING<n>_<X>), and
+ 3) optional embedded ringlet/gap keywords (BODYNNN_RING<n>_<n>) with
+ required names (BODYNNN_RING<n>_<n>_NAME).
+
+
+ The total number of rings (BODYNNN_RING<n>) that can be defined is from
+ 01 to 99. A complete ring can be segmented (BODYNNN_RING<n>_<X>) in upto
+ 26 (A-Z) sub-segments. Embedded ringlets/gaps (BODYNNN_RING<n>_<n>) can
+ be defined from 1 to 99. Ring geometry is defined in the form of one set
+ of R1, R2, Z1, Z2, OD where R1 and R2 are inner and outer radii
+ respectively of the ring (in kilometers), Z1 and Z2 are the vertical
+ heights of the ring at R1 and R2 respectively (also in km, equal to
+ one-half of the total thickness of the ring), and OD is the average optical
+ depth of the ring sub-segment/gap across R1 to R2. A complex ring
+ thickness model is pieced together by sub-segmenting Rs, Zs, & ODs; each
+ sub-segment is uniquely numbered.
+
+
+
+
+BODY699_RING7_FCENTER
+ Elliptical orbital characteristics for the F Ring: The array items (and
+ units) are (in order):
+
+
+ SEMIMAJOR_AXIS (km)
+ ECCENTRICITY (degrees)
+ LONGITUDE_PERICENTER_EPOCH (degrees)
+ PERICENTER_PRECESSION_RATE (degrees)
+ INCLINATION (degrees)
+ LONGITUDE_ASCENDING_NODE_EPOCH (degrees)
+ NODAL_REGRESSION_RATE (degrees).
+
+
+ The epoch for the elements is J2000 (noon UTC on 1/1/2000) at the ring
+ (i.e., with no light-time correction). Longitudes are measured in the
+ prograde direction from the ascending node of Saturn's equatorial plane
+ on Earth's J2000 equator.
+
+
+-------- REFERENCES
+
+ 1. Seidelmann, P.K., Abalakin, V.K., Bursa, M., Davies, M.E.,
+ Bergh, C. de, Lieske, J.H., Oberst, J., Simon, J.L.,
+ Standish, E.M., Stooke, P., and Thomas, P.C. (2002).
+ "Report of the IAU/IAG Working Group on Cartographic
+ Coordinates and Rotational Elements of the Planets and
+ Satellites: 2000," Celestial Mechanics and Dynamical
+ Astronomy, v.82, Issue 1, pp. 83-111.
+
+ 2. Nautical Almanac Office, United States Naval Observatory
+ and H.M. Nautical Almanac Office, Rutherford Appleton
+ Laboratory (2005). "The Astronomical Almanac for
+ the Year 2002," U.S. Government Printing Office,
+ Washington, D.C.: and The Stationary Office, London.
+
+ 3. Russell, Christopher T., "Geophysical Coordinate Transformations,"
+ Cosmic Electrodynamics 2 (1971) 184-186.
+
+ 4. Showalter, Mark R. "Properties of Saturn's E and G Rings from the
+ 1995 Ring Plane Crossings", presented at Ames ring hazard
+ workshop, 25 January 1996.
+
+ 5. Jacobson, R. A. 2003b. private communication of constants
+ used in the JUP230 ephemeris
+
+ 6. Jacobson, R.A., JPL IOM 312.F-99-084, 13 Oct 1999, "Sat105"
+ ephemeris file
+
+ 7. Jacobson, R. A., 1996, "Orbits of the Saturnian Satellites
+ from Earthbased and Voyager Observations", Blulletin of the
+ American Astronmical Society 28(3), 1185.
+
+ 8. Bosh A.S., Olkin C.B., French R.G., Nicholson P.D. Icarus,
+ May 2002, vol. 157, iss. 1, pp. 57-75(19)
+
+ 9. Campbell, J.K., and J.D. Anderson, Gravity Field of the Saturnian
+ System From Pioneer and Voyager Tracking Data, Astronomical
+ Journal, 97, 1485-1495, 1989.
+
+ 10. Cassini NAV OD solution SM828D.
+
+ 11. Cassini Mission Plan, JPL D-5564, Cassini document 699-100,
+ revision N, May 2002.
+
+ 12. Cassini Dust Protection Plan, JPL D-24251, Cassini document 699-525,
+ revision A, October 2002.
+
+ 13. Bauer, Simonelli, Buratti, IAU Circular 8279, 1/30/2004;
+ re-reduced by Owen 2/5/2004
+
+ 14. Cassini NAV OD solution 040409_00Sa.
+
+ 15. Cassini NAV OD solution 040615_00Sa.
+
+ 16. IOM 312.0-024-04 "Navigation Results from the Phoebe flyby",
+ J.B. Jones, 16 June 2004.
+
+ 17. Cassini NAV OD solution 040909R. Reconstruction from Jupiter to SOI.
+
+ 19. Cuzzi, J. N., J. J. Lissauer, L. W. Esposito, J. B. Holberg,
+ E. A. Marouf, G. L. Tyler, and A. Bouschot 1984. "Saturn's rings:
+ Properties and processes." In Planetary Rings, (R. Greenberg and
+ A. Brahic, Eds.), University of Arizona Press, Tucson, pp. 73-199.
+
+ 20. HST High-Resolution Backscatter Image of Saturn's G Ring
+ Jack J. Lissauer, Richard G. French Icarus, Vol. 146, No. 1,
+ Jul 2000, pp. 12-18.
+
+ 21. NASA/JPL Web page: "Natural Satellite Physical Parameters",
+ 2004 September 22 <http://ssd.jpl.nasa.gov/sat_props.html>
+
+ 22. Porco, C.C., Thomas, P.C., Weiss, J.W., Richardson, D.C. 2007.
+ Saturns Small Inner Satellites: Clues to Their Origins. Science 318, 1602.
+
+ Thomas, P.C., and 12 colleagues 2007. Shapes of the saturnian
+ icy satellites and their significance. Icarus 190, 573-584.
+
+ 23. Stiles, B. et als, "Determining Titan's Spin State from Cassini Radar
+ Images", Astronomical Journal, 135, 1669, May 2008.
+
+ 24. Archinal, B.A., et als (2010).
+ "Report of the IAU Working Group on Cartographic
+ Coordinates and Rotational Elements of the Planets and
+ Satellites: 2009"; Cassini ECR-100654
+
+ Unless noted otherwise, values are from the IAU report. [1]
+
diff --git a/tests/pytests/data/v1514284191_1/naif0012.tls b/tests/pytests/data/v1514284191_1/naif0012.tls
new file mode 100644
index 0000000..e1afdee
--- /dev/null
+++ b/tests/pytests/data/v1514284191_1/naif0012.tls
@@ -0,0 +1,152 @@
+KPL/LSK
+
+
+LEAPSECONDS KERNEL FILE
+===========================================================================
+
+Modifications:
+--------------
+
+2016, Jul. 14 NJB Modified file to account for the leapsecond that
+ will occur on December 31, 2016.
+
+2015, Jan. 5 NJB Modified file to account for the leapsecond that
+ will occur on June 30, 2015.
+
+2012, Jan. 5 NJB Modified file to account for the leapsecond that
+ will occur on June 30, 2012.
+
+2008, Jul. 7 NJB Modified file to account for the leapsecond that
+ will occur on December 31, 2008.
+
+2005, Aug. 3 NJB Modified file to account for the leapsecond that
+ will occur on December 31, 2005.
+
+1998, Jul 17 WLT Modified file to account for the leapsecond that
+ will occur on December 31, 1998.
+
+1997, Feb 22 WLT Modified file to account for the leapsecond that
+ will occur on June 30, 1997.
+
+1995, Dec 14 KSZ Corrected date of last leapsecond from 1-1-95
+ to 1-1-96.
+
+1995, Oct 25 WLT Modified file to account for the leapsecond that
+ will occur on Dec 31, 1995.
+
+1994, Jun 16 WLT Modified file to account for the leapsecond on
+ June 30, 1994.
+
+1993, Feb. 22 CHA Modified file to account for the leapsecond on
+ June 30, 1993.
+
+1992, Mar. 6 HAN Modified file to account for the leapsecond on
+ June 30, 1992.
+
+1990, Oct. 8 HAN Modified file to account for the leapsecond on
+ Dec. 31, 1990.
+
+
+Explanation:
+------------
+
+The contents of this file are used by the routine DELTET to compute the
+time difference
+
+[1] DELTA_ET = ET - UTC
+
+the increment to be applied to UTC to give ET.
+
+The difference between UTC and TAI,
+
+[2] DELTA_AT = TAI - UTC
+
+is always an integral number of seconds. The value of DELTA_AT was 10
+seconds in January 1972, and increases by one each time a leap second
+is declared. Combining [1] and [2] gives
+
+[3] DELTA_ET = ET - (TAI - DELTA_AT)
+
+ = (ET - TAI) + DELTA_AT
+
+The difference (ET - TAI) is periodic, and is given by
+
+[4] ET - TAI = DELTA_T_A + K sin E
+
+where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
+heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
+small-period fluctuations, is accurate to about 0.000030 seconds.
+
+The eccentric anomaly E is given by
+
+[5] E = M + EB sin M
+
+where M is the mean anomaly, which in turn is given by
+
+[6] M = M + M t
+ 0 1
+
+where t is the number of ephemeris seconds past J2000.
+
+Thus, in order to compute DELTA_ET, the following items are necessary.
+
+ DELTA_TA
+ K
+ EB
+ M0
+ M1
+ DELTA_AT after each leap second.
+
+The numbers, and the formulation, are taken from the following sources.
+
+ 1) Moyer, T.D., Transformation from Proper Time on Earth to
+ Coordinate Time in Solar System Barycentric Space-Time Frame
+ of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
+ 33-56 and 57-68.
+
+ 2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
+ Reference System on Algorithms for Computing Time Differences
+ and Clock Rates, JPL IOM 314.5--942, 1 October 1985.
+
+The variable names used above are consistent with those used in the
+Astronomical Almanac.
+
+\begindata
+
+DELTET/DELTA_T_A = 32.184
+DELTET/K = 1.657D-3
+DELTET/EB = 1.671D-2
+DELTET/M = ( 6.239996D0 1.99096871D-7 )
+
+DELTET/DELTA_AT = ( 10, @1972-JAN-1
+ 11, @1972-JUL-1
+ 12, @1973-JAN-1
+ 13, @1974-JAN-1
+ 14, @1975-JAN-1
+ 15, @1976-JAN-1
+ 16, @1977-JAN-1
+ 17, @1978-JAN-1
+ 18, @1979-JAN-1
+ 19, @1980-JAN-1
+ 20, @1981-JUL-1
+ 21, @1982-JUL-1
+ 22, @1983-JUL-1
+ 23, @1985-JUL-1
+ 24, @1988-JAN-1
+ 25, @1990-JAN-1
+ 26, @1991-JAN-1
+ 27, @1992-JUL-1
+ 28, @1993-JUL-1
+ 29, @1994-JUL-1
+ 30, @1996-JAN-1
+ 31, @1997-JUL-1
+ 32, @1999-JAN-1
+ 33, @2006-JAN-1
+ 34, @2009-JAN-1
+ 35, @2012-JUL-1
+ 36, @2015-JUL-1
+ 37, @2017-JAN-1 )
+
+\begintext
+
+
diff --git a/tests/pytests/data/v1514284191_1/pck00009.tpc b/tests/pytests/data/v1514284191_1/pck00009.tpc
new file mode 100644
index 0000000..bfadaab
--- /dev/null
+++ b/tests/pytests/data/v1514284191_1/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/v1514284191_1/v1514284191_1_vis_isis.lbl b/tests/pytests/data/v1514284191_1/v1514284191_1_vis_isis.lbl
new file mode 100644
index 0000000..0b35b57
--- /dev/null
+++ b/tests/pytests/data/v1514284191_1/v1514284191_1_vis_isis.lbl
@@ -0,0 +1,448 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 64
+ TileLines = 64
+
+ Group = Dimensions
+ Samples = 64
+ Lines = 64
+ Bands = 96
+ End_Group
+
+ Group = Pixels
+ Type = Real
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftName = Cassini-Huygens
+ InstrumentId = VIMS
+ TargetName = TITAN
+ SpacecraftClockStartCount = 1514284209.126
+ SpacecraftClockStopCount = 1514285336.126
+ StartTime = 2005-360T10:00:34.063
+ StopTime = 2005-360T10:19:19.470
+ NativeStartTime = 1514284191.13981
+ NativeStopTime = 1514285317.04523
+ InterlineDelayDuration = 671.000000
+ XOffset = 1
+ ZOffset = 1
+ SwathWidth = 64
+ SwathLength = 64
+ SamplingMode = NORMAL
+ Channel = VIS
+ ExposureDuration = (260.000000 <IR>, 10000.000000 <VIS>)
+ GainMode = LOW
+ End_Group
+
+ Group = Archive
+ MissionPhaseName = TOUR
+ SequenceId = S17
+ SequenceTitle = VIMS_019TI_MEDRES001_PRIME
+ ObservationId = VIMS_019TI_MEDRES001_PRIME
+ ProductId = 1_1514284191.13981
+ InstrumentModeId = IMAGE
+ CompressorId = 1
+ PowerStateFlag = (ON, ON)
+ SpectralSummingFlag = OFF
+ SpectralEditingFlag = OFF
+ StarTracking = OFF
+ SnapshotMode = ON
+ End_Group
+
+ Group = BandBin
+ OriginalBand = (1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17,
+ 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32,
+ 33, 34, 35, 36, 37, 38, 39, 40, 41, 42, 43, 44, 45, 46, 47,
+ 48, 49, 50, 51, 52, 53, 54, 55, 56, 57, 58, 59, 60, 61, 62,
+ 63, 64, 65, 66, 67, 68, 69, 70, 71, 72, 73, 74, 75, 76, 77,
+ 78, 79, 80, 81, 82, 83, 84, 85, 86, 87, 88, 89, 90, 91, 92,
+ 93, 94, 95, 96)
+ Center = (0.35054, 0.35895, 0.36629, 0.37322, 0.37949, 0.38790,
+ 0.39518, 0.40252, 0.40955, 0.41731, 0.42436, 0.43184,
+ 0.43919, 0.44652, 0.45372, 0.46163, 0.46841, 0.47622,
+ 0.48629, 0.48967, 0.49777, 0.50628, 0.51222, 0.51963,
+ 0.52766, 0.53416, 0.54156, 0.54954, 0.55614, 0.56353,
+ 0.57131, 0.57810, 0.58548, 0.59312, 0.59938, 0.60757,
+ 0.61505, 0.62207, 0.62940, 0.63704, 0.64408, 0.65142,
+ 0.65910, 0.66609, 0.67342, 0.68102, 0.68803, 0.69535,
+ 0.70288, 0.71000, 0.71733, 0.72484, 0.73198, 0.73930,
+ 0.74676, 0.75396, 0.76128, 0.76874, 0.77595, 0.78328,
+ 0.79072, 0.79793, 0.80522, 0.81262, 0.81989, 0.82721,
+ 0.83463, 0.84190, 0.84922, 0.85663, 0.86391, 0.87122,
+ 0.87863, 0.88589, 0.89386, 0.90032, 0.90787, 0.91518,
+ 0.92254, 0.92983, 0.93713, 0.94445, 0.95177, 0.95907,
+ 0.96638, 0.97382, 0.98100, 0.98883, 0.99588, 1.00295,
+ 1.01005, 1.01695, 1.02471, 1.03195, 1.03865, 1.04598)
+ End_Group
+
+ Group = Kernels
+ NaifFrameCode = -82370
+ LeapSecond = $base/kernels/lsk/naif0012.tls
+ TargetAttitudeShape = ($base/kernels/pck/pck00009.tpc,
+ $cassini/kernels/pck/cpck15Dec2017.tpc)
+ TargetPosition = (Table, $base/kernels/spk/de430.bsp,
+ $base/kernels/spk/sat425.bsp)
+ InstrumentPointing = (Table, $cassini/kernels/ck/05357_05362ra.bc,
+ $cassini/kernels/fk/cas_v40_usgs.tf)
+ Instrument = Null
+ SpacecraftClock = $cassini/kernels/sclk/cas00172.tsc
+ InstrumentPosition = (Table,
+ $cassini/kernels/spk/180628RU_SCPSE_05348_060-
+ 05.bsp)
+ InstrumentAddendum = $cassini/kernels/iak/vimsAddendum04.ti
+ ShapeModel = Null
+ InstrumentPositionQuality = Reconstructed
+ InstrumentPointingQuality = Reconstructed
+ CameraVersion = 1
+ Source = isis
+ End_Group
+End_Object
+
+Object = Label
+ Bytes = 65536
+End_Object
+
+Object = Table
+ Name = SideplaneVis
+ StartByte = 1638401
+ Bytes = 73728
+ Records = 6144
+ ByteOrder = Lsb
+ Association = Lines
+
+ Group = Field
+ Name = Line
+ Type = Integer
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = Band
+ Type = Integer
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = Value
+ Type = Integer
+ Size = 1
+ End_Group
+End_Object
+
+Object = Table
+ Name = SideplaneIr
+ StartByte = 1712129
+ Bytes = 196608
+ Records = 16384
+ ByteOrder = Lsb
+ Association = Lines
+
+ Group = Field
+ Name = Line
+ Type = Integer
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = Band
+ Type = Integer
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = Value
+ Type = Integer
+ Size = 1
+ End_Group
+End_Object
+
+Object = Table
+ Name = InstrumentPointing
+ StartByte = 1924341
+ Bytes = 10368
+ Records = 162
+ ByteOrder = Lsb
+ TimeDependentFrames = (-82000, 1)
+ ConstantFrames = (-82370, -82000)
+ ConstantRotation = (0.99991568332482, 0.0014510663863786,
+ -0.012904287946602, 0.012904407824453,
+ -7.32810212777781e-05, 0.99991673197751,
+ 0.0014499999195506, -0.99999894451756,
+ -9.19999948958952e-05)
+ CkTableStartTime = 188863301.78065
+ CkTableEndTime = 188863941.78065
+ CkTableOriginalSize = 65
+ FrameTypeCode = 3
+ Description = "Created by spiceinit"
+ Kernels = ($cassini/kernels/ck/05357_05362ra.bc,
+ $cassini/kernels/fk/cas_v40_usgs.tf)
+
+ Group = Field
+ Name = J2000Q0
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q1
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q2
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q3
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV1
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV2
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV3
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = ET
+ Type = Double
+ Size = 1
+ End_Group
+End_Object
+
+Object = Table
+ Name = InstrumentPosition
+ StartByte = 1934709
+ Bytes = 168
+ Records = 3
+ ByteOrder = Lsb
+ CacheType = HermiteSpline
+ SpkTableStartTime = 188863301.78065
+ SpkTableEndTime = 188863941.78065
+ SpkTableOriginalSize = 65.0
+ Description = "Created by spiceinit"
+ Kernels = $cassini/kernels/spk/180628RU_SCPSE_05348_06005.bsp
+
+ Group = Field
+ Name = J2000X
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Y
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Z
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000XV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000YV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000ZV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = ET
+ Type = Double
+ Size = 1
+ End_Group
+End_Object
+
+Object = Table
+ Name = BodyRotation
+ StartByte = 1934877
+ Bytes = 128
+ Records = 2
+ ByteOrder = Lsb
+ TimeDependentFrames = (10044, 1)
+ CkTableStartTime = 188863301.78065
+ CkTableEndTime = 188863941.78065
+ CkTableOriginalSize = 2
+ FrameTypeCode = 2
+ PoleRa = (39.4827, 0.0, 0.0)
+ PoleDec = (83.4279, 0.0, 0.0)
+ PrimeMeridian = (186.5855, 22.5769768, 0.0)
+ PoleRaNutPrec = (0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+ PoleDecNutPrec = (0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+ PmNutPrec = (0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
+ SysNutPrec0 = (353.32, 28.72, 177.4, 300.0, 316.45, 345.2, 29.8,
+ 706.64, 57.44)
+ SysNutPrec1 = (75706.7, 75706.7, -36505.5, -7225.9, 506.2, -1016.3,
+ -52.1, 151413.4, 151413.4)
+ Description = "Created by spiceinit"
+ Kernels = ($base/kernels/spk/de430.bsp,
+ $base/kernels/spk/sat425.bsp,
+ $base/kernels/pck/pck00009.tpc,
+ $cassini/kernels/pck/cpck15Dec2017.tpc)
+ SolarLongitude = 294.88589938614
+
+ Group = Field
+ Name = J2000Q0
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q1
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q2
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q3
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV1
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV2
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV3
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = ET
+ Type = Double
+ Size = 1
+ End_Group
+End_Object
+
+Object = Table
+ Name = SunPosition
+ StartByte = 1935005
+ Bytes = 112
+ Records = 2
+ ByteOrder = Lsb
+ CacheType = Linear
+ SpkTableStartTime = 188863301.78065
+ SpkTableEndTime = 188863941.78065
+ SpkTableOriginalSize = 2.0
+ Description = "Created by spiceinit"
+ Kernels = ($base/kernels/spk/de430.bsp,
+ $base/kernels/spk/sat425.bsp)
+
+ Group = Field
+ Name = J2000X
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Y
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Z
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000XV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000YV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000ZV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = ET
+ Type = Double
+ Size = 1
+ End_Group
+End_Object
+
+Object = History
+ Name = IsisCube
+ StartByte = 1935117
+ Bytes = 1365
+End_Object
+
+Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 1909203
+ Bytes = 15138
+End_Object
+
+Object = NaifKeywords
+ BODY_CODE = 606
+ BODY606_RADII = (2575.0, 2575.0, 2575.0)
+ BODY_FRAME_CODE = 10044
+ CLOCK_ET_-82_1514284191_COMPUTED = 98d4e182a683a641
+ CLOCK_ET_-82_1514285317_COMPUTED = d025de4eaf83a641
+ INS-82370_TRANSX = (0.0, 1.0, 0.0)
+ INS-82370_TRANSY = (0.0, 0.0, 1.0)
+ INS-82370_ITRANSS = (0.0, 1.0, 0.0)
+ INS-82370_ITRANSL = (0.0, 0.0, 1.0)
+End_Object
+End
diff --git a/tests/pytests/data/v1514284191_1/v1514284191_1_vis_isis_0.xsp b/tests/pytests/data/v1514284191_1/v1514284191_1_vis_isis_0.xsp
new file mode 100644
index 0000000..503fbf7
--- /dev/null
+++ b/tests/pytests/data/v1514284191_1/v1514284191_1_vis_isis_0.xsp
@@ -0,0 +1,401 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 27
+'MONTE Chebyshev Polynomial Table '
+'B41C118C550BA8^7'
+'B41C4899677A88^7'
+'6'
+'0'
+'1'
+'2'
+27
+'B3EA34^7'
+'1518^6'
+'-3040A73B3CEA0C^8'
+'-AEBA8A595EF4C^6'
+'4F63DAC1CAB528^4'
+'2CF4C4F849E9F^2'
+'-F00FFE4E356A^-1'
+'-42D8C8C502DB88^-3'
+'2CCC79649194C4^-5'
+'3B9648BB0D6252^8'
+'-732A0487DF917C^6'
+'-6204708C004C44^4'
+'2348D10CBBD2D4^2'
+'D5A18178C069C8^-1'
+'-5323E6D468751^-3'
+'1DCD1D25940EF^-5'
+'1AB05FC5DACB63^8'
+'-280BAB4FBD1828^6'
+'-2BE710132EA9A8^4'
+'CA3A8D3C568E8^1'
+'628E0CFDC9102C^-1'
+'-1F81CF99D5C144^-3'
+'A616D121ADD468^-6'
+'B298B4^7'
+'2A3^6'
+'17^2'
+'1^1'
+END_ARRAY 1 27
+BEGIN_ARRAY 2 39
+'MONTE Chebyshev Polynomial Table '
+'B41C118C550BA8^7'
+'B41C4899677A88^7'
+'A'
+'0'
+'1'
+'2'
+39
+'B492F4^7'
+'A8C^5'
+'8DA91266E68DF^5'
+'-C95686CD09671^3'
+'-150F936C3FF99E^2'
+'-1F9244441E5F92^0'
+'-67A96D5921FC1^-3'
+'84087694B9CCE^-3'
+'5F3B570C4D2D6^-4'
+'-AFAC21E3CF738^-5'
+'11F29B6007DB5F^-5'
+'-1757F092366F28^-6'
+'1571231A76CAFE^-7'
+'4B8C87F0A2184C^5'
+'1B0361B18A5EA2^4'
+'-599AA63F29502^1'
+'-FE03927149DF2^-1'
+'-B733773883ACC^-2'
+'-69E87E93FE22E4^-3'
+'B3574FC0C88C78^-4'
+'-619E802D836E4C^-5'
+'35F90BECBC546C^-6'
+'86443D0F98D418^-7'
+'-1363811BC0B872^-7'
+'1C139B22C7B972^5'
+'BB3626411D23A8^3'
+'-1D445915F8C0B3^1'
+'-63C84A0017578^-1'
+'-47D5CC743F87C4^-2'
+'-41723213AD193C^-3'
+'53688A86E05D^-4'
+'-225F0AF3DDE672^-5'
+'-6C042A94329AA^-8'
+'6D8D89BFF02A54^-7'
+'-D1A26009F4F02^-8'
+'B3EA34^7'
+'1518^6'
+'23^2'
+'1^1'
+END_ARRAY 2 39
+BEGIN_ARRAY 3 54
+'MONTE Chebyshev Polynomial Table '
+'B41C118C550BA8^7'
+'B41C4899677A88^7'
+'25E'
+'6'
+'1'
+'2'
+54
+'B42436^7'
+'2F76^5'
+'-FB8AD22F5D8358^5'
+'-CE83E60222B8C8^4'
+'342F95B08483A4^5'
+'9AFCB7BE4E7868^3'
+'-C04B1F0A1B8B8^3'
+'-2E56FF5D36FE^2'
+'814565AA3D^1'
+'70C57E26F4^0'
+'183FA78B4^0'
+'-73FCA455^-2'
+'247ACE6^-2'
+'1F5CDD72^-2'
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+ ~NAIF/SPC BEGIN COMMENTS~
+; ../sliced_kernels/v1514284191_1_vis_isis_0.bsp LOG FILE
+
+; Created 2022-08-15/16:53:01.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /Volumes/pkgs/isis3/isis_data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = ../sliced_kernels/v1514284191_1_vis_isis_0.bsp
+SOURCE_SPK_KERNEL = /Volumes/pkgs/isis3/isis_data/cassini/kernels/spk/180628RU_SCPSE_05348_06005.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 6, 10, -82, 606
+ BEGIN_TIME = 2005 DEC 26 08:43:04.587
+ END_TIME = 2005 DEC 26 08:57:45.404
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/v1514284191_1/v1514284191_1_vis_isis_1.xsp b/tests/pytests/data/v1514284191_1/v1514284191_1_vis_isis_1.xsp
new file mode 100644
index 0000000..ac24b07
--- /dev/null
+++ b/tests/pytests/data/v1514284191_1/v1514284191_1_vis_isis_1.xsp
@@ -0,0 +1,761 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
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+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'-293E915CBADBF4^-4'
+'285BDE1AF83318^-7'
+'-1C41BD65A7A87E^-A'
+'-DA3498E4A8EA2^-C'
+'6D1A2^-D'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'6^1'
+'5^1'
+'4^1'
+'4^1'
+'B41D4CC1E3C238^7'
+'22731BDB2E^2'
+'44E637B65C^2'
+'675953918A^2'
+'89CC6F6CB8^2'
+'AC3F8B47E6^2'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-105901CE29334A^6'
+'-624CDD7B26DA0C^1'
+'276B4BD3098042^5'
+'-32511ED95B8FE2^1'
+'146928D86C4AE^5'
+'C0C2D69DD2E66^0'
+'20ED2CBB6E5824^-3'
+'-3078C269B46AD4^-6'
+'4DE29B549908^-9'
+'-37B335E45220D^-B'
+'9D2EA5D83304A^-D'
+'-1054C^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'-4DD906A9CF128^-4'
+'1A13E53890E8DA^-6'
+'-4C6D54849C2E14^-9'
+'29937CFF09371^-B'
+'790EC^-C'
+'B24674^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'-293700D485115^-4'
+'285648AD5E6DE8^-7'
+'-1E55D0C655A33C^-A'
+'-6C2962E4A8EA2^-C'
+'C8DB^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'6^1'
+'5^1'
+'5^1'
+'4^1'
+'B41D53C1456AC^7'
+'26C17F5694^2'
+'4D82FEAD28^2'
+'6FF61A8856^2'
+'9269366384^2'
+'B4DC523EB2^2'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-105BB1790D4A7F^6'
+'-623E79244492B8^1'
+'275549D08A819E^5'
+'-32533E70313898^1'
+'146E6D760397A1^5'
+'C0B0D1EFE1FE8^0'
+'20E3564B77FB62^-3'
+'-36767D96F89248^-6'
+'61CD154572A0C4^-9'
+'-445A8157EFF6A8^-B'
+'-2A85AF366AAAE8^-D'
+'-11EF6^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'-4D8466D5DACF9^-4'
+'1D4559F3C734CB^-6'
+'-5FE62755C4B6FC^-9'
+'4A7613FADBAF68^-B'
+'36768EADA9A4^-D'
+'-236AB^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'-292ED0196259B4^-4'
+'2D5A80F567FD2^-7'
+'-245E38F859316A^-A'
+'BE9608C4C91988^-C'
+'-1DB2C^-D'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'6^1'
+'5^1'
+'5^1'
+'4^1'
+'B41D5FDDBD35D^7'
+'4D82FEAD28^2'
+'9B05FD5A5^2'
+'C1C77CB0E4^2'
+'E888FC0778^2'
+'10F4A7B5E0C^3'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-106056BCE2BB02^6'
+'-62259A8EF0BEF4^1'
+'272F3074CC0EF2^5'
+'-3256E5CF07A2D2^1'
+'14778A70AC7458^5'
+'C091AAEA33C7E8^0'
+'20D256F57218E8^-3'
+'-6CB667D7AA2BF4^-6'
+'182B75AE2D755D^-8'
+'-1E10E9D54DD842^-A'
+'-2406E211AF077^-C'
+'2901E^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'-4CF26552559A0C^-4'
+'3A553B729320EA^-6'
+'-17AC37AE514858^-8'
+'1FFBA7997DCFB4^-A'
+'-7D2C535314ABC4^-C'
+'-BC1844^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'-2920A5D769C49C^-4'
+'5AA1C3145EA4E8^-7'
+'-851E66D028ED18^-A'
+'50BB96DAE44E6^-B'
+'-36227E^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'6^1'
+'5^1'
+'5^1'
+'4^1'
+'B41D66397C1A^7'
+'21E94F6BC2^2'
+'43D29ED784^2'
+'65BBEE4346^2'
+'B33EECF06E^2'
+'100C1EB9D96^3'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1^1'
+'-1062C6A19B99EA^6'
+'-6218913FB1D2F8^1'
+'271B2ED6B69BF6^5'
+'-3258CE1DE6710E^1'
+'147C52AA1AA328^5'
+'C0815451B31468^0'
+'20C96E45D1ACBC^-3'
+'-2F7F151D25CCBA^-6'
+'49274A535D535C^-9'
+'-35161C6E1C0EEA^-B'
+'-47C5E06755138^-D'
+'1CAFA^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'-4CA5F9269819D8^-4'
+'1974E74FDA81F4^-6'
+'-47BACA4997A67^-9'
+'2C802E3ACFCD64^-B'
+'-7C789EE3376A^-E'
+'27C464^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'-2919375A1F770C^-4'
+'27A105F4A9784E^-7'
+'-19712A14DA9A2B^-A'
+'-27107535615A64^-C'
+'3D247C7CA85B9C^-C'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'6^1'
+'5^1'
+'5^1'
+'4^1'
+'B41D2EC5580F4^7'
+'B41D3869AA7DD8^7'
+'B41D3FD6B95008^7'
+'B41D464C4E892^7'
+'B41D4CC1E3C238^7'
+'B41D53C1456AC^7'
+'B41D5FDDBD35D^7'
+'B41D66397C1A^7'
+'8^1'
+END_ARRAY 4 577
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; ../sliced_kernels/v1514284191_1_vis_isis_1.bsp LOG FILE
+
+; Created 2022-08-15/16:53:06.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /Volumes/pkgs/isis3/isis_data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = ../sliced_kernels/v1514284191_1_vis_isis_1.bsp
+SOURCE_SPK_KERNEL = /Volumes/pkgs/isis3/isis_data/cassini/kernels/spk/180628RU_SCPSE_05348_06005.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 6, 10, -82, 606
+ BEGIN_TIME = 2005 DEC 26 09:58:51.749
+ END_TIME = 2005 DEC 26 10:13:31.749
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/v1514284191_1/vimsAddendum04.ti b/tests/pytests/data/v1514284191_1/vimsAddendum04.ti
new file mode 100644
index 0000000..d40d66a
--- /dev/null
+++ b/tests/pytests/data/v1514284191_1/vimsAddendum04.ti
@@ -0,0 +1,38 @@
+\begindata
+INS-82370_TRANSX = ( 0.0, 1.0, 0.0)
+INS-82370_TRANSY = ( 0.0, 0.0, 1.0)
+INS-82370_ITRANSS = ( 0.0, 1.0, 0.0)
+INS-82370_ITRANSL = ( 0.0, 0.0, 1.0)
+
+INS-82371_TRANSX = ( 0.0, 1.0, 0.0)
+INS-82371_TRANSY = ( 0.0, 0.0, 1.0)
+INS-82371_ITRANSS = ( 0.0, 1.0, 0.0)
+INS-82371_ITRANSL = ( 0.0, 0.0, 1.0)
+
+\begintext
+These are the parameters required for writing c-kernels. Isis will
+create ck with the same frame endpoints as the mission ck. For
+the Cassini spacecraft the ck frame is CASSINI_SC_COORD (-915240), and the
+ck reference frame is J2000 (1).
+
+\begindata
+INS-82371_CK_FRAME_ID=-915240
+INS-82371_CK_REFERENCE_ID=1
+INS-82370_CK_FRAME_ID=-915240
+INS-82370_CK_REFERENCE_ID=1
+
+\begintext
+The parallel arrays within the cassini vims ik kernels is not present within the
+ISIS kernel suite. There is also a problem within the cassini ik kernels where
+VIMS_IR has code (-82370) and VIMS_V has code (-82371). Then both of those frames
+are defined in again, where VIMS_IR is (-82371) and VIMS_V is (-82370). This is
+a discrepency within the kernels and until resolved we will be using the
+parallel array definition below.
+
+\begindata
+
+NAIF_BODY_NAME += ( 'CASSINI_VIMS_V' )
+NAIF_BODY_CODE += ( -82370 )
+
+NAIF_BODY_NAME += ( 'CASSINI_VIMS_IR' )
+NAIF_BODY_CODE += ( -82371 )
diff --git a/tests/pytests/test_cassini_drivers.py b/tests/pytests/test_cassini_drivers.py
index 79041a7..bfee670 100644
--- a/tests/pytests/test_cassini_drivers.py
+++ b/tests/pytests/test_cassini_drivers.py
@@ -1,30 +1,35 @@
import pytest
import ale
import os
-import pvl
-import numpy as np
-from ale.drivers import co_drivers
import unittest
from unittest.mock import PropertyMock, patch
import json
from conftest import get_image_label, get_image_kernels, get_isd, convert_kernels, compare_dicts, get_table_data
-from ale.drivers.co_drivers import CassiniIssPds3LabelNaifSpiceDriver, CassiniIssIsisLabelNaifSpiceDriver
+from ale.drivers.co_drivers import CassiniIssPds3LabelNaifSpiceDriver, CassiniIssIsisLabelNaifSpiceDriver, CassiniVimsIsisLabelNaifSpiceDriver
@pytest.fixture()
-def test_kernels(scope="module", autouse=True):
+def test_iss_kernels(scope="module", autouse=True):
kernels = get_image_kernels("N1702360370_1")
updated_kernels, binary_kernels = convert_kernels(kernels)
yield updated_kernels
for kern in binary_kernels:
os.remove(kern)
-def test_load_pds(test_kernels):
+@pytest.fixture()
+def test_vims_kernels(scope="module", autouse=True):
+ kernels = get_image_kernels("v1514284191_1")
+ updated_kernels, binary_kernels = convert_kernels(kernels)
+ yield updated_kernels
+ for kern in binary_kernels:
+ os.remove(kern)
+
+def test_load_pds(test_iss_kernels):
label_file = get_image_label("N1702360370_1")
compare_dict = get_isd("cassiniiss")
- isd_str = ale.loads(label_file, props={'kernels': test_kernels})
+ isd_str = ale.loads(label_file, props={'kernels': test_iss_kernels})
isd_obj = json.loads(isd_str)
print(json.dumps(isd_obj, indent=2))
assert compare_dicts(isd_obj, compare_dict) == []
@@ -43,18 +48,28 @@ def test_load_isis():
x = compare_dicts(isd_obj, compare_dict)
assert x == []
-def test_load_isis_naif(test_kernels):
+def test_load_iss_isis_naif(test_iss_kernels):
label_file = get_image_label("N1702360370_1")
compare_dict = get_isd("cassiniiss")
- isd_str = ale.loads(label_file, props={"kernels": test_kernels})
+ isd_str = ale.loads(label_file, props={"kernels": test_iss_kernels})
isd_obj = json.loads(isd_str)
print(json.dumps(isd_obj, indent=2))
x = compare_dicts(isd_obj, compare_dict)
assert x == []
-# ========= Test cassini pds3label and naifspice driver =========
-class test_cassini_pds3_naif(unittest.TestCase):
+def test_load_vims_isis_naif(test_vims_kernels):
+ label_file = get_image_label("v1514284191_1_vis", label_type="isis")
+ compare_dict = get_isd("cassinivims")
+
+ isd_str = ale.loads(label_file, props={"kernels": test_vims_kernels})
+ isd_obj = json.loads(isd_str)
+ print(json.dumps(isd_obj, indent=2))
+ x = compare_dicts(isd_obj, compare_dict)
+ assert x == []
+
+# ========= Test cassini ISS pds3label and naifspice driver =========
+class test_cassini_iss_pds3_naif(unittest.TestCase):
def setUp(self):
label = get_image_label("N1702360370_1", "pds3")
@@ -142,8 +157,8 @@ class test_cassini_pds3_naif(unittest.TestCase):
assert len(frame_chain.nodes()) == 0
from_spice.assert_called_with(center_ephemeris_time=2.4, ephemeris_times=[2.4], nadir=False, sensor_frame=14082360, target_frame=-800, exact_ck_times=True, inst_time_bias=0)
-# ========= Test cassini isislabel and naifspice driver =========
-class test_cassini_isis_naif(unittest.TestCase):
+# ========= Test cassini ISS isislabel and naifspice driver =========
+class test_cassini_iss_isis_naif(unittest.TestCase):
def setUp(self):
label = get_image_label("N1702360370_1", "isis3")
@@ -213,3 +228,51 @@ class test_cassini_isis_naif(unittest.TestCase):
frame_chain = self.driver.frame_chain
assert len(frame_chain.nodes()) == 0
from_spice.assert_called_with(center_ephemeris_time=2.4000000000000004, ephemeris_times=[2.4000000000000004], nadir=False, sensor_frame=14082360, target_frame=-800, exact_ck_times=True, inst_time_bias=0)
+
+# ========= Test cassini ISS pds3label and naifspice driver =========
+class test_cassini_vims_isis_naif(unittest.TestCase):
+
+ def setUp(self):
+ label = get_image_label("v1514284191_1_vis", "isis")
+ self.driver = CassiniVimsIsisLabelNaifSpiceDriver(label)
+
+ def test_vims_channel(self):
+ assert self.driver.vims_channel == "VIS"
+
+ def test_instrument_id(self):
+ assert self.driver.instrument_id == "CASSINI_VIMS_V"
+
+ def test_spacecraft_names(self):
+ assert self.driver.spacecraft_name == "Cassini"
+
+ def test_focal2pixel_lines(self):
+ assert self.driver.exposure_duration == 10.0
+
+ def test_focal_length(self):
+ assert self.driver.focal_length == 143.0
+
+ def test_detector_center_line(self):
+ assert self.driver.detector_center_line == 0
+
+ def test_detector_center_sample(self):
+ assert self.driver.detector_center_sample == 0
+
+ def test_compute_vims_time(self):
+ # This value isn't used for anything in the test, as it's only used for the
+ # default focal length calculation if the filter can't be found.
+ with patch('ale.drivers.co_drivers.spice.scs2e', return_value=12345) as scs2e:
+ assert self.driver.compute_vims_time(1, 1, self.driver.image_samples, "VIS")
+ scs2e.assert_called_with(-82, '1514284191')
+
+ def test_ephemeris_start_time(self):
+ with patch('ale.drivers.co_drivers.CassiniVimsIsisLabelNaifSpiceDriver.compute_vims_time', return_value=12345) as compute_vims_time:
+ assert self.driver.ephemeris_start_time == 12345
+ compute_vims_time.assert_called_with(-0.5, -0.5, 64, mode="VIS")
+
+ def test_ephemeris_stop_time(self):
+ with patch('ale.drivers.co_drivers.CassiniVimsIsisLabelNaifSpiceDriver.compute_vims_time', return_value=12345) as compute_vims_time:
+ assert self.driver.ephemeris_stop_time == 12345
+ compute_vims_time.assert_called_with(63.5, 63.5, 64, mode="VIS")
+
+ def test_sensor_model_version(self):
+ assert self.driver.sensor_model_version == 1
diff --git a/tests/pytests/test_util.py b/tests/pytests/test_util.py
index 50c0590..68733dc 100644
--- a/tests/pytests/test_util.py
+++ b/tests/pytests/test_util.py
@@ -164,7 +164,7 @@ def test_kernel_from_cube_list(cube_kernels):
def test_kernel_from_cube_list_expanded(monkeypatch, tmpdir, pvl_four_group, cube_kernels):
monkeypatch.setenv('ISISROOT', str(tmpdir))
- monkeypatch.setenv('ISIS3DATA', '/test/path')
+ monkeypatch.setenv('ISISDATA', '/test/path')
with open(tmpdir.join('IsisPreferences'), 'w+') as pvl_isisroot_file:
pvl_isisroot_file.write(pvl_four_group)
@@ -185,7 +185,7 @@ def test_kernel_from_cube_dict(cube_kernels):
def test_kernel_from_cube_dict_expanded(monkeypatch, tmpdir, pvl_four_group, cube_kernels):
monkeypatch.setenv('ISISROOT', str(tmpdir))
- monkeypatch.setenv('ISIS3DATA', '/test/path')
+ monkeypatch.setenv('ISISDATA', '/test/path')
with open(tmpdir.join('IsisPreferences'), 'w+') as pvl_isisroot_file:
pvl_isisroot_file.write(pvl_four_group)
--
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