diff --git a/ale/drivers/vo_drivers.py b/ale/drivers/vo_drivers.py
index 5a2505b4be7a1c22165c06924522b806d2dba3e9..4cb6bedcf5a121f680078b477158493b03c13112 100644
--- a/ale/drivers/vo_drivers.py
+++ b/ale/drivers/vo_drivers.py
@@ -6,7 +6,19 @@ from ale.base.label_isis import IsisLabel
from ale.base.type_sensor import Framer
from ale.base.base import Driver
-class Voyager2IssnacIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, Driver):
+class VoyagerCameraLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, Driver):
+
+ @property
+ def instrument_id(self):
+ sc_lookup = {
+ "VOYAGER_1" : "VG1",
+ "VOYAGER_2" : "VG2"
+ }
+ sensor_lookup = {
+ "NARROW_ANGLE_CAMERA" : "ISSNA",
+ "WIDE_ANGLE_CAMERA" : "ISSWA"
+ }
+ return sc_lookup[super().spacecraft_name] + '_' + sensor_lookup[super().instrument_id]
@property
def sensor_model_version(self):
@@ -44,4 +56,3 @@ class Voyager2IssnacIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, Drive
@property
def ephemeris_stop_time(self):
return self.ephemeris_start_time + self.exposure_duration
-
diff --git a/ale/rotation.py b/ale/rotation.py
index cba6f04b027dd3da544a7917ce4cf3c4b3804e88..62bc3855a56d75bf98606ef5e1086673f3732d15 100644
--- a/ale/rotation.py
+++ b/ale/rotation.py
@@ -217,12 +217,11 @@ class TimeDependentRotation:
Get the inverse rotation, that is the rotation from the destination
reference frame to the source reference frame.
"""
- new_rots = self._rots.inv()
if self.av is not None:
- new_av = -new_rots.apply(self.av)
+ new_av = -self._rots.apply(self.av)
else:
new_av = None
- return TimeDependentRotation(new_rots.as_quat(), self.times, self.dest, self.source, av=new_av)
+ return TimeDependentRotation(self._rots.inv().as_quat(), self.times, self.dest, self.source, av=new_av)
def _slerp(self, times):
"""
diff --git a/tests/pytests/data/c1637937/c1637937_0.xsp b/tests/pytests/data/c1637937/c1637937_0.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..56ab9149fef964b37e7fb2abe0e2992831d05e39
--- /dev/null
+++ b/tests/pytests/data/c1637937/c1637937_0.xsp
@@ -0,0 +1,283 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 39
+'DE-0431LE-0431 '
+'-272D39D79FA172^8'
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+'E^1'
+'E^1'
+'-272D1F442AEC7A^8'
+'1^1'
+END_ARRAY 4 73
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /work/users/jmapel/ale/voyager_images/kernels_1_nac/c1637937_0.bsp LOG FILE
+
+; Created 2019-09-19/12:36:09.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /work/users/jmapel/ale/voyager_images/kernels_1_nac/c1637937_0.bsp
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/spk/jup310.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 5, 10, 599
+ BEGIN_TIME = 1979 MAR 05 03:29:58.191
+ END_TIME = 1979 MAR 05 03:32:03.398
+SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/voyager1/kernels/spk//vgr1_jup230.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -31
+ BEGIN_TIME = 1979 MAR 05 03:29:58.191
+ END_TIME = 1979 MAR 05 03:32:03.398
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c1637937/c1637937_1.xsp b/tests/pytests/data/c1637937/c1637937_1.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..04cd371664e3ba7cf2e9d2fc2d9df1f4c05b63c2
--- /dev/null
+++ b/tests/pytests/data/c1637937/c1637937_1.xsp
@@ -0,0 +1,283 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 39
+'DE-0431LE-0431 '
+'-272D2F87E336EA^8'
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+'490EF1E6C28AC^-A'
+'19B480ED9EF8A^-A'
+'784586660AA418^-B'
+'1E9E0B062A3A98^-B'
+'5C5896DA4A22DC^-C'
+'-10A7C^-C'
+'F^1'
+'E^1'
+'E^1'
+'E^1'
+'-272D1F442AEC7A^8'
+'1^1'
+END_ARRAY 4 73
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /work/users/jmapel/ale/voyager_images/kernels_1_nac/c1637937_1.bsp LOG FILE
+
+; Created 2019-09-19/12:36:09.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /work/users/jmapel/ale/voyager_images/kernels_1_nac/c1637937_1.bsp
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/spk/jup310.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 5, 10, 599
+ BEGIN_TIME = 1979 MAR 05 04:13:57.927
+ END_TIME = 1979 MAR 05 04:15:57.927
+SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/voyager1/kernels/spk//vgr1_jup230.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -31
+ BEGIN_TIME = 1979 MAR 05 04:13:57.927
+ END_TIME = 1979 MAR 05 04:15:57.927
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c1637937/c1637937_isis3.lbl b/tests/pytests/data/c1637937/c1637937_isis3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..050af4be6cf4d3e2e7d82fbf259f41cfca83d349
--- /dev/null
+++ b/tests/pytests/data/c1637937/c1637937_isis3.lbl
@@ -0,0 +1,139 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 800
+ TileLines = 800
+
+ Group = Dimensions
+ Samples = 800
+ Lines = 800
+ Bands = 1
+ End_Group
+
+ Group = Pixels
+ Type = UnsignedByte
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftClockCount = 1637937
+ SpacecraftName = VOYAGER_1
+ TargetName = Jupiter
+ StartTime = 1979-03-05T04:14:59.927
+ InstrumentId = NARROW_ANGLE_CAMERA
+ ScanModeId = 1:1
+ ShutterModeId = BSIMAN
+ GainModeId = LOW
+ EditModeId = 1:1
+ ExposureDuration = 0.4800 <seconds>
+ CameraState1 = 1
+ CameraState2 = 0
+ End_Group
+
+ Group = Archive
+ MissionPhaseName = JUPITER_ENCOUNTER
+ ProductId = 1214J1-001
+ End_Group
+
+ Group = BandBin
+ FilterName = VIOLET
+ FilterNumber = 1
+ Center = 0.400000 <micrometers>
+ Width = 0.100000 <micrometers>
+ End_Group
+
+ Group = Kernels
+ NaifFrameCode = -31101
+ End_Group
+
+ Group = Reseaus
+ Line = (3.0, -1.0, 1.0, 0.0, -2.0, 1.0, 1.0, 1.0, 3.0, 6.0, 3.0, 16.0,
+ 14.0, 21.0, 20.0, 20.0, 20.0, 21.0, 22.0, 23.0, 25.0, 28.0,
+ 26.0, 50.6, 48.8, 48.0, 48.0, 49.0, 49.0, 50.0, 50.0, 52.0,
+ 54.0, 58.0, 61.5, 86.7, 86.0, 86.0, 87.0, 87.0, 88.0, 88.0,
+ 90.0, 91.0, 92.0, 96.0, 125.0, 125.0, 132.0, 133.7, 164.0,
+ 164.0, 165.0, 165.0, 166.0, 166.0, 166.0, 167.0, 168.0, 169.0,
+ 171.0, 203.0, 203.0, 209.0, 209.7, 243.0, 243.0, 244.0, 245.0,
+ 245.0, 246.0, 246.0, 246.0, 247.0, 247.0, 249.0, 281.9, 282.0,
+ 287.0, 287.5, 322.0, 323.0, 323.0, 324.0, 324.0, 324.0, 324.0,
+ 325.0, 326.0, 325.0, 328.0, 360.9, 362.0, 366.0, 366.0, 401.0,
+ 402.0, 403.0, 403.0, 403.0, 404.0, 404.0, 404.0, 405.0, 405.0,
+ 406.0, 439.6, 441.0, 445.0, 443.8, 480.0, 481.0, 482.0, 482.0,
+ 482.0, 483.0, 483.0, 483.0, 483.0, 483.0, 485.0, 517.8, 520.0,
+ 524.0, 522.8, 559.0, 560.0, 560.0, 561.0, 561.0, 562.0, 562.0,
+ 562.0, 562.0, 563.0, 563.0, 596.0, 598.0, 603.0, 600.6, 635.0,
+ 637.0, 638.0, 639.0, 639.0, 640.0, 640.0, 640.0, 641.0, 641.0,
+ 642.0, 672.0, 674.0, 680.0, 680.0, 710.0, 713.0, 715.0, 716.0,
+ 716.0, 717.0, 717.0, 718.0, 718.0, 718.0, 718.0, 744.0, 747.0,
+ 751.0, 753.0, 754.0, 754.0, 756.0, 756.0, 756.0, 756.0, 756.0,
+ 754.0, 780.0, 776.0, 779.0, 781.0, 783.0, 783.0, 784.0, 784.0,
+ 784.0, 783.0, 791.0, 789.0, 800.0, 798.0, 800.0, 800.5, 801.8,
+ 802.1, 802.7, 803.5, 801.8, 803.8, 800.0, 129.0)
+ Sample = (12.0, 50.5, 126.0, 204.2, 281.0, 361.0, 440.0, 518.0, 596.0,
+ 674.0, 750.0, 796.0, 22.0, 92.0, 168.0, 245.0, 323.0, 402.0,
+ 481.0, 559.0, 637.0, 714.0, 787.0, 4.7, 54.0, 129.0, 206.0,
+ 283.0, 362.0, 441.0, 520.0, 598.0, 676.0, 752.0, 799.7, 25.6,
+ 90.0, 166.0, 244.0, 322.0, 401.0, 480.0, 559.0, 637.0, 715.0,
+ 780.0, 5.0, 52.0, 752.0, 799.3, 24.0, 89.0, 166.0, 244.0,
+ 322.0, 401.0, 480.0, 558.0, 637.0, 715.0, 781.0, 2.0, 51.0,
+ 753.0, 799.8, 22.0, 88.0, 165.0, 244.0, 322.0, 401.0, 480.0,
+ 559.0, 638.0, 715.0, 782.0, 0.0, 50.0, 754.0, 801.0, 22.0,
+ 88.0, 165.0, 244.0, 322.0, 401.0, 480.0, 559.0, 637.0, 716.0,
+ 782.0, 0.0, 50.0, 753.0, 802.0, 22.0, 89.0, 166.0, 245.0,
+ 324.0, 403.0, 481.0, 560.0, 639.0, 716.0, 782.0, 0.0, 50.0,
+ 754.0, 801.8, 22.0, 88.0, 167.0, 245.0, 324.0, 403.0, 482.0,
+ 560.0, 639.0, 716.0, 782.0, 0.0, 51.0, 754.0, 801.0, 23.0,
+ 89.0, 167.0, 246.0, 325.0, 404.0, 482.0, 561.0, 639.0, 716.0,
+ 782.0, 2.0, 51.0, 754.0, 799.8, 24.0, 90.0, 168.0, 247.0,
+ 326.0, 404.0, 483.0, 561.0, 639.0, 716.0, 781.0, 4.0, 53.0,
+ 753.0, 800.0, 25.0, 91.0, 168.0, 247.0, 326.0, 405.0, 483.0,
+ 562.0, 639.0, 715.0, 779.0, 1.0, 54.0, 130.0, 208.0, 287.0,
+ 365.0, 444.0, 522.0, 600.0, 676.0, 751.0, 800.0, 20.0, 93.0,
+ 169.0, 247.0, 326.0, 404.0, 483.0, 561.0, 637.0, 713.0, 784.0,
+ 10.0, 56.0, 131.0, 209.0, 284.2, 363.1, 441.5, 519.7, 597.0,
+ 673.2, 746.2, 793.0, 597.0)
+ Type = (5, 0, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 0, 0, 0, 0, 0, 0, 0, 5, 5)
+ Valid = (0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0)
+ Template = $voyager1/reseaus/vg1.issna.template.cub
+ Status = Nominal
+ End_Group
+End_Object
+
+Object = Label
+ Bytes = 65536
+End_Object
+
+Object = History
+ Name = IsisCube
+ StartByte = 705537
+ Bytes = 444
+End_Object
+
+Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 705981
+ Bytes = 1995
+End_Object
+End
diff --git a/tests/pytests/data/c1637937/naif0012.tls b/tests/pytests/data/c1637937/naif0012.tls
new file mode 100644
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/c1637937/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/c1637937/pck00009.tpc b/tests/pytests/data/c1637937/pck00009.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..bfadaab2b26817327189ff3173e9609f49dedc9d
--- /dev/null
+++ b/tests/pytests/data/c1637937/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/c1637937/vg100010.tsc b/tests/pytests/data/c1637937/vg100010.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..78975fabf9470ad28dee3232360ef671a66f9ebe
--- /dev/null
+++ b/tests/pytests/data/c1637937/vg100010.tsc
@@ -0,0 +1,1108 @@
+
+KPL/SCLK
+
+
+\beginlabel
+
+MISSION_NAME = VOYAGER
+SPACECRAFT_NAME = VG1
+SPICE_DATA_TYPE = SCLK
+DATA_SET_ID = "VG1-X-SPICE-6-SCLK-V2.0"
+FILE_NAME = "VG100010.TSC"
+PRODUCT_ID = "VG100010.TSC"
+SOURCE_PRODUCT_ID = { "SCLK_SCET.31 version A061115,
+dated 2006-11-15T14:06:22", "SCLK_SCET.31 version A051104,
+dated 2005-11-04T14:46:04", "SCLK_SCET.31 version A991116,
+dated 1999-11-16T16:34:17", "SDT*FDSCSCEA., DATED 1999-08-27T14:40:04"}
+SOFTWARE_NAME = "MAKVSK, by Nat Bachman of NAIF"
+PRODUCT_CREATION _TIME = 2007-01-19T04:30:00
+PRODUCER_ID = NAIF, N. Bachman
+MISSION_PHASE_TYPE = {"CRUISE","ENCOUNTER","EXTENDED MISION"}
+MISSION_PHASE_NAME = {"CRUISE","JUPITER ENCOUNTER","SATURN
+ENCOUNTER","EXTENDED MISSION"}
+PRODUCT_VERSION_TYPE = RECONSTRUCTION
+START_TIME = 1977-09-05T14:09:24
+STOP_TIME = 2006-11-14T22:08:55
+SPACECRAFT_CLOCK_START_COUNT = "1/00012:00:001"
+SPACECRAFT_CLOCK_STOP_COUNT = "7/09650:00:001"
+NOTE = "CALIBRATED DATA COVERS FROM LAUNCH TO 2006-NOV-14 (2006//318).
+BUT THE FILE MAY BE USED IN PREDICT MODE THROUGH 2059-OCT-27
+(SCLK =15/65535:59:800). Records for partitions 1-4 were derived from the
+SCLKvSCET file dated 1999-08-27T14:40:04. Records for partition 5 start
+at UTC epoch 1994-01-11T04:33:25. These records were derived from the
+SCLKvSCET file having version ID A991116. Records for partition 6 start at
+UTC epoch 2000-01-004T17:21:06. These records were derived from the SCLKvSCET
+file having version ID A051104. Records for partition 7 start at UTC epoch
+2005-12-28T06:08:58. These records were derived from the SCLKvSCET file
+having version ID A061115. The portion of partition 7 that follows the
+stop time cited above, and partitions 8-15, constitute the predict region."
+
+\endlabel
+
+
+
+Voyager 1 SPICE SCLK Kernel
+--------------------------------------------------------
+
+ This file contains the data necessary to convert between Voyager 1
+ spacecraft clock time (SCLK) and ephemeris time.
+
+ NAIF suggests that you do not modify this file. If you do modify it,
+ be sure to indicate this in the `Version' section below.
+
+
+Version
+--------------------------------------------------------
+
+ This file is VG1 version 00010, produced January 19, 2007 by NAIF
+ (N. Bachman).
+
+ See label above for source file identification.
+
+Implementation notes
+--------------------------------------------------------
+
+ Older versions of this SCLK kernel contained code examples showing
+ calls to LDPOOL. NAIF now recommends using the more capable
+ routine FURNSH as the kernel loading interface. LDPOOL will
+ continue to be supported: existing SPICE-based applications that
+ load kernels using LDPOOL will continue to work as before when
+ linked against current (N0050 or greater) versions of SPICELIB or
+ CSPICE.
+
+ You must load this file into the kernel pool before using any of the
+ SPICELIB or CSPICE SCLK routines. The Fortran or C code fragments
+
+ CALL FURNSH ( name of this SCLK kernel ) {Fortran}
+
+ furnsh_c ( name of this SCLK kernel ); {C}
+
+ perform this task. To convert between ET and UTC, you will also need
+ to load a leapseconds kernel. The additional call to FURNSH,
+
+ CALL FURNSH ( name of your leapsecond file )
+
+ furnsh_c ( name of your leapsecond file );
+
+ You may find it more convenient to create a setup kernel and list the
+ names of these kernels in it. For example, we could call the setup
+ file setup.ker. This file would contain the kernel variable
+ assignment:
+
+ \begindata [The \begindata token starts a data section; it must
+ appear alone on a line to be recognized. This comment
+ is not part of the setup file's contents.]
+
+ KERNELS_TO_LOAD = ( 'name of SCLK kernel',
+ 'name of leapseconds kernel' )
+
+ The file names are delimited by single quotes regardless of whether
+ you're using the Fortran or C SPICE Toolkit.
+
+ You would load the kernels by supplying the name of your setup
+ file to FURNSH:
+
+ CALL FURNSH ( 'setup.ker' )
+
+ furnsh_c ( "setup.ker" );
+
+ You may list all of the SPICE kernels needed by your program in your
+ setup file. This one call to FURNSH may then replace all calls to LDPOOL
+ or other kernel loaders.
+
+ You must supply the actual names of the kernel files used on your system
+ as arguments to FURNSH or as values specified as "kernels to load" in
+ your FURNSH setup file. Because the file names are application
+ dependent, we do not list them here.
+
+ For more information on using SCLK within the SPICE system, consult your
+ SPICELIB required reading files. The following documents are pertinent:
+
+ SCLK system SCLK required reading
+ Time systems and conversion TIME required reading
+ FURNSH and kernel loading KERNEL required reading
+
+
+
+
+\begindata
+
+SCLK_KERNEL_ID = ( @19-JAN-2007/04:30 )
+
+SCLK_DATA_TYPE_31 = ( 1 )
+SCLK01_N_FIELDS_31 = ( 3 )
+SCLK01_MODULI_31 = ( 65536 60 800 )
+SCLK01_OFFSETS_31 = ( 0 0 1 )
+SCLK01_OUTPUT_DELIM_31 = ( 2 )
+
+SCLK_PARTITION_START_31 = ( 5.7600000000000E+05
+ 1.6964640000000E+08
+ 0.0000000000000E+00
+ 2.4800000000000E+04
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00 )
+
+SCLK_PARTITION_END_31 = ( 1.6964638300000E+08
+ 3.1457280010000E+09
+ 2.3082488000000E+09
+ 3.1457280000000E+09
+ 3.1457280020000E+09
+ 3.1457280010000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09 )
+
+SCLK01_COEFFICIENTS_31 = (
+
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+ 15353279987.000 2.1678540063173E+08 2.8799845200000E+03
+ 15353759987.000 2.1681420047773E+08 2.8799997600000E+03 )
+
+\begintext
diff --git a/tests/pytests/data/c1637937/vg1_issna_v02.ti b/tests/pytests/data/c1637937/vg1_issna_v02.ti
new file mode 100644
index 0000000000000000000000000000000000000000..13d63f5cad13246b9bb266dde5e828e4022fedbc
--- /dev/null
+++ b/tests/pytests/data/c1637937/vg1_issna_v02.ti
@@ -0,0 +1,50 @@
+KPL/IK
+
+Voyager 1 Imaging Subsytem Narrow Angle camera (ISSNA)
+----------------------------------------------------------------
+
+ Version 2 by Jeff Bytof -- 27 November 2000.
+
+ Changed shape from POLYGON to RECTANGLE.
+
+
+ Version 1.0 by Jeff Bytof, NAIF/JPL, 31 March 2000.
+
+ Provide the corner vector directions of the ISSNA
+ field of view.
+
+\begintext
+
+ Field of view description
+ -------------------------
+
+ - FOV is square with its sides along X and Y
+ axes of the instrument's frame;
+
+ - full FOV angular size in X and Y directions is 0.424 degrees;
+
+ - boresight vector intersects FOV exactly in the center of
+ the square;
+
+
+\begindata
+
+
+ INS-31101_FOV_FRAME = 'VG1_ISSNA'
+
+ INS-31101_FOV_SHAPE = 'RECTANGLE'
+
+ INS-31101_BORESIGHT = ( 0.0 0.0 1.0 )
+
+
+ INS-31101_FOV_BOUNDARY_CORNERS = (
+
+ .003700098 .003700098 1.0
+ -.003700098 .003700098 1.0
+ -.003700098 -.003700098 1.0
+ .003700098 -.003700098 1.0
+
+ )
+
+\begintext
+
diff --git a/tests/pytests/data/c1637937/vg1_jup_qmw_na_fc-31100_t2_0_sliced_-31100.xc b/tests/pytests/data/c1637937/vg1_jup_qmw_na_fc-31100_t2_0_sliced_-31100.xc
new file mode 100644
index 0000000000000000000000000000000000000000..80b5368a1ee328a378250ef72541c2edd22f17c8
--- /dev/null
+++ b/tests/pytests/data/c1637937/vg1_jup_qmw_na_fc-31100_t2_0_sliced_-31100.xc
@@ -0,0 +1,41 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+' '
+BEGIN_ARRAY 1 20
+'VG1 JUP SEDR QMW IMAGE NAV POINTING: NA '
+'2ED3502A^8'
+'2ED35851^8'
+'-797C'
+'2'
+'2'
+'1'
+20
+'B78954E4F6A0A^0'
+'68D3EF47349FC4^0'
+'806ED2ADE0D728^0'
+'-42144F2B86B9C8^0'
+'0^0'
+'0^0'
+'0^0'
+'1^1'
+'B7829A567F79F8^0'
+'68D763CF7A70C8^0'
+'806FE1B4A83DF^0'
+'-421F743ACF976^0'
+'0^0'
+'0^0'
+'0^0'
+'1^1'
+'2ED3502A^8'
+'2ED3559E^8'
+'2ED3527E^8'
+'2ED35851^8'
+END_ARRAY 1 20
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /work/users/jmapel/ale/voyager_images/c1637937.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c1637937/vg1_jup_qmw_na_fc-31100_t2_1_sliced_-31100.xc b/tests/pytests/data/c1637937/vg1_jup_qmw_na_fc-31100_t2_1_sliced_-31100.xc
new file mode 100644
index 0000000000000000000000000000000000000000..e0b536c4944a5ef2a1b8629ac0e8f88491e0ebf3
--- /dev/null
+++ b/tests/pytests/data/c1637937/vg1_jup_qmw_na_fc-31100_t2_1_sliced_-31100.xc
@@ -0,0 +1,31 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+' '
+BEGIN_ARRAY 1 10
+'VG1 JUP SEDR QMW IMAGE NAV POINTING: NA '
+'2ED3FC06^8'
+'2ED403D6^8'
+'-797C'
+'2'
+'2'
+'1'
+10
+'B9101C46365348^0'
+'69A6A42953B344^0'
+'7F53745A1D4914^0'
+'-3E8F3621691CE2^0'
+'0^0'
+'0^0'
+'0^0'
+'1^1'
+'2ED3FE5E^8'
+'2ED4017E^8'
+END_ARRAY 1 10
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /work/users/jmapel/ale/voyager_images/c1637937.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c1637937/vg1_v02.tf b/tests/pytests/data/c1637937/vg1_v02.tf
new file mode 100644
index 0000000000000000000000000000000000000000..2b2b6ffaf80b4c2f88be245d98e27e737837aa56
--- /dev/null
+++ b/tests/pytests/data/c1637937/vg1_v02.tf
@@ -0,0 +1,331 @@
+KPL/FK
+
+Voyager-1 Frame Kernel
+===========================================================================
+
+ This file contains various frame definitions for Voyager-1, related
+ to the spacecraft body and the scan platform.
+
+
+Version and Date
+--------------------------------------------------------
+
+ Version 2.0 -- 27 November 2000 -- Jeff Bytof
+
+ Changed instrument base frame to VG1_SCAN_PLATFORM.
+
+
+ Version 1.1 -- 8 March 2000 -- Jeff Bytof
+
+ Added the spacecraft high-gain antenna frame, FRAME_VG1_HGA.
+
+ Added -100 to all scan platform instrument ID codes, to
+ associate them to the scan platform ID code of -31100.
+
+
+ Version 1.0 -- 4 November 1999 -- Jeff Bytof
+
+ Initial Release.
+
+
+References
+--------------------------------------------------------
+
+ (1) Frames Required Reading (NAIF document).
+
+ (2) C Kernel Required Reading (NAIF document).
+
+
+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. Loading the kernel associates data items with
+ their names in a data structure called the `kernel pool'. The SPICELIB
+ routine LDPOOL loads a kernel file into the pool as shown below.
+
+
+ CALL LDPOOL ( kernel_name )
+
+
+ In order for a program or subroutine to extract data from the pool,
+ the SPICELIB routines GDPOOL and GIPOOL are used. See [3] for more
+ details.
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+Naming Conventions
+--------------------------------------------------------
+
+ All names referencing values in this frame kernel start with the
+ characters `FRAME', 'CK' or `TKFRAME' followed by the Voyager-1
+ spacecraft bus ID number (-31000) added to the instrument or
+ alternate frame index number.
+
+ The remainder of the name is an underscore character followed by the
+ unique name of the data item. For example, the Voyager-1 cone/clock
+ offsets relative to the spacecraft frame, given as three Euler angles,
+ are specified using two items:
+
+ TKFRAME_-31200_ANGLES = ( 55.0, 0.0, 180.0 )
+ TKFRAME_-31200_AXES = ( 3, 2, 1 )
+
+ The upper bound on the length of the name of any data item is 32
+ characters.
+
+ If the same item is included in more then one file, or if the same
+ item appears more than once within a single file, the latest value
+ supersedes any earlier values.
+
+
+TKFRAME Keyword Description
+--------------------------------------------------------
+
+ This section describes the TKFRAME keywords. The rotational offsets
+ can be given as three angles -- ROLL, PITCH and YAW, from which
+ a rotation matrix can be constructed that will transform the components of
+ a vector expressed in the spacecraft frame to components expressed in
+ the antenna fixed frame. For example, if x, y and z are the components of
+ a vector expressed in the spacecraft frame, X, Y and Z will be the components
+ of the same vector expressed in the antenna fixed frame:
+
+
+ [ X ] [ ] [ x ]
+ | Y | = | ROT | | y |
+ [ Z ] [ ] [ z ]
+
+
+ where ROT is the rotation matrix constructed from the rotation angles
+ as follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ YAW ] [ PITCH ] [ ROLL ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where each of three matrixes on the right side represent a coordinate
+ frame rotation by the given angle around the indicated axis. See the
+ SPICELIB routine EUL2M for more information about constructing
+ a rotation matrix from a set of rotation angles.
+
+ Following are some examples of use of the TKFRAME keywords:
+
+ The keyword that indicates which frame the axis rotations are
+ referred to is:
+
+ TKFRAME_-31200_RELATIVE = 'VG1_SC_BUS'
+
+
+ The keyword TKFRAME_-91000_ANGLES contain these values, in radians,
+ in the following order:
+
+ ``ROLL'' ``PITCH'' ``YAW''
+ TKFRAME_-31200_ANGLES = ( 55.0, 0.0, 180.0 )
+
+
+ The keyword TKFRAME_-31200_AXES contains integer codes of the
+ corresponding axes of rotations (1 -- X, 2 -- Y, 3 -- Z).
+
+ TKFRAME_-31200_AXES = ( 3, 2, 1 )
+
+
+ The keyword TKFRAME_-31200_UNITS gives the units of the angles.
+
+ TKFRAME_-31202_UNITS = 'DEGREES'
+
+
+
+
+
+Spacecraft Bus
+--------------------------------------------------------
+
+ The following data represents the basic spacecraft bus, and
+ the scan platform. Spacecraft bus attitude with respect to an inertial
+ frame is provided by a C kernel (see [2] for more information).
+ Scan platform orientation with respect to an inertial frame
+ is also provided by a C-kernel. Each instrument mounted
+ on the scan platform may have measureable offsets from the
+ nominal scan platform orientation. The Narrow Angle camera
+ has been chosen as representative of the scan platform orientation.
+
+\begindata
+
+ FRAME_VG1_SC_BUS = -31000
+ FRAME_-31000_NAME = 'VG1_SC_BUS'
+ FRAME_-31000_CLASS = 3
+ FRAME_-31000_CLASS_ID = -31000
+ FRAME_-31000_CENTER = -31
+ CK_-31000_SCLK = -31
+ CK_-31000_SPK = -31
+
+ FRAME_VG1_SCAN_PLATFORM = -31100
+ FRAME_-31100_NAME = 'VG1_SCAN_PLATFORM'
+ FRAME_-31100_CLASS = 3
+ FRAME_-31100_CLASS_ID = -31100
+ FRAME_-31100_CENTER = -31
+ CK_-31100_SCLK = -31
+ CK_-31100_SPK = -31
+
+\begintext
+
+
+Frame Definitions
+--------------------------------------------------------
+
+ Here are the frame definitions for Voyager 1. These are
+ utilized by SPICE's FRAMES subsystem to provide automatic state
+ transformations to/from the various frames. Note that SPICE toolkit
+ version N0047 or higher is required to use fixed-offset frames.
+
+ Note that angles in the frame definitions are specified for the "from
+ instrument to base (relative to) frame" transformation.
+
+
+ Spacecraft body-fixed reference frames:
+
+
+\begindata
+
+ FRAME_VG1_CONE_CLOCK = -31200
+ FRAME_-31200_NAME = 'VG1_CONE_CLOCK'
+ FRAME_-31200_CLASS = 4
+ FRAME_-31200_CLASS_ID = -31200
+ FRAME_-31200_CENTER = -31
+ TKFRAME_-31200_SPEC = 'ANGLES'
+ TKFRAME_-31200_RELATIVE = 'VG1_SC_BUS'
+ TKFRAME_-31200_ANGLES = ( 55.0, 0.0, 180.0 )
+ TKFRAME_-31200_AXES = ( 3, 2, 1 )
+ TKFRAME_-31200_UNITS = 'DEGREES'
+
+ FRAME_VG1_AZ_EL = -31300
+ FRAME_-31300_NAME = 'VG1_AZ_EL'
+ FRAME_-31300_CLASS = 4
+ FRAME_-31300_CLASS_ID = -31300
+ FRAME_-31300_CENTER = -31
+ TKFRAME_-31300_SPEC = 'ANGLES'
+ TKFRAME_-31300_RELATIVE = 'VG1_SC_BUS'
+ TKFRAME_-31300_ANGLES = ( -173.0, 0.0, 180.0 )
+ TKFRAME_-31300_AXES = ( 1, 2, 3 )
+ TKFRAME_-31300_UNITS = 'DEGREES'
+
+\begintext
+
+ The boresight of the antenna is the +Z axis.
+
+\begindata
+
+ FRAME_VG1_HGA = -31400
+ FRAME_-31400_NAME = 'VG1_HGA'
+ FRAME_-31400_CLASS = 4
+ FRAME_-31400_CLASS_ID = -31400
+ FRAME_-31400_CENTER = -31
+ TKFRAME_-31400_SPEC = 'ANGLES'
+ TKFRAME_-31400_RELATIVE = 'VG1_SC_BUS'
+ TKFRAME_-31400_ANGLES = ( 180.0, 0.0, 0.0 )
+ TKFRAME_-31400_AXES = ( 1, 2, 3 )
+ TKFRAME_-31400_UNITS = 'DEGREES'
+
+\begintext
+
+ Voyager-1 scan platform instrument frame definitions.
+
+ The Euler angles of rotation given below are
+ referred to the ISSNA frame of reference which
+ in this case is considered the equivalent of the
+ scan platform's frame.
+
+ Boresights are +Z in each instrument frame.
+
+
+\begindata
+
+
+ FRAME_VG1_ISSNA = -31101
+ FRAME_-31101_NAME = 'VG1_ISSNA'
+ FRAME_-31101_CLASS = 4
+ FRAME_-31101_CLASS_ID = -31101
+ FRAME_-31101_CENTER = -31
+ TKFRAME_-31101_SPEC = 'ANGLES'
+ TKFRAME_-31101_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31101_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-31101_AXES = ( 1, 2, 3 )
+ TKFRAME_-31101_UNITS = 'DEGREES'
+
+
+ FRAME_VG1_ISSWA = -31102
+ FRAME_-31102_NAME = 'VG1_ISSWA'
+ FRAME_-31102_CLASS = 4
+ FRAME_-31102_CLASS_ID = -31102
+ FRAME_-31102_CENTER = -31
+ TKFRAME_-31102_SPEC = 'ANGLES'
+ TKFRAME_-31102_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31102_ANGLES = ( 0.275, -0.0247, 0.0315 )
+ TKFRAME_-31102_AXES = ( 3, 1, 2 )
+ TKFRAME_-31102_UNITS = 'DEGREES'
+
+
+ FRAME_VG1_PPS = -31103
+ FRAME_-31103_NAME = 'VG1_PPS'
+ FRAME_-31103_CLASS = 4
+ FRAME_-31103_CLASS_ID = -31103
+ FRAME_-31103_CENTER = -31
+ TKFRAME_-31103_SPEC = 'ANGLES'
+ TKFRAME_-31103_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31103_ANGLES = ( 0.0, 0.0, -0.034 )
+ TKFRAME_-31103_AXES = ( 3, 1, 2 )
+ TKFRAME_-31103_UNITS = 'DEGREES'
+
+
+ FRAME_VG1_UVS = -31104
+ FRAME_-31104_NAME = 'VG1_UVS'
+ FRAME_-31104_CLASS = 4
+ FRAME_-31104_CLASS_ID = -31104
+ FRAME_-31104_CENTER = -31
+ TKFRAME_-31104_SPEC = 'ANGLES'
+ TKFRAME_-31104_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31104_ANGLES = ( 0.0, 0.030, 0.010 )
+ TKFRAME_-31104_AXES = ( 3, 1, 2 )
+ TKFRAME_-31104_UNITS = 'DEGREES'
+
+
+ FRAME_VG1_UVSOCC = -31105
+ FRAME_-31105_NAME = 'VG1_UVSOCC'
+ FRAME_-31105_CLASS = 4
+ FRAME_-31105_CLASS_ID = -31105
+ FRAME_-31105_CENTER = -31
+ TKFRAME_-31105_SPEC = 'ANGLES'
+ TKFRAME_-31105_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31105_ANGLES = ( 0.0, -0.00368, -19.5 )
+ TKFRAME_-31105_AXES = ( 3, 1, 2 )
+ TKFRAME_-31105_UNITS = 'DEGREES'
+
+
+ FRAME_VG1_IRIS = -31106
+ FRAME_-31106_NAME = 'VG1_IRIS'
+ FRAME_-31106_CLASS = 4
+ FRAME_-31106_CLASS_ID = -31106
+ FRAME_-31106_CENTER = -31
+ TKFRAME_-31106_SPEC = 'ANGLES'
+ TKFRAME_-31106_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31106_ANGLES = ( 0.0, -0.020, 0.024 )
+ TKFRAME_-31106_AXES = ( 3, 1, 2 )
+ TKFRAME_-31106_UNITS = 'DEGREES'
+
+
+ FRAME_VG1_IRISOCC = -31107
+ FRAME_-31107_NAME = 'VG1_IRISOCC'
+ FRAME_-31107_CLASS = 4
+ FRAME_-31107_CLASS_ID = -31107
+ FRAME_-31107_CENTER = -31
+ TKFRAME_-31107_SPEC = 'ANGLES'
+ TKFRAME_-31107_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31107_ANGLES = ( 0.0, -0.000591, -20.8 )
+ TKFRAME_-31107_AXES = ( 3, 1, 2 )
+ TKFRAME_-31107_UNITS = 'DEGREES'
+
+\begintext
+
diff --git a/tests/pytests/data/c1637937/voyagerAddendum004.ti b/tests/pytests/data/c1637937/voyagerAddendum004.ti
new file mode 100644
index 0000000000000000000000000000000000000000..39cf4aed9ea5c0195e4045c179e81661639b5546
--- /dev/null
+++ b/tests/pytests/data/c1637937/voyagerAddendum004.ti
@@ -0,0 +1,36 @@
+\begindata
+INS-31101_SPK_TIME_BIAS = 0.0
+INS-31101_CK_TIME_BIAS = 0.0
+INS-31101_CK_TIME_TOLERANCE = 2000
+INS-31101_PIXEL_PITCH = 0.0117894735849433
+INS-31101_FOCAL_LENGTH = 1500.19
+
+INS-31101_TRANSX = ( 0.0, 0.0117894735849433, 0.0)
+INS-31101_TRANSY = ( 0.0, 0.0, 0.0117894735849433)
+INS-31101_ITRANSS = ( 0.0, 84.8214292856238, 0.0)
+INS-31101_ITRANSL = ( 0.0, 0.0, 84.8214292856238)
+INS-31101_PLATFORM_ID = -31001
+
+INS-31102_SPK_TIME_BIAS = 0.0
+INS-31102_CK_TIME_BIAS = 0.0
+INS-31102_CK_TIME_TOLERANCE = 2000
+INS-31102_PIXEL_PITCH = 0.0117995980726038
+INS-31102_FOCAL_LENGTH = 200.465
+
+INS-31102_TRANSX = ( 0.0, 0.0117995980726038, 0.0)
+INS-31102_TRANSY = ( 0.0, 0.0, 0.0117995980726038)
+INS-31102_ITRANSS = ( 0.0, 84.7486493901678597, 0.0)
+INS-31102_ITRANSL = ( 0.0, 0.0, 84.7486493901678597)
+INS-31102_PLATFORM_ID = -31002
+
+\begintext
+These are the parameters for writing c-kernels. Isis will create ck
+with the same frame endpoints as the mission ck. For Voyager 1 the ck
+instrument frame is VG1_SCAN_PLATFORM (-31100) and the ck reference frame
+is B1950 (2).
+
+\begindata
+INS-31101_CK_FRAME_ID=-31100
+INS-31101_CK_REFERENCE_ID=2
+INS-31102_CK_FRAME_ID=-31100
+INS-31102_CK_REFERENCE_ID=2
diff --git a/tests/pytests/data/c1638610/c1638610_0.xsp b/tests/pytests/data/c1638610/c1638610_0.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..920087c1ea094323d7c88737a987fb7ec3156344
--- /dev/null
+++ b/tests/pytests/data/c1638610/c1638610_0.xsp
@@ -0,0 +1,283 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 39
+'DE-0431LE-0431 '
+'-272CF056F563CE^8'
+'-272CEFDB397C6^8'
+'A'
+'0'
+'1'
+'2'
+39
+'-272430C^8'
+'A8C^5'
+'EC78E52955EAB8^5'
+'1C3B51130EA43B^4'
+'-1517B2F2A083FE^2'
+'-7302FFCDF5B21C^-1'
+'4C56C1FC317FE^-1'
+'D84BC3DD7A3738^-3'
+'-18BA33A1847741^-2'
+'262F93E1AB77F2^-3'
+'5982DE342B8E2^-4'
+'-1A7957C52EF343^-4'
+'B47810D3A6AED8^-6'
+'-578BFFD7D2315^5'
+'19684CFAEC5644^4'
+'102AC456B383AF^2'
+'-35AD5955304CB8^0'
+'-105989430F77B4^-1'
+'99B8C6DF26516^-2'
+'-7219916C05E8A8^-3'
+'-2C6E9A4DE71BE8^-3'
+'815BA1AEFEBB98^-4'
+'40731B19C9E9E8^-5'
+'-4025C01F55786C^-5'
+'-2D3077BE089514^5'
+'A0E1BDB40DA398^3'
+'78A5619A09CC78^1'
+'-18B400BD2BC245^0'
+'-1103AA104BFD5E^-1'
+'505243F36CEFE8^-2'
+'-13CF0B4B289C2^-3'
+'-1BB1A4CD0B023D^-3'
+'3BCDD0C9E1EA66^-4'
+'4E61B89824181C^-5'
+'-236EECAD1C1A7A^-5'
+'-272EBCC^8'
+'1518^6'
+'23^2'
+'1^1'
+END_ARRAY 1 39
+BEGIN_ARRAY 2 30
+'DE-0431LE-0431 '
+'-272CF056F563CE^8'
+'-272CEFDB397C6^8'
+'5'
+'0'
+'1'
+'2'
+30
+'-272EBCC^8'
+'1518^6'
+'-1C98F7183CAA49^8'
+'-DE1D01F7B5228^6'
+'F038B4AC7943^4'
+'117A9725966F3E^3'
+'-D6E2F741064B5^0'
+'-26EF0C06801A4^-2'
+'54CBC8E3C79E6^-4'
+'622B6EF27493FC^-5'
+'222588455BDA1C^8'
+'-901B5206B6BDE8^6'
+'-11E95B6C84571E^5'
+'EEA6A0384935^2'
+'917136918B187^0'
+'-88F4F7AE87406^-2'
+'3B00FFE44905E6^-4'
+'-36ABAA7A67DDE4^-5'
+'F559B240B237A^7'
+'-385CD0236907A4^6'
+'-80B47F78587C9^4'
+'5F7DD244B77274^2'
+'439758CE355188^0'
+'-39D00CF72F80F8^-2'
+'15B92AD2AE995E^-4'
+'-106D0765B70BD8^-5'
+'-2743D4C^8'
+'2A3^6'
+'1A^2'
+'1^1'
+END_ARRAY 2 30
+BEGIN_ARRAY 3 72
+'JUP310 '
+'-272CF056F563CE^8'
+'-272CEFDB397C6^8'
+'257'
+'5'
+'1'
+'3'
+72
+'-272CC28^8'
+'A8C^4'
+'9DDE18B142717^2'
+'3BD5F202FB747C^2'
+'-41DACEF4DC252^1'
+'-3EB79240A3E86A^1'
+'-1D46107C41E08^0'
+'2672D91BB290C8^0'
+'EDF84594AF4^-2'
+'-A23881693EE8^-2'
+'140B384638^-3'
+'7974914508^-4'
+'-5873E1B88C6^-4'
+'-6E8C630FB7639^2'
+'2D1E72DB893FF6^2'
+'DB59BEBDBDF35^1'
+'1D25FC7D84317^0'
+'-C4F97266EF9A2^0'
+'-621680F439C38^-1'
+'4F69FB6E1FCE^-1'
+'12E693142F9C^-2'
+'-C6FF5E308A^-3'
+'E71F66729^-4'
+'-1FB5A0818DE^-4'
+'-326E10FD62D74E^2'
+'164B65854DD05A^2'
+'67EDD04B2EFC2^1'
+'-2420DADC9431^-1'
+'-5E5EFDA21BD83^0'
+'-24C5CD2AB5586^-1'
+'260DF83613F4^-1'
+'665CF9151AC^-3'
+'-5E30A6E11F8^-3'
+'6F7EB825B8^-4'
+'-10FCA19187C^-4'
+'4A0BE8919432B8^-2'
+'-1A4C221B9079C9^-2'
+'-2173F6C48407B8^-2'
+'-15246275FE0245^-3'
+'239DF4739ED244^-3'
+'1100083C16C78A^-4'
+'-D685F64910216^-5'
+'13EC87FCA9F562^-6'
+'CF48A601C28F58^-7'
+'-A7BB8250AF2B98^-7'
+'0^0'
+'44C9727B632FE4^-2'
+'4A337319C3DEF^-2'
+'ADFA41611CC56^-4'
+'-8FD60CE9F79EE^-3'
+'-5B5666EC67D4CC^-4'
+'59295B6CA42204^-4'
+'1AA13581334321^-5'
+'-131A510A7E0451^-5'
+'18A730797258BF^-6'
+'-3C216D0C6DBF86^-7'
+'0^0'
+'21B6E93F01FB62^-2'
+'231BEAECA849F2^-2'
+'-36D77A902418AC^-4'
+'-44E956066E0314^-3'
+'-2249E86FF4336A^-4'
+'2ABB4B1F9074A8^-4'
+'93C53B6268704^-6'
+'-90E72DE4AE9E88^-6'
+'BE48E85BAE1478^-7'
+'-20364B08973AC8^-7'
+'0^0'
+'-272D6B4^8'
+'1518^5'
+'44^2'
+'1^1'
+END_ARRAY 3 72
+BEGIN_ARRAY 4 73
+'vgr1.jup230.nio '
+'-272CF056F563CE^8'
+'-272CEFDB397C6^8'
+'-1F'
+'5'
+'1'
+'1'
+73
+'-272CE5F90BDD98^8'
+'23B2BEACB7C^3'
+'47657D596F8^3'
+'6B183C06274^3'
+'8ECAFAB2DF^3'
+'B27DB95F96C^3'
+'D630780C4E8^3'
+'F9E336B9064^3'
+'11D95F565BE^4'
+'14148B41275C^4'
+'164FB72BF2D8^4'
+'188AE316BE54^4'
+'1AC60F0189D^4'
+'1D013AEC554C^4'
+'1F3C66D720C8^4'
+'217792C1EC44^4'
+'5DE65D9E1B6A64^5'
+'-11C43C35EDB5AE^2'
+'1DC7A43A6209DC^5'
+'12D3CB9A2BA836^2'
+'5A3B22097C7018^4'
+'88AC5C018D3FD8^1'
+'-306C722BC1383A^-2'
+'-F97B7CB668B46^-4'
+'15BF60798105B4^-4'
+'490EBD63074128^-5'
+'6C3862C02CE428^-6'
+'-32657EFD422C1A^-7'
+'-3E2F712826134E^-7'
+'-F0BBE638A53A38^-8'
+'-1AEF702F40EFC2^-8'
+'4C2FB61D26675^-9'
+'3B96D6D37EA446^-9'
+'12FB3757CE1072^-9'
+'31D1EA6BE348^-A'
+'-83A9F52A36B29^-B'
+'-B5F18^-B'
+'-F60BDFB5B2A45^-3'
+'-1FD871E81FAF99^-3'
+'-20EDDD65B95572^-4'
+'-1832D108B62BE^-6'
+'7037ED09B34FC^-6'
+'16D3C1C4995F62^-6'
+'222AA564ED1BFE^-7'
+'-49887FB40124E8^-8'
+'-3157766E8C8FB4^-8'
+'-CF277437A9789^-9'
+'-18F41BA97BAF78^-9'
+'65552272072524^-A'
+'54057C54FD1328^-A'
+'1EE8EA5CDB2B4E^-A'
+'66A078^-B'
+'-2E894B74D06BA8^-3'
+'-B7E72F1261867^-4'
+'-E54C328F0BCBE8^-5'
+'-550F4F16843898^-6'
+'250ACD3D098E28^-6'
+'929482C4C7A38^-7'
+'116E00F2AEBF7^-7'
+'-D42D326C18495^-9'
+'-119BAFCAEF8E36^-8'
+'-5629F8ABD1D768^-9'
+'-DA3DB078AAF96^-A'
+'14121E0BA345FE^-A'
+'1DB25752C99531^-A'
+'C9C8D16961367^-B'
+'32CD54^-B'
+'F^1'
+'E^1'
+'E^1'
+'E^1'
+'-272CE5F90BDD98^8'
+'1^1'
+END_ARRAY 4 73
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /work/users/jmapel/ale/voyager_images/kernels_1_wac/c1638610_0.bsp LOG FILE
+
+; Created 2019-09-19/12:38:51.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /work/users/jmapel/ale/voyager_images/kernels_1_wac/c1638610_0.bsp
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/spk/jup310.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 5, 10, 599
+ BEGIN_TIME = 1979 MAR 05 08:43:34.856
+ END_TIME = 1979 MAR 05 08:45:38.590
+SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/voyager1/kernels/spk//vgr1_jup230.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -31
+ BEGIN_TIME = 1979 MAR 05 08:43:34.856
+ END_TIME = 1979 MAR 05 08:45:38.590
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c1638610/c1638610_1.xsp b/tests/pytests/data/c1638610/c1638610_1.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..8b90522621c064c7b4091a3a2770a72a9fb204ca
--- /dev/null
+++ b/tests/pytests/data/c1638610/c1638610_1.xsp
@@ -0,0 +1,355 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
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+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /work/users/jmapel/ale/voyager_images/kernels_1_wac/c1638610_1.bsp LOG FILE
+
+; Created 2019-09-19/12:38:51.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /work/users/jmapel/ale/voyager_images/kernels_1_wac/c1638610_1.bsp
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/spk/jup310.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 5, 10, 599
+ BEGIN_TIME = 1979 MAR 05 09:27:34.628
+ END_TIME = 1979 MAR 05 09:29:34.628
+SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/voyager1/kernels/spk//vgr1_jup230.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -31
+ BEGIN_TIME = 1979 MAR 05 09:27:34.628
+ END_TIME = 1979 MAR 05 09:29:34.628
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c1638610/c1638610_isis3.lbl b/tests/pytests/data/c1638610/c1638610_isis3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..1d6231b0b4c66717c27b78a95f4313370f4d0b47
--- /dev/null
+++ b/tests/pytests/data/c1638610/c1638610_isis3.lbl
@@ -0,0 +1,140 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 800
+ TileLines = 800
+
+ Group = Dimensions
+ Samples = 800
+ Lines = 800
+ Bands = 1
+ End_Group
+
+ Group = Pixels
+ Type = UnsignedByte
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftClockCount = 1638610
+ SpacecraftName = VOYAGER_1
+ TargetName = Jupiter
+ StartTime = 1979-03-05T09:28:36.628
+ InstrumentId = WIDE_ANGLE_CAMERA
+ ScanModeId = 1:1
+ ShutterModeId = BSIMAN
+ GainModeId = LOW
+ EditModeId = 1:1
+ ExposureDuration = 0.3600 <seconds>
+ CameraState1 = 1
+ CameraState2 = 1
+ End_Group
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+ Group = Archive
+ MissionPhaseName = JUPITER_ENCOUNTER
+ ProductId = 1607J1-001
+ End_Group
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+ Group = BandBin
+ FilterName = ORANGE
+ FilterNumber = 7
+ FilterNameLong = ORANGE
+ Center = 0.615000 <micrometers>
+ Width = 0.090000 <micrometers>
+ End_Group
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+ Group = Kernels
+ NaifFrameCode = -31102
+ End_Group
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+ Group = Reseaus
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+Object = History
+ Name = IsisCube
+ StartByte = 705537
+ Bytes = 444
+End_Object
+
+Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 705981
+ Bytes = 1946
+End_Object
+End
diff --git a/tests/pytests/data/c1638610/naif0012.tls b/tests/pytests/data/c1638610/naif0012.tls
new file mode 100644
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/c1638610/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/c1638610/pck00009.tpc b/tests/pytests/data/c1638610/pck00009.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..bfadaab2b26817327189ff3173e9609f49dedc9d
--- /dev/null
+++ b/tests/pytests/data/c1638610/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/c1638610/vg100010.tsc b/tests/pytests/data/c1638610/vg100010.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..78975fabf9470ad28dee3232360ef671a66f9ebe
--- /dev/null
+++ b/tests/pytests/data/c1638610/vg100010.tsc
@@ -0,0 +1,1108 @@
+
+KPL/SCLK
+
+
+\beginlabel
+
+MISSION_NAME = VOYAGER
+SPACECRAFT_NAME = VG1
+SPICE_DATA_TYPE = SCLK
+DATA_SET_ID = "VG1-X-SPICE-6-SCLK-V2.0"
+FILE_NAME = "VG100010.TSC"
+PRODUCT_ID = "VG100010.TSC"
+SOURCE_PRODUCT_ID = { "SCLK_SCET.31 version A061115,
+dated 2006-11-15T14:06:22", "SCLK_SCET.31 version A051104,
+dated 2005-11-04T14:46:04", "SCLK_SCET.31 version A991116,
+dated 1999-11-16T16:34:17", "SDT*FDSCSCEA., DATED 1999-08-27T14:40:04"}
+SOFTWARE_NAME = "MAKVSK, by Nat Bachman of NAIF"
+PRODUCT_CREATION _TIME = 2007-01-19T04:30:00
+PRODUCER_ID = NAIF, N. Bachman
+MISSION_PHASE_TYPE = {"CRUISE","ENCOUNTER","EXTENDED MISION"}
+MISSION_PHASE_NAME = {"CRUISE","JUPITER ENCOUNTER","SATURN
+ENCOUNTER","EXTENDED MISSION"}
+PRODUCT_VERSION_TYPE = RECONSTRUCTION
+START_TIME = 1977-09-05T14:09:24
+STOP_TIME = 2006-11-14T22:08:55
+SPACECRAFT_CLOCK_START_COUNT = "1/00012:00:001"
+SPACECRAFT_CLOCK_STOP_COUNT = "7/09650:00:001"
+NOTE = "CALIBRATED DATA COVERS FROM LAUNCH TO 2006-NOV-14 (2006//318).
+BUT THE FILE MAY BE USED IN PREDICT MODE THROUGH 2059-OCT-27
+(SCLK =15/65535:59:800). Records for partitions 1-4 were derived from the
+SCLKvSCET file dated 1999-08-27T14:40:04. Records for partition 5 start
+at UTC epoch 1994-01-11T04:33:25. These records were derived from the
+SCLKvSCET file having version ID A991116. Records for partition 6 start at
+UTC epoch 2000-01-004T17:21:06. These records were derived from the SCLKvSCET
+file having version ID A051104. Records for partition 7 start at UTC epoch
+2005-12-28T06:08:58. These records were derived from the SCLKvSCET file
+having version ID A061115. The portion of partition 7 that follows the
+stop time cited above, and partitions 8-15, constitute the predict region."
+
+\endlabel
+
+
+
+Voyager 1 SPICE SCLK Kernel
+--------------------------------------------------------
+
+ This file contains the data necessary to convert between Voyager 1
+ spacecraft clock time (SCLK) and ephemeris time.
+
+ NAIF suggests that you do not modify this file. If you do modify it,
+ be sure to indicate this in the `Version' section below.
+
+
+Version
+--------------------------------------------------------
+
+ This file is VG1 version 00010, produced January 19, 2007 by NAIF
+ (N. Bachman).
+
+ See label above for source file identification.
+
+Implementation notes
+--------------------------------------------------------
+
+ Older versions of this SCLK kernel contained code examples showing
+ calls to LDPOOL. NAIF now recommends using the more capable
+ routine FURNSH as the kernel loading interface. LDPOOL will
+ continue to be supported: existing SPICE-based applications that
+ load kernels using LDPOOL will continue to work as before when
+ linked against current (N0050 or greater) versions of SPICELIB or
+ CSPICE.
+
+ You must load this file into the kernel pool before using any of the
+ SPICELIB or CSPICE SCLK routines. The Fortran or C code fragments
+
+ CALL FURNSH ( name of this SCLK kernel ) {Fortran}
+
+ furnsh_c ( name of this SCLK kernel ); {C}
+
+ perform this task. To convert between ET and UTC, you will also need
+ to load a leapseconds kernel. The additional call to FURNSH,
+
+ CALL FURNSH ( name of your leapsecond file )
+
+ furnsh_c ( name of your leapsecond file );
+
+ You may find it more convenient to create a setup kernel and list the
+ names of these kernels in it. For example, we could call the setup
+ file setup.ker. This file would contain the kernel variable
+ assignment:
+
+ \begindata [The \begindata token starts a data section; it must
+ appear alone on a line to be recognized. This comment
+ is not part of the setup file's contents.]
+
+ KERNELS_TO_LOAD = ( 'name of SCLK kernel',
+ 'name of leapseconds kernel' )
+
+ The file names are delimited by single quotes regardless of whether
+ you're using the Fortran or C SPICE Toolkit.
+
+ You would load the kernels by supplying the name of your setup
+ file to FURNSH:
+
+ CALL FURNSH ( 'setup.ker' )
+
+ furnsh_c ( "setup.ker" );
+
+ You may list all of the SPICE kernels needed by your program in your
+ setup file. This one call to FURNSH may then replace all calls to LDPOOL
+ or other kernel loaders.
+
+ You must supply the actual names of the kernel files used on your system
+ as arguments to FURNSH or as values specified as "kernels to load" in
+ your FURNSH setup file. Because the file names are application
+ dependent, we do not list them here.
+
+ For more information on using SCLK within the SPICE system, consult your
+ SPICELIB required reading files. The following documents are pertinent:
+
+ SCLK system SCLK required reading
+ Time systems and conversion TIME required reading
+ FURNSH and kernel loading KERNEL required reading
+
+
+
+
+\begindata
+
+SCLK_KERNEL_ID = ( @19-JAN-2007/04:30 )
+
+SCLK_DATA_TYPE_31 = ( 1 )
+SCLK01_N_FIELDS_31 = ( 3 )
+SCLK01_MODULI_31 = ( 65536 60 800 )
+SCLK01_OFFSETS_31 = ( 0 0 1 )
+SCLK01_OUTPUT_DELIM_31 = ( 2 )
+
+SCLK_PARTITION_START_31 = ( 5.7600000000000E+05
+ 1.6964640000000E+08
+ 0.0000000000000E+00
+ 2.4800000000000E+04
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00
+ 0.0000000000000E+00 )
+
+SCLK_PARTITION_END_31 = ( 1.6964638300000E+08
+ 3.1457280010000E+09
+ 2.3082488000000E+09
+ 3.1457280000000E+09
+ 3.1457280020000E+09
+ 3.1457280010000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09
+ 3.1457279990000E+09 )
+
+SCLK01_COEFFICIENTS_31 = (
+
+ 0.00000000000000 -7.0441138821345E+08 2.8800027600000E+03
+ 480000.00000000 -7.0438258818546E+08 2.8800027600000E+03
+ 11424000.000000 -7.0372594755655E+08 2.8800101400000E+03
+ 11904000.000000 -7.0369714745555E+08 2.8800033600000E+03
+ 17904000.000000 -7.0333714703559E+08 2.8799953800000E+03
+ 18384000.000000 -7.0330834708159E+08 2.8800024000000E+03
+ 25824000.000000 -7.0286194670963E+08 2.8800063000000E+03
+ 26304000.000000 -7.0283314664663E+08 2.8800027600000E+03
+ 67200000.000000 -7.0037938429458E+08 2.8799969400000E+03
+ 67680000.000000 -7.0035058432558E+08 2.8800024600000E+03
+ 91008000.000000 -6.9895090312938E+08 2.8799972400000E+03
+ 91488000.000000 -6.9892210315738E+08 2.8800022800000E+03
+ 104112000.00000 -6.9816466255722E+08 2.8799979600000E+03
+ 104592000.00000 -6.9813586257821E+08 2.8800019200000E+03
+ 109440000.00000 -6.9784498238415E+08 2.8799978400000E+03
+ 109920000.00000 -6.9781618240514E+08 2.8800017400000E+03
+ 115440000.00000 -6.9748498220506E+08 2.8799943600000E+03
+ 115920000.00000 -6.9745618226205E+08 2.8800012600000E+03
+ 126480000.00000 -6.9682258198488E+08 2.8800096600000E+03
+ 126960000.00000 -6.9679378188887E+08 2.8800018000000E+03
+ 153264000.00000 -6.9521554090238E+08 2.8799986200000E+03
+ 153744000.00000 -6.9518674091537E+08 2.8800017400000E+03
+ 155616000.00000 -6.9507442084734E+08 2.8799970000000E+03
+ 156096000.00000 -6.9504562087733E+08 2.8800013200000E+03
+ 164400000.00000 -6.9454738064916E+08 2.8799965200000E+03
+ 164880000.00000 -6.9451858068415E+08 2.8800008400000E+03
+ 169070383.00000 -6.9426715761107E+08 2.8800008400000E+03
+ 169870383.00000 -6.9421915659705E+08 2.8800008400000E+03
+ 182159983.00000 -6.9348178038180E+08 2.8800076800000E+03
+ 182639983.00000 -6.9345298030479E+08 2.8800013800000E+03
+ 216431983.00000 -6.9142545933316E+08 2.8799972400000E+03
+ 216911983.00000 -6.9139665936115E+08 2.8800012000000E+03
+ 280703983.00000 -6.8756913776540E+08 2.8799963400000E+03
+ 281183983.00000 -6.8754033780240E+08 2.8800006600000E+03
+ 288863983.00000 -6.8707953769636E+08 2.8800061800000E+03
+ 289343983.00000 -6.8705073763536E+08 2.8800013200000E+03
+ 302303983.00000 -6.8627313727934E+08 2.8799955000000E+03
+ 302783983.00000 -6.8624433732434E+08 2.8800010800000E+03
+ 324431983.00000 -6.8494545683740E+08 2.8799952600000E+03
+ 324911983.00000 -6.8491665688440E+08 2.8800006000000E+03
+ 333023983.00000 -6.8442993678345E+08 2.8800060000000E+03
+ 333503983.00000 -6.8440113672345E+08 2.8800009600000E+03
+ 355967983.00000 -6.8305329627467E+08 2.8800057600000E+03
+ 356447983.00000 -6.8302449621667E+08 2.8800010200000E+03
+ 361055983.00000 -6.8274801611873E+08 2.8799943000000E+03
+ 361535983.00000 -6.8271921617573E+08 2.8800003000000E+03
+ 371471983.00000 -6.8212305611387E+08 2.8800069600000E+03
+ 371951983.00000 -6.8209425604388E+08 2.8800009000000E+03
+ 397055983.00000 -6.8058801557328E+08 2.8799944200000E+03
+ 397535983.00000 -6.8055921562929E+08 2.8800006600000E+03
+ 413231983.00000 -6.7961745541357E+08 2.8799939400000E+03
+ 413711983.00000 -6.7958865547458E+08 2.8800002400000E+03
+ 431087983.00000 -6.7854609538792E+08 2.8800061800000E+03
+ 431567983.00000 -6.7851729532593E+08 2.8800006000000E+03
+ 461423983.00000 -6.7672593495350E+08 2.8799955000000E+03
+ 461903983.00000 -6.7669713499851E+08 2.8800004200000E+03
+ 484703983.00000 -6.7532913479991E+08 2.8800103200000E+03
+ 485183983.00000 -6.7530033469592E+08 2.8800009000000E+03
+ 493343983.00000 -6.7481073454304E+08 2.8799941200000E+03
+ 493823983.00000 -6.7478193460205E+08 2.8800004200000E+03
+ 519167983.00000 -6.7326129438038E+08 2.8800069600000E+03
+ 519647983.00000 -6.7323249431139E+08 2.8800007800000E+03
+ 537215983.00000 -6.7217841402654E+08 2.8799950200000E+03
+ 537695983.00000 -6.7214961407555E+08 2.8800004800000E+03
+ 555551983.00000 -6.7107825389664E+08 2.8799937600000E+03
+ 556031983.00000 -6.7104945395964E+08 2.8800000000000E+03
+ 578879983.00000 -6.6967857395964E+08 2.8800073200000E+03
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+ 13707551986.000 1.1804172505035E+08 2.8800272400000E+03
+ 13708031986.000 1.1807052532335E+08 2.8800003000000E+03
+ 13743551986.000 1.2020172555542E+08 2.8799635800000E+03
+ 13744031986.000 1.2023052519143E+08 2.8799996400000E+03
+ 13801151986.000 1.2365772477711E+08 2.8800273000000E+03
+ 13801631986.000 1.2368652505012E+08 2.8800002400000E+03
+ 13948511986.000 1.3249932583956E+08 2.8799226000000E+03
+ 13948991986.000 1.3252812506556E+08 2.8800004200000E+03
+ 13994111986.000 1.3523532550263E+08 2.8799512800000E+03
+ 13994591986.000 1.3526412501562E+08 2.8800004200000E+03
+ 14009951986.000 1.3618572515254E+08 2.8799770800000E+03
+ 14010431986.000 1.3621452492353E+08 2.8800003600000E+03
+ 14040671986.000 1.3802892517922E+08 2.8799503800000E+03
+ 14041151986.000 1.3805772468421E+08 2.8800003000000E+03
+ 14064671986.000 1.3946892485885E+08 2.8799741400000E+03
+ 14065151986.000 1.3949772459985E+08 2.8800000000000E+03
+ 14102591986.000 1.4174412461016E+08 2.8800196200000E+03
+ 14103071986.000 1.4177292480715E+08 2.8799997600000E+03
+ 14164031986.000 1.4543052457003E+08 2.8800102600000E+03
+ 14164511986.000 1.4545932467302E+08 2.8799997600000E+03
+ 14331071986.000 1.5545292400418E+08 2.8799827800000E+03
+ 14331551986.000 1.5548172383219E+08 2.8799997600000E+03
+ 14366591986.000 1.5758412366986E+08 2.8799825400000E+03
+ 14367071986.000 1.5761292349587E+08 2.8799997600000E+03
+ 14439551986.000 1.6196172314519E+08 2.8800198600000E+03
+ 14440031986.000 1.6199052334419E+08 2.8799998200000E+03
+ 14606111986.000 1.7195532290358E+08 2.8800118200000E+03
+ 14606591986.000 1.7198412302257E+08 2.8799998200000E+03
+ 14716991986.000 1.7860812262666E+08 2.8799684400000E+03
+ 14717471986.000 1.7863692231065E+08 2.8799998800000E+03
+ 14767391986.000 1.8163212220234E+08 2.8800223200000E+03
+ 14767871986.000 1.8166092242634E+08 2.8799998800000E+03
+ 14812031986.000 1.8431052235155E+08 2.8799901000000E+03
+ 14812511986.000 1.8433932225256E+08 2.8799998200000E+03
+ 14890559987.000 1.8902220202682E+08 2.8799998200000E+03
+ 14890560787.000 1.8902225002682E+08 2.8799998200000E+03
+ 14895950387.000 1.8934562601093E+08 2.8199998200000E+03
+ 14895951187.000 1.8934567501093E+08 2.8799998200000E+03
+ 14899199987.000 1.8954060300199E+08 2.8799036400000E+03
+ 14899679987.000 1.8956940203800E+08 2.8799998800000E+03
+ 15020159987.000 1.9679820181665E+08 2.8799739600000E+03
+ 15020639987.000 1.9682700155665E+08 2.8799994000000E+03
+ 15068159987.000 1.9967820097749E+08 2.8800327600000E+03
+ 15068639987.000 1.9970700130548E+08 2.8799997000000E+03
+ 15119999987.000 2.0278860099980E+08 2.8800135600000E+03
+ 15120479987.000 2.0281740113579E+08 2.8799998200000E+03
+ 15213599987.000 2.0840460084907E+08 2.8800239400000E+03
+ 15214079987.000 2.0843340108906E+08 2.8799999400000E+03
+ 15251039987.000 2.1065100105357E+08 2.8799805600000E+03
+ 15251519987.000 2.1067980085957E+08 2.8799997000000E+03
+ 15285599987.000 2.1272460067535E+08 2.8800172800000E+03
+ 15286079987.000 2.1275340084835E+08 2.8799998200000E+03
+ 15353279987.000 2.1678540063173E+08 2.8799845200000E+03
+ 15353759987.000 2.1681420047773E+08 2.8799997600000E+03 )
+
+\begintext
diff --git a/tests/pytests/data/c1638610/vg1_isswa_v01.ti b/tests/pytests/data/c1638610/vg1_isswa_v01.ti
new file mode 100644
index 0000000000000000000000000000000000000000..de474fd19cf6b4ad23ea3393733d797e6218aa52
--- /dev/null
+++ b/tests/pytests/data/c1638610/vg1_isswa_v01.ti
@@ -0,0 +1,48 @@
+KPL/IK
+
+
+Voyager 1 Imaging Subsytem Wide Angle camera (ISSWA)
+----------------------------------------------------------------
+
+ Version 1 by Jeff Bytof -- 27 November 2000.
+
+ First version of the instrument kernel for Voyager 1's
+ ISSWA instrument.
+
+
+\begintext
+
+
+ Field of view description
+ -------------------------
+
+ - FOV is square with its sides along X and Y
+ axes of the instrument's frame;
+
+ - full FOV angular size in X and Y directions is 3.169 degrees;
+
+ - boresight vector intersects FOV exactly in the center of
+ the rectangle;
+
+
+\begindata
+
+
+ INS-31102_FOV_FRAME = 'VG1_ISSWA'
+
+ INS-31102_FOV_SHAPE = 'RECTANGLE'
+
+ INS-31102_BORESIGHT = ( 0.0 0.0 1.0 )
+
+
+ INS-31102_FOV_BOUNDARY_CORNERS = (
+
+ .02765 .02765 1.0
+ -.02765 .02765 1.0
+ -.02765 -.02765 1.0
+ .02765 -.02765 1.0
+
+ )
+
+\begintext
+
diff --git a/tests/pytests/data/c1638610/vg1_jup_qmw_wa_fc-31100_t2_0_sliced_-31100.xc b/tests/pytests/data/c1638610/vg1_jup_qmw_wa_fc-31100_t2_0_sliced_-31100.xc
new file mode 100644
index 0000000000000000000000000000000000000000..06c44c55e6fb80e45c66e4a0567c6676e842d06e
--- /dev/null
+++ b/tests/pytests/data/c1638610/vg1_jup_qmw_wa_fc-31100_t2_0_sliced_-31100.xc
@@ -0,0 +1,31 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+' '
+BEGIN_ARRAY 1 10
+'VG1 JUP SEDR QMW IMAGE NAV POINTING: WA '
+'2ED81932^8'
+'2ED8214^8'
+'-797C'
+'2'
+'2'
+'1'
+10
+'87D8B06B603248^0'
+'502240E7BBD1B8^0'
+'B04DCCAEF892F^0'
+'-61DD09CF5B6C7^0'
+'0^0'
+'0^0'
+'0^0'
+'1^1'
+'2ED81932^8'
+'2ED81B7E^8'
+END_ARRAY 1 10
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /work/users/jmapel/ale/voyager_images/c1638610.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c1638610/vg1_jup_qmw_wa_fc-31100_t2_1_sliced_-31100.xc b/tests/pytests/data/c1638610/vg1_jup_qmw_wa_fc-31100_t2_1_sliced_-31100.xc
new file mode 100644
index 0000000000000000000000000000000000000000..31727dbf9553607b704fff19f7e73419cf08d8a9
--- /dev/null
+++ b/tests/pytests/data/c1638610/vg1_jup_qmw_wa_fc-31100_t2_1_sliced_-31100.xc
@@ -0,0 +1,31 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+' '
+BEGIN_ARRAY 1 10
+'VG1 JUP SEDR QMW IMAGE NAV POINTING: WA '
+'2ED8C506^8'
+'2ED8CCD5^8'
+'-797C'
+'2'
+'2'
+'1'
+10
+'77A6B0ECAC4A2C^0'
+'3FD95D038688FE^0'
+'B669223990BF28^0'
+'-75C48BEC4B2CB8^0'
+'0^0'
+'0^0'
+'0^0'
+'1^1'
+'2ED8C75E^8'
+'2ED8CA7E^8'
+END_ARRAY 1 10
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /work/users/jmapel/ale/voyager_images/c1638610.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c1638610/vg1_v02.tf b/tests/pytests/data/c1638610/vg1_v02.tf
new file mode 100644
index 0000000000000000000000000000000000000000..2b2b6ffaf80b4c2f88be245d98e27e737837aa56
--- /dev/null
+++ b/tests/pytests/data/c1638610/vg1_v02.tf
@@ -0,0 +1,331 @@
+KPL/FK
+
+Voyager-1 Frame Kernel
+===========================================================================
+
+ This file contains various frame definitions for Voyager-1, related
+ to the spacecraft body and the scan platform.
+
+
+Version and Date
+--------------------------------------------------------
+
+ Version 2.0 -- 27 November 2000 -- Jeff Bytof
+
+ Changed instrument base frame to VG1_SCAN_PLATFORM.
+
+
+ Version 1.1 -- 8 March 2000 -- Jeff Bytof
+
+ Added the spacecraft high-gain antenna frame, FRAME_VG1_HGA.
+
+ Added -100 to all scan platform instrument ID codes, to
+ associate them to the scan platform ID code of -31100.
+
+
+ Version 1.0 -- 4 November 1999 -- Jeff Bytof
+
+ Initial Release.
+
+
+References
+--------------------------------------------------------
+
+ (1) Frames Required Reading (NAIF document).
+
+ (2) C Kernel Required Reading (NAIF document).
+
+
+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. Loading the kernel associates data items with
+ their names in a data structure called the `kernel pool'. The SPICELIB
+ routine LDPOOL loads a kernel file into the pool as shown below.
+
+
+ CALL LDPOOL ( kernel_name )
+
+
+ In order for a program or subroutine to extract data from the pool,
+ the SPICELIB routines GDPOOL and GIPOOL are used. See [3] for more
+ details.
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+Naming Conventions
+--------------------------------------------------------
+
+ All names referencing values in this frame kernel start with the
+ characters `FRAME', 'CK' or `TKFRAME' followed by the Voyager-1
+ spacecraft bus ID number (-31000) added to the instrument or
+ alternate frame index number.
+
+ The remainder of the name is an underscore character followed by the
+ unique name of the data item. For example, the Voyager-1 cone/clock
+ offsets relative to the spacecraft frame, given as three Euler angles,
+ are specified using two items:
+
+ TKFRAME_-31200_ANGLES = ( 55.0, 0.0, 180.0 )
+ TKFRAME_-31200_AXES = ( 3, 2, 1 )
+
+ The upper bound on the length of the name of any data item is 32
+ characters.
+
+ If the same item is included in more then one file, or if the same
+ item appears more than once within a single file, the latest value
+ supersedes any earlier values.
+
+
+TKFRAME Keyword Description
+--------------------------------------------------------
+
+ This section describes the TKFRAME keywords. The rotational offsets
+ can be given as three angles -- ROLL, PITCH and YAW, from which
+ a rotation matrix can be constructed that will transform the components of
+ a vector expressed in the spacecraft frame to components expressed in
+ the antenna fixed frame. For example, if x, y and z are the components of
+ a vector expressed in the spacecraft frame, X, Y and Z will be the components
+ of the same vector expressed in the antenna fixed frame:
+
+
+ [ X ] [ ] [ x ]
+ | Y | = | ROT | | y |
+ [ Z ] [ ] [ z ]
+
+
+ where ROT is the rotation matrix constructed from the rotation angles
+ as follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ YAW ] [ PITCH ] [ ROLL ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where each of three matrixes on the right side represent a coordinate
+ frame rotation by the given angle around the indicated axis. See the
+ SPICELIB routine EUL2M for more information about constructing
+ a rotation matrix from a set of rotation angles.
+
+ Following are some examples of use of the TKFRAME keywords:
+
+ The keyword that indicates which frame the axis rotations are
+ referred to is:
+
+ TKFRAME_-31200_RELATIVE = 'VG1_SC_BUS'
+
+
+ The keyword TKFRAME_-91000_ANGLES contain these values, in radians,
+ in the following order:
+
+ ``ROLL'' ``PITCH'' ``YAW''
+ TKFRAME_-31200_ANGLES = ( 55.0, 0.0, 180.0 )
+
+
+ The keyword TKFRAME_-31200_AXES contains integer codes of the
+ corresponding axes of rotations (1 -- X, 2 -- Y, 3 -- Z).
+
+ TKFRAME_-31200_AXES = ( 3, 2, 1 )
+
+
+ The keyword TKFRAME_-31200_UNITS gives the units of the angles.
+
+ TKFRAME_-31202_UNITS = 'DEGREES'
+
+
+
+
+
+Spacecraft Bus
+--------------------------------------------------------
+
+ The following data represents the basic spacecraft bus, and
+ the scan platform. Spacecraft bus attitude with respect to an inertial
+ frame is provided by a C kernel (see [2] for more information).
+ Scan platform orientation with respect to an inertial frame
+ is also provided by a C-kernel. Each instrument mounted
+ on the scan platform may have measureable offsets from the
+ nominal scan platform orientation. The Narrow Angle camera
+ has been chosen as representative of the scan platform orientation.
+
+\begindata
+
+ FRAME_VG1_SC_BUS = -31000
+ FRAME_-31000_NAME = 'VG1_SC_BUS'
+ FRAME_-31000_CLASS = 3
+ FRAME_-31000_CLASS_ID = -31000
+ FRAME_-31000_CENTER = -31
+ CK_-31000_SCLK = -31
+ CK_-31000_SPK = -31
+
+ FRAME_VG1_SCAN_PLATFORM = -31100
+ FRAME_-31100_NAME = 'VG1_SCAN_PLATFORM'
+ FRAME_-31100_CLASS = 3
+ FRAME_-31100_CLASS_ID = -31100
+ FRAME_-31100_CENTER = -31
+ CK_-31100_SCLK = -31
+ CK_-31100_SPK = -31
+
+\begintext
+
+
+Frame Definitions
+--------------------------------------------------------
+
+ Here are the frame definitions for Voyager 1. These are
+ utilized by SPICE's FRAMES subsystem to provide automatic state
+ transformations to/from the various frames. Note that SPICE toolkit
+ version N0047 or higher is required to use fixed-offset frames.
+
+ Note that angles in the frame definitions are specified for the "from
+ instrument to base (relative to) frame" transformation.
+
+
+ Spacecraft body-fixed reference frames:
+
+
+\begindata
+
+ FRAME_VG1_CONE_CLOCK = -31200
+ FRAME_-31200_NAME = 'VG1_CONE_CLOCK'
+ FRAME_-31200_CLASS = 4
+ FRAME_-31200_CLASS_ID = -31200
+ FRAME_-31200_CENTER = -31
+ TKFRAME_-31200_SPEC = 'ANGLES'
+ TKFRAME_-31200_RELATIVE = 'VG1_SC_BUS'
+ TKFRAME_-31200_ANGLES = ( 55.0, 0.0, 180.0 )
+ TKFRAME_-31200_AXES = ( 3, 2, 1 )
+ TKFRAME_-31200_UNITS = 'DEGREES'
+
+ FRAME_VG1_AZ_EL = -31300
+ FRAME_-31300_NAME = 'VG1_AZ_EL'
+ FRAME_-31300_CLASS = 4
+ FRAME_-31300_CLASS_ID = -31300
+ FRAME_-31300_CENTER = -31
+ TKFRAME_-31300_SPEC = 'ANGLES'
+ TKFRAME_-31300_RELATIVE = 'VG1_SC_BUS'
+ TKFRAME_-31300_ANGLES = ( -173.0, 0.0, 180.0 )
+ TKFRAME_-31300_AXES = ( 1, 2, 3 )
+ TKFRAME_-31300_UNITS = 'DEGREES'
+
+\begintext
+
+ The boresight of the antenna is the +Z axis.
+
+\begindata
+
+ FRAME_VG1_HGA = -31400
+ FRAME_-31400_NAME = 'VG1_HGA'
+ FRAME_-31400_CLASS = 4
+ FRAME_-31400_CLASS_ID = -31400
+ FRAME_-31400_CENTER = -31
+ TKFRAME_-31400_SPEC = 'ANGLES'
+ TKFRAME_-31400_RELATIVE = 'VG1_SC_BUS'
+ TKFRAME_-31400_ANGLES = ( 180.0, 0.0, 0.0 )
+ TKFRAME_-31400_AXES = ( 1, 2, 3 )
+ TKFRAME_-31400_UNITS = 'DEGREES'
+
+\begintext
+
+ Voyager-1 scan platform instrument frame definitions.
+
+ The Euler angles of rotation given below are
+ referred to the ISSNA frame of reference which
+ in this case is considered the equivalent of the
+ scan platform's frame.
+
+ Boresights are +Z in each instrument frame.
+
+
+\begindata
+
+
+ FRAME_VG1_ISSNA = -31101
+ FRAME_-31101_NAME = 'VG1_ISSNA'
+ FRAME_-31101_CLASS = 4
+ FRAME_-31101_CLASS_ID = -31101
+ FRAME_-31101_CENTER = -31
+ TKFRAME_-31101_SPEC = 'ANGLES'
+ TKFRAME_-31101_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31101_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-31101_AXES = ( 1, 2, 3 )
+ TKFRAME_-31101_UNITS = 'DEGREES'
+
+
+ FRAME_VG1_ISSWA = -31102
+ FRAME_-31102_NAME = 'VG1_ISSWA'
+ FRAME_-31102_CLASS = 4
+ FRAME_-31102_CLASS_ID = -31102
+ FRAME_-31102_CENTER = -31
+ TKFRAME_-31102_SPEC = 'ANGLES'
+ TKFRAME_-31102_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31102_ANGLES = ( 0.275, -0.0247, 0.0315 )
+ TKFRAME_-31102_AXES = ( 3, 1, 2 )
+ TKFRAME_-31102_UNITS = 'DEGREES'
+
+
+ FRAME_VG1_PPS = -31103
+ FRAME_-31103_NAME = 'VG1_PPS'
+ FRAME_-31103_CLASS = 4
+ FRAME_-31103_CLASS_ID = -31103
+ FRAME_-31103_CENTER = -31
+ TKFRAME_-31103_SPEC = 'ANGLES'
+ TKFRAME_-31103_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31103_ANGLES = ( 0.0, 0.0, -0.034 )
+ TKFRAME_-31103_AXES = ( 3, 1, 2 )
+ TKFRAME_-31103_UNITS = 'DEGREES'
+
+
+ FRAME_VG1_UVS = -31104
+ FRAME_-31104_NAME = 'VG1_UVS'
+ FRAME_-31104_CLASS = 4
+ FRAME_-31104_CLASS_ID = -31104
+ FRAME_-31104_CENTER = -31
+ TKFRAME_-31104_SPEC = 'ANGLES'
+ TKFRAME_-31104_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31104_ANGLES = ( 0.0, 0.030, 0.010 )
+ TKFRAME_-31104_AXES = ( 3, 1, 2 )
+ TKFRAME_-31104_UNITS = 'DEGREES'
+
+
+ FRAME_VG1_UVSOCC = -31105
+ FRAME_-31105_NAME = 'VG1_UVSOCC'
+ FRAME_-31105_CLASS = 4
+ FRAME_-31105_CLASS_ID = -31105
+ FRAME_-31105_CENTER = -31
+ TKFRAME_-31105_SPEC = 'ANGLES'
+ TKFRAME_-31105_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31105_ANGLES = ( 0.0, -0.00368, -19.5 )
+ TKFRAME_-31105_AXES = ( 3, 1, 2 )
+ TKFRAME_-31105_UNITS = 'DEGREES'
+
+
+ FRAME_VG1_IRIS = -31106
+ FRAME_-31106_NAME = 'VG1_IRIS'
+ FRAME_-31106_CLASS = 4
+ FRAME_-31106_CLASS_ID = -31106
+ FRAME_-31106_CENTER = -31
+ TKFRAME_-31106_SPEC = 'ANGLES'
+ TKFRAME_-31106_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31106_ANGLES = ( 0.0, -0.020, 0.024 )
+ TKFRAME_-31106_AXES = ( 3, 1, 2 )
+ TKFRAME_-31106_UNITS = 'DEGREES'
+
+
+ FRAME_VG1_IRISOCC = -31107
+ FRAME_-31107_NAME = 'VG1_IRISOCC'
+ FRAME_-31107_CLASS = 4
+ FRAME_-31107_CLASS_ID = -31107
+ FRAME_-31107_CENTER = -31
+ TKFRAME_-31107_SPEC = 'ANGLES'
+ TKFRAME_-31107_RELATIVE = 'VG1_SCAN_PLATFORM'
+ TKFRAME_-31107_ANGLES = ( 0.0, -0.000591, -20.8 )
+ TKFRAME_-31107_AXES = ( 3, 1, 2 )
+ TKFRAME_-31107_UNITS = 'DEGREES'
+
+\begintext
+
diff --git a/tests/pytests/data/c1638610/voyagerAddendum004.ti b/tests/pytests/data/c1638610/voyagerAddendum004.ti
new file mode 100644
index 0000000000000000000000000000000000000000..39cf4aed9ea5c0195e4045c179e81661639b5546
--- /dev/null
+++ b/tests/pytests/data/c1638610/voyagerAddendum004.ti
@@ -0,0 +1,36 @@
+\begindata
+INS-31101_SPK_TIME_BIAS = 0.0
+INS-31101_CK_TIME_BIAS = 0.0
+INS-31101_CK_TIME_TOLERANCE = 2000
+INS-31101_PIXEL_PITCH = 0.0117894735849433
+INS-31101_FOCAL_LENGTH = 1500.19
+
+INS-31101_TRANSX = ( 0.0, 0.0117894735849433, 0.0)
+INS-31101_TRANSY = ( 0.0, 0.0, 0.0117894735849433)
+INS-31101_ITRANSS = ( 0.0, 84.8214292856238, 0.0)
+INS-31101_ITRANSL = ( 0.0, 0.0, 84.8214292856238)
+INS-31101_PLATFORM_ID = -31001
+
+INS-31102_SPK_TIME_BIAS = 0.0
+INS-31102_CK_TIME_BIAS = 0.0
+INS-31102_CK_TIME_TOLERANCE = 2000
+INS-31102_PIXEL_PITCH = 0.0117995980726038
+INS-31102_FOCAL_LENGTH = 200.465
+
+INS-31102_TRANSX = ( 0.0, 0.0117995980726038, 0.0)
+INS-31102_TRANSY = ( 0.0, 0.0, 0.0117995980726038)
+INS-31102_ITRANSS = ( 0.0, 84.7486493901678597, 0.0)
+INS-31102_ITRANSL = ( 0.0, 0.0, 84.7486493901678597)
+INS-31102_PLATFORM_ID = -31002
+
+\begintext
+These are the parameters for writing c-kernels. Isis will create ck
+with the same frame endpoints as the mission ck. For Voyager 1 the ck
+instrument frame is VG1_SCAN_PLATFORM (-31100) and the ck reference frame
+is B1950 (2).
+
+\begindata
+INS-31101_CK_FRAME_ID=-31100
+INS-31101_CK_REFERENCE_ID=2
+INS-31102_CK_FRAME_ID=-31100
+INS-31102_CK_REFERENCE_ID=2
diff --git a/tests/pytests/data/c2065801/c2065801_0.xsp b/tests/pytests/data/c2065801/c2065801_0.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..2c6136bfa5044f8ae782e17bc2eae6e61cef99b3
--- /dev/null
+++ b/tests/pytests/data/c2065801/c2065801_0.xsp
@@ -0,0 +1,283 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 73
+'vgr2.jup230.nio '
+'-26862CD9C39E12^8'
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+'0^0'
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+'1518^5'
+'44^2'
+'1^1'
+END_ARRAY 4 72
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /work/users/jmapel/ale/voyager_images/kernels/c2065801_0.bsp LOG FILE
+
+; Created 2019-09-19/10:05:04.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /work/users/jmapel/ale/voyager_images/kernels/c2065801_0.bsp
+SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/voyager2/kernels/spk//vgr2_jup230.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -32
+ BEGIN_TIME = 1979 JUL 09 20:33:56.052
+ END_TIME = 1979 JUL 09 20:34:09.618
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/spk/jup310.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 5, 10, 599
+ BEGIN_TIME = 1979 JUL 09 20:33:56.052
+ END_TIME = 1979 JUL 09 20:34:09.618
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c2065801/c2065801_1.xsp b/tests/pytests/data/c2065801/c2065801_1.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..9ef7e862ccc266d41748f44b3f89b8c9536761df
--- /dev/null
+++ b/tests/pytests/data/c2065801/c2065801_1.xsp
@@ -0,0 +1,283 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 73
+'vgr2.jup230.nio '
+'-26862275DA66D4^8'
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+'-20'
+'5'
+'1'
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+BEGIN_ARRAY 4 72
+'JUP310 '
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+'0^0'
+'-26874E4^8'
+'1518^5'
+'44^2'
+'1^1'
+END_ARRAY 4 72
+TOTAL_ARRAYS 4
+ ~NAIF/SPC BEGIN COMMENTS~
+; /work/users/jmapel/ale/voyager_images/kernels/c2065801_1.bsp LOG FILE
+
+; Created 2019-09-19/10:05:04.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /work/users/jmapel/ale/voyager_images/kernels/c2065801_1.bsp
+SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/voyager2/kernels/spk//vgr2_jup230.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -32
+ BEGIN_TIME = 1979 JUL 09 21:18:15.963
+ END_TIME = 1979 JUL 09 21:18:25.963
+ SOURCE_SPK_KERNEL = /usgs/cpkgs/isis3/data/base/kernels/spk/jup310.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 5, 10, 599
+ BEGIN_TIME = 1979 JUL 09 21:18:15.963
+ END_TIME = 1979 JUL 09 21:18:25.963
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c2065801/c2065801_isis3.lbl b/tests/pytests/data/c2065801/c2065801_isis3.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..8268809c49f8f017274543ca70fd525f7c494b6d
--- /dev/null
+++ b/tests/pytests/data/c2065801/c2065801_isis3.lbl
@@ -0,0 +1,140 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 800
+ TileLines = 800
+
+ Group = Dimensions
+ Samples = 800
+ Lines = 800
+ Bands = 1
+ End_Group
+
+ Group = Pixels
+ Type = UnsignedByte
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftClockCount = 2065801
+ SpacecraftName = VOYAGER_2
+ TargetName = Jupiter
+ StartTime = 1979-07-09T21:18:22.963
+ InstrumentId = WIDE_ANGLE_CAMERA
+ ScanModeId = 1:1
+ ShutterModeId = BSIMAN
+ GainModeId = LOW
+ EditModeId = 1:1
+ ExposureDuration = 0.3600 <seconds>
+ CameraState1 = 1
+ CameraState2 = 1
+ End_Group
+
+ Group = Archive
+ MissionPhaseName = JUPITER_ENCOUNTER
+ ProductId = 1714J2-001
+ End_Group
+
+ Group = BandBin
+ FilterName = ORANGE
+ FilterNumber = 7
+ FilterNameLong = ORANGE
+ Center = 0.615000 <micrometers>
+ Width = 0.090000 <micrometers>
+ End_Group
+
+ Group = Kernels
+ NaifFrameCode = -32102
+ End_Group
+
+ Group = Reseaus
+ Line = (22.0, 14.0, 11.0, 6.0, 3.0, 3.0, 1.0, 1.0, 1.0, 1.0, -7.1,
+ 3.0, 31.0, 33.0, 29.0, 26.0, 24.0, 23.0, 22.0, 21.0, 20.0,
+ 20.0, 13.0, 67.0, 62.0, 58.0, 55.0, 53.0, 52.0, 50.0, 49.0,
+ 49.0, 48.0, 48.0, 46.7, 100.0, 96.0, 94.0, 92.0, 90.0, 89.0,
+ 88.0, 87.0, 86.0, 86.0, 86.0, 138.0, 135.0, 124.0, 121.6,
+ 174.0, 172.0, 170.0, 169.0, 168.0, 167.0, 167.0, 166.0, 165.0,
+ 164.0, 163.0, 214.0, 212.0, 203.0, 199.5, 251.0, 250.0, 248.0,
+ 247.0, 246.0, 245.0, 245.0, 244.0, 244.0, 243.0, 242.0, 289.5,
+ 289.0, 282.0, 277.7, 329.0, 327.0, 327.0, 326.0, 326.0, 325.0,
+ 324.0, 324.0, 323.0, 322.0, 321.0, 367.5, 367.0, 361.0, 357.0,
+ 407.0, 405.0, 405.0, 405.0, 405.0, 404.0, 404.0, 403.0, 403.0,
+ 402.0, 400.0, 445.7, 446.0, 440.0, 436.2, 486.0, 485.0, 484.0,
+ 483.0, 483.0, 483.0, 483.0, 482.0, 481.0, 481.0, 480.0, 524.2,
+ 525.0, 519.0, 515.0, 564.0, 564.0, 563.0, 562.0, 562.0, 562.0,
+ 561.0, 561.0, 561.0, 560.0, 558.0, 602.4, 603.0, 598.0, 593.2,
+ 641.0, 642.0, 641.0, 641.0, 640.0, 640.0, 640.0, 640.0, 639.0,
+ 638.0, 636.0, 681.0, 681.0, 674.0, 669.8, 718.0, 719.0, 719.0,
+ 719.0, 719.0, 718.0, 718.0, 717.0, 716.0, 714.0, 712.0, 755.0,
+ 755.0, 756.0, 757.0, 757.0, 757.0, 756.0, 756.0, 755.0, 753.0,
+ 750.0, 744.1, 791.0, 784.0, 784.0, 785.0, 785.0, 785.0, 784.0,
+ 784.0, 782.0, 779.0, 784.0, 801.0, 806.4, 804.1, 804.5, 804.5,
+ 804.4, 803.5, 802.3, 800.0, 798.2, 797.9, 794.0, 125.0)
+ Sample = (12.0, 58.0, 132.0, 208.0, 286.0, 365.0, 442.0, 521.0, 599.0,
+ 676.0, 750.3, 799.0, 21.0, 93.0, 169.0, 248.0, 326.0, 405.0,
+ 484.0, 562.0, 640.0, 717.0, 789.0, 4.0, 56.0, 131.0, 209.0,
+ 287.0, 366.0, 445.0, 524.0, 601.0, 678.0, 753.0, 801.8, 27.0,
+ 92.0, 169.0, 247.0, 326.0, 405.0, 484.0, 562.0, 641.0, 718.0,
+ 783.0, 6.0, 53.0, 756.0, 802.7, 25.0, 91.0, 168.0, 247.0,
+ 326.0, 404.0, 483.0, 562.0, 640.0, 718.0, 785.0, 4.0, 52.0,
+ 757.0, 804.2, 24.0, 90.0, 168.0, 246.0, 325.0, 404.0, 483.0,
+ 562.0, 640.0, 718.0, 785.0, 1.0, 51.0, 756.0, 804.3, 23.0,
+ 90.0, 167.0, 246.0, 325.0, 404.0, 482.0, 560.0, 640.0, 718.0,
+ 785.0, 1.0, 51.0, 756.0, 804.1, 22.0, 89.0, 166.0, 244.0,
+ 323.0, 402.0, 481.0, 560.0, 638.0, 717.0, 784.0, 1.0, 50.0,
+ 756.0, 803.6, 22.0, 88.0, 166.0, 244.0, 323.0, 402.0, 480.0,
+ 560.0, 638.0, 716.0, 783.0, 1.0, 50.0, 754.0, 802.8, 22.0,
+ 88.0, 165.0, 244.0, 322.0, 401.0, 479.0, 557.0, 637.0, 715.0,
+ 782.0, 1.0, 50.0, 753.0, 801.6, 23.0, 87.0, 164.0, 242.0,
+ 321.0, 399.0, 479.0, 557.0, 636.0, 714.0, 781.0, 4.0, 51.0,
+ 752.0, 800.5, 25.0, 88.0, 164.0, 242.0, 320.0, 399.0, 478.0,
+ 557.0, 635.0, 713.0, 779.0, 4.0, 53.0, 126.0, 203.0, 281.0,
+ 360.0, 438.0, 517.0, 596.0, 674.0, 750.0, 801.0, 20.0, 90.0,
+ 165.0, 242.0, 320.0, 399.0, 478.0, 556.0, 634.0, 712.0, 786.0,
+ 10.7, 55.0, 127.7, 203.8, 281.3, 359.6, 437.9, 517.0, 595.4,
+ 672.9, 748.6, 796.0, 603.0)
+ Type = (5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 5, 5, 5, 5, 5, 5, 5, 5, 5, 0, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5, 5,
+ 0, 0, 0, 0, 0, 0, 0, 0, 5, 5, 5, 5, 5)
+ Valid = (0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
+ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0)
+ Template = $voyager2/reseaus/vg2.isswa.template.cub
+ Status = Nominal
+ End_Group
+End_Object
+
+Object = Label
+ Bytes = 65536
+End_Object
+
+Object = History
+ Name = IsisCube
+ StartByte = 705537
+ Bytes = 444
+End_Object
+
+Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 705981
+ Bytes = 1912
+End_Object
+End
diff --git a/tests/pytests/data/c2065801/naif0012.tls b/tests/pytests/data/c2065801/naif0012.tls
new file mode 100644
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/c2065801/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/c2065801/pck00009.tpc b/tests/pytests/data/c2065801/pck00009.tpc
new file mode 100644
index 0000000000000000000000000000000000000000..bfadaab2b26817327189ff3173e9609f49dedc9d
--- /dev/null
+++ b/tests/pytests/data/c2065801/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/c2065801/vg200011.tsc b/tests/pytests/data/c2065801/vg200011.tsc
new file mode 100644
index 0000000000000000000000000000000000000000..12511cd3643e3c138dd49df21d22d04f74b657b1
--- /dev/null
+++ b/tests/pytests/data/c2065801/vg200011.tsc
@@ -0,0 +1,1391 @@
+KPL/SCLK
+
+
+\beginlabel
+
+MISSION_NAME = VOYAGER
+SPACECRAFT_NAME = VG2
+SPICE_DATA_TYPE = SCLK
+DATA_SET_ID = "VG2-X-SPICE-6-SCLK-V2.0"
+FILE_NAME = "VG200011.TSC"
+PRODUCT_ID = "VG200011.TSC"
+SOURCE_PRODUCT_ID = { "SCLK.SCET.32 version B100719,
+dated 2010-07-19T13:34:27", "SCLK_SCET.32 version B060714,
+dated 2006-07-14T14:46:43", "SCLK_SCET.32 version B000623,
+dated 2000-06-23T14:00:23", "FDSC/SCE FILE, DATED 1999-07-16T15:20:53" }
+SOFTWARE_NAME = "MAKVSK, by Nat Bachman of NAIF"
+PRODUCT_CREATION _TIME = 2010-07-20T02:40
+PRODUCER_ID = NAIF, N. Bachman
+MISSION_PHASE_TYPE = {"CRUISE","ENCOUNTER","EXTENDED MISSION"}
+MISSION_PHASE_NAME = {"CRUISE","JUPITER ENCOUNTER","SATURN
+ENCOUNTER","URANUS ENCOUNTER","NEPTUNE ENCOUNTER","EXTENDED MISSION"}
+PRODUCT_VERSION_TYPE = RECONSTRUCTION
+START_TIME = 1977-08-20T15:42:18
+STOP_TIME = 2010-10-16T18:06:30
+SPACECRAFT_CLOCK_START_COUNT = "1/00011:00:001"
+SPACECRAFT_CLOCK_STOP_COUNT = "7/46460:00:247"
+NOTE = "Calibrated data cover from launch to 2010-JUL-19 (2010//199),
+but the file may be used in predict mode through 2060 MAY 18,
+(SCLK =15/65535:59:800). Records for partitions 1-4 were derived from the
+SCLKvSCET file dated 1999-07-16. Records for partition 5 start at UTC epoch
+1994-08-04T00:34:09. These records were derived from the SCLKvSCET file
+having version ID B000623. Records for partition 6 start at UTC epoch
+2000-07-27T13:17:47. These records were derived from the SCLKvSCET file
+having version ID B060714. Records for partition 7 start at UTC epoch
+2006-07-21T02:01:22.573 These records were derived from the SCLKvSCET file
+having version ID B100719. The portion of partition 7 following
+2010-199T18:06:30 and partitions 8-15 constitute the predict region."
+
+\endlabel
+
+
+Voyager 2 SPICE SCLK Kernel
+--------------------------------------------------------
+
+ This file contains the data necessary to convert between Voyager 2
+ spacecraft clock time (SCLK) and ephemeris time.
+
+ NAIF suggests that you do not modify this file. If you do modify it,
+ be sure to indicate this in the `Version' section below.
+
+
+Version
+--------------------------------------------------------
+
+ This file is VG2 version 00011, produced July 20, 2010 by NAIF
+ (N. Bachman).
+
+ See the label above for list of source SCLKvSCET coefficient files.
+
+
+Implementation notes
+--------------------------------------------------------
+
+ You must load this file into the kernel pool before using any of the
+ SPICELIB SCLK routines. The code fragment
+
+ CALL FURNSH ( < name of this file > )
+
+ performs this task. To convert between ET and UTC, you will also need
+ to load a leapseconds kernel. The additional call to FURNSH,
+
+ CALL FURNSH ( < name of your leapsecond file > )
+
+ will accomplish this. Note that you must supply the actual names of
+ the files used on your system as arguments to FURNSH. Because the file
+ names are system dependent, we do not list them here.
+
+ For more information, consult your SPICELIB required reading files.
+ The following areas are covered:
+
+ SCLK system SCLK required reading
+ Time systems and conversion TIME required reading
+ Kernel pool KERNEL required reading
+
+
+Kernel data
+--------------------------------------------------------
+
+
+
+\begindata
+
+SCLK_KERNEL_ID = ( @20-JUL-2010/02:13 )
+
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+ 17308944032.000 3.3274845631262E+08 2.8799945400000E+03 )
+
+\begintext
diff --git a/tests/pytests/data/c2065801/vg2_isswa_v01.ti b/tests/pytests/data/c2065801/vg2_isswa_v01.ti
new file mode 100644
index 0000000000000000000000000000000000000000..24e53fa8d136b975679752751f2cedf9795b14ad
--- /dev/null
+++ b/tests/pytests/data/c2065801/vg2_isswa_v01.ti
@@ -0,0 +1,48 @@
+KPL/IK
+
+
+Voyager 2 Imaging Subsytem Wide Angle camera (ISSWA)
+----------------------------------------------------------------
+
+ Version 1 by Jeff Bytof -- 27 November 2000.
+
+ First version of the instrument kernel for Voyager 2's
+ ISSWA instrument.
+
+
+\begintext
+
+
+ Field of view description
+ -------------------------
+
+ - FOV is square with its sides along X and Y
+ axes of the instrument's frame;
+
+ - full FOV angular size in X and Y directions is 3.169 degrees;
+
+ - boresight vector intersects FOV exactly in the center of
+ the rectangle;
+
+
+\begindata
+
+
+ INS-32102_FOV_FRAME = 'VG2_ISSWA'
+
+ INS-32102_FOV_SHAPE = 'RECTANGLE'
+
+ INS-32102_BORESIGHT = ( 0.0 0.0 1.0 )
+
+
+ INS-32102_FOV_BOUNDARY_CORNERS = (
+
+ .02765 .02765 1.0
+ -.02765 .02765 1.0
+ -.02765 -.02765 1.0
+ .02765 -.02765 1.0
+
+ )
+
+\begintext
+
diff --git a/tests/pytests/data/c2065801/vg2_jup_qmw_wa_fc-32100_t2_0_sliced_-32100.xc b/tests/pytests/data/c2065801/vg2_jup_qmw_wa_fc-32100_t2_0_sliced_-32100.xc
new file mode 100644
index 0000000000000000000000000000000000000000..70658fad2e9edad351b0cd1d1b3dfa125560d5fa
--- /dev/null
+++ b/tests/pytests/data/c2065801/vg2_jup_qmw_wa_fc-32100_t2_0_sliced_-32100.xc
@@ -0,0 +1,31 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+' '
+BEGIN_ARRAY 1 10
+'VG2 JUP SEDR QMW IMAGE NAV POINTING: WA '
+'3B11A2CE^8'
+'3B11A3B1^8'
+'-7D64'
+'2'
+'2'
+'1'
+10
+'63DD97357FA3F4^0'
+'2ECA0EBE763CA^0'
+'BE2219D3A1D088^0'
+'-833C842E29CD5^0'
+'0^0'
+'0^0'
+'0^0'
+'1^1'
+'3B11A2CE^8'
+'3B11A2DE^8'
+END_ARRAY 1 10
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /work/users/jmapel/ale/voyager_images/c2065801.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c2065801/vg2_jup_qmw_wa_fc-32100_t2_1_sliced_-32100.xc b/tests/pytests/data/c2065801/vg2_jup_qmw_wa_fc-32100_t2_1_sliced_-32100.xc
new file mode 100644
index 0000000000000000000000000000000000000000..5a1819c456870107d687545b2e4a16a87e3a5761
--- /dev/null
+++ b/tests/pytests/data/c2065801/vg2_jup_qmw_wa_fc-32100_t2_1_sliced_-32100.xc
@@ -0,0 +1,31 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+' '
+BEGIN_ARRAY 1 10
+'VG2 JUP SEDR QMW IMAGE NAV POINTING: WA '
+'3B124FFA^8'
+'3B1250A1^8'
+'-7D64'
+'2'
+'2'
+'1'
+10
+'5ABA809877C32^0'
+'26094774A37598^0'
+'BFF25EA7F2B6E8^0'
+'-89E42EC5F9884^0'
+'0^0'
+'0^0'
+'0^0'
+'1^1'
+'3B124FFA^8'
+'3B1250A1^8'
+END_ARRAY 1 10
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /work/users/jmapel/ale/voyager_images/c2065801.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/c2065801/vg2_v02.tf b/tests/pytests/data/c2065801/vg2_v02.tf
new file mode 100644
index 0000000000000000000000000000000000000000..dfae5d6790ad479614ec7d32759c79c80063677b
--- /dev/null
+++ b/tests/pytests/data/c2065801/vg2_v02.tf
@@ -0,0 +1,339 @@
+KPL/FK
+
+Voyager-2 Frame Kernel
+===========================================================================
+
+ This file contains various frame definitions for Voyager-2,
+ related to the spacecraft body and the scan platform.
+
+
+Version and Date
+--------------------------------------------------------
+
+ Version 2 -- 27 Nov. 2000 -- Jeff Bytof
+
+ Changed base frame of instruments to VG2_SCAN_PLATFORM.
+
+ Eliminated multiple frames for PPS. That can
+ be handled in the PPS instrument kernel.
+
+
+ Version 1.2 -- 16 Aug. 2000 -- Jeff Bytof
+
+ Added additional frame definitions for the PPS instrument
+ because it has multiple fields of view.
+
+
+ Version 1.1 -- 8 March 2000 -- Jeff Bytof
+
+ Added the spacecraft high-gain antenna frame, FRAME_VG2_HGA.
+
+ Added -100 to all scan platform instrument ID codes, to
+ associate them to the scan platform ID code of -32100.
+
+
+ Version 1.0 -- 4 November 1999 -- Jeff Bytof
+
+ Initial Release.
+
+
+References
+--------------------------------------------------------
+
+ (1) Frames Required Reading (NAIF document).
+
+ (2) C Kernel Required Reading (NAIF document).
+
+
+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. Loading the kernel associates data items with
+ their names in a data structure called the `kernel pool'. The SPICELIB
+ routine LDPOOL loads a kernel file into the pool as shown below.
+
+
+ CALL LDPOOL ( kernel_name )
+
+
+ In order for a program or subroutine to extract data from the pool,
+ the SPICELIB routines GDPOOL and GIPOOL are used. See [3] for more
+ details.
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+Naming Conventions
+--------------------------------------------------------
+
+ All names referencing values in this frame kernel start with the
+ characters `FRAME', 'CK' or `TKFRAME' followed by the Voyager-2
+ spacecraft bus ID number (-32000) added to the instrument or
+ alternate frame index number.
+
+ The remainder of the name is an underscore character followed by the
+ unique name of the data item. For example, the Voyager-2 cone/clock
+ offsets relative to the spacecraft frame, given as three Euler angles,
+ are specified using two items:
+
+ TKFRAME_-32200_ANGLES = ( 55.0, 0.0, 180.0 )
+ TKFRAME_-32200_AXES = ( 3, 2, 1 )
+
+ The upper bound on the length of the name of any data item is 32
+ characters.
+
+ If the same item is included in more then one file, or if the same
+ item appears more than once within a single file, the latest value
+ supersedes any earlier values.
+
+
+TKFRAME Keyword Description
+--------------------------------------------------------
+
+ This section describes the TKFRAME keywords. The rotational offsets
+ can be given as three angles -- ROLL, PITCH and YAW, from which
+ a rotation matrix can be constructed that will transform the components
+ of a vector expressed in the spacecraft frame to components expressed
+ in the antenna fixed frame. For example, if x, y and z are the
+ components of a vector expressed in the spacecraft frame, X, Y and Z
+ will be the components of the same vector expressed in the antenna
+ fixed frame:
+
+
+ [ X ] [ ] [ x ]
+ | Y | = | ROT | | y |
+ [ Z ] [ ] [ z ]
+
+
+ where ROT is the rotation matrix constructed from the rotation angles
+ as follows:
+
+ [ ] [ ] [ ] [ ]
+ [ ROT ] = [ YAW ] [ PITCH ] [ ROLL ]
+ [ ] [ ] [ ] [ ]
+ Z Y X
+
+ where each of three matrixes on the right side represent a coordinate
+ frame rotation by the given angle around the indicated axis. See the
+ SPICELIB routine EUL2M for more information about constructing
+ a rotation matrix from a set of rotation angles.
+
+ Following are some examples of use of the TKFRAME keywords:
+
+ The keyword that indicates which frame the axis rotations are
+ referred to is:
+
+ TKFRAME_-32200_RELATIVE = 'VG2_SC_BUS'
+
+
+ The keyword TKFRAME_-91000_ANGLES contain these values, in radians,
+ in the following order:
+
+ ``ROLL'' ``PITCH'' ``YAW''
+ TKFRAME_-32200_ANGLES = ( 55.0, 0.0, 180.0 )
+
+
+ The keyword TKFRAME_-32200_AXES contains integer codes of the
+ corresponding axes of rotations (1 -- X, 2 -- Y, 3 -- Z).
+
+ TKFRAME_-32200_AXES = ( 3, 2, 1 )
+
+
+ The keyword TKFRAME_-32200_UNITS gives the units of the angles.
+
+ TKFRAME_-32202_UNITS = 'DEGREES'
+
+
+
+Spacecraft Bus
+--------------------------------------------------------
+
+ The following data represents the basic spacecraft bus, and
+ the scan platform. Spacecraft bus attitude with respect to an inertial
+ frame is provided by a C kernel (see [2] for more information).
+ Scan platform orientation with respect to an inertial frame
+ is also provided by a C-kernel. Each instrument mounted
+ on the scan platform may have measureable offsets from the
+ nominal scan platform orientation. The Narrow Angle camera
+ has been chosen as representative of the scan platform orientation.
+
+\begindata
+
+ FRAME_VG2_SC_BUS = -32000
+ FRAME_-32000_NAME = 'VG2_SC_BUS'
+ FRAME_-32000_CLASS = 3
+ FRAME_-32000_CLASS_ID = -32000
+ FRAME_-32000_CENTER = -32
+ CK_-32000_SCLK = -32
+ CK_-32000_SPK = -32
+
+ FRAME_VG2_SCAN_PLATFORM = -32100
+ FRAME_-32100_NAME = 'VG2_SCAN_PLATFORM'
+ FRAME_-32100_CLASS = 3
+ FRAME_-32100_CLASS_ID = -32100
+ FRAME_-32100_CENTER = -32
+ CK_-32100_SCLK = -32
+ CK_-32100_SPK = -32
+
+\begintext
+
+
+Frame Definitions
+--------------------------------------------------------
+
+ Here are the antenna frame definitions for Voyager 2. These will be
+ utilized by SPICE's FRAMES subsystem to provide automatic state
+ transformations to/from the Voyager-2 frame. Note that SPICE toolkit
+ version N0047 or higher is required to use fixed-offset frames.
+
+ Note that angles in the frame definitions are specified for the "from
+ instrument to base (relative to) frame" transformation.
+
+
+ Spacecraft body-fixed frames:
+
+
+\begindata
+
+ FRAME_VG2_CONE_CLOCK = -32200
+ FRAME_-32200_NAME = 'VG2_CONE_CLOCK'
+ FRAME_-32200_CLASS = 4
+ FRAME_-32200_CLASS_ID = -32200
+ FRAME_-32200_CENTER = -32
+ TKFRAME_-32200_SPEC = 'ANGLES'
+ TKFRAME_-32200_RELATIVE = 'VG2_SC_BUS'
+ TKFRAME_-32200_ANGLES = ( 55.0, 0.0, 180.0 )
+ TKFRAME_-32200_AXES = ( 3, 2, 1 )
+ TKFRAME_-32200_UNITS = 'DEGREES'
+
+ FRAME_VG2_AZ_EL = -32300
+ FRAME_-32300_NAME = 'VG2_AZ_EL'
+ FRAME_-32300_CLASS = 4
+ FRAME_-32300_CLASS_ID = -32300
+ FRAME_-32300_CENTER = -32
+ TKFRAME_-32300_SPEC = 'ANGLES'
+ TKFRAME_-32300_RELATIVE = 'VG2_SC_BUS'
+ TKFRAME_-32300_ANGLES = ( -173.0, 0.0, 180.0 )
+ TKFRAME_-32300_AXES = ( 1, 2, 3 )
+ TKFRAME_-32300_UNITS = 'DEGREES'
+
+
+\begintext
+
+ The boresight of the antenna is the +Z axis.
+
+\begindata
+
+ FRAME_VG2_HGA = -32400
+ FRAME_-32400_NAME = 'VG2_HGA'
+ FRAME_-32400_CLASS = 4
+ FRAME_-32400_CLASS_ID = -32400
+ FRAME_-32400_CENTER = -32
+ TKFRAME_-32400_SPEC = 'ANGLES'
+ TKFRAME_-32400_RELATIVE = 'VG2_SC_BUS'
+ TKFRAME_-32400_ANGLES = ( 180.0, 0.0, 0.0 )
+ TKFRAME_-32400_AXES = ( 1, 2, 3 )
+ TKFRAME_-32400_UNITS = 'DEGREES'
+
+\begintext
+
+ Voyager-2 scan platform instrument frame definitions.
+
+ The Euler angles of rotation given below are
+ referred to the ISSNA frame of reference which
+ in this case is considered the equivalent of the
+ scan platform's frame.
+
+ Boresights are +Z in each instrument frame.
+
+
+\begindata
+
+
+ FRAME_VG2_ISSNA = -32101
+ FRAME_-32101_NAME = 'VG2_ISSNA'
+ FRAME_-32101_CLASS = 4
+ FRAME_-32101_CLASS_ID = -32101
+ FRAME_-32101_CENTER = -32
+ TKFRAME_-32101_SPEC = 'ANGLES'
+ TKFRAME_-32101_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32101_ANGLES = ( 0.0, 0.0, 0.0 )
+ TKFRAME_-32101_AXES = ( 1, 2, 3 )
+ TKFRAME_-32101_UNITS = 'DEGREES'
+
+
+ FRAME_VG2_ISSWA = -32102
+ FRAME_-32102_NAME = 'VG2_ISSWA'
+ FRAME_-32102_CLASS = 4
+ FRAME_-32102_CLASS_ID = -32102
+ FRAME_-32102_CENTER = -32
+ TKFRAME_-32102_SPEC = 'ANGLES'
+ TKFRAME_-32102_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32102_ANGLES = ( 0.171102, 0.0068, -0.0308 )
+ TKFRAME_-32102_AXES = ( 3, 1, 2 )
+ TKFRAME_-32102_UNITS = 'DEGREES'
+
+
+ FRAME_VG2_PPS = -32103
+ FRAME_-32103_NAME = 'VG2_PPS'
+ FRAME_-32103_CLASS = 4
+ FRAME_-32103_CLASS_ID = -32103
+ FRAME_-32103_CENTER = -32
+ TKFRAME_-32103_SPEC = 'ANGLES'
+ TKFRAME_-32103_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32103_ANGLES = ( 0.0, -0.003, -0.060 )
+ TKFRAME_-32103_AXES = ( 3, 1, 2 )
+ TKFRAME_-32103_UNITS = 'DEGREES'
+
+
+ FRAME_VG2_UVS = -32104
+ FRAME_-32104_NAME = 'VG2_UVS'
+ FRAME_-32104_CLASS = 4
+ FRAME_-32104_CLASS_ID = -32104
+ FRAME_-32104_CENTER = -32
+ TKFRAME_-32104_SPEC = 'ANGLES'
+ TKFRAME_-32104_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32104_ANGLES = ( 0.0, -0.08, 0.0 )
+ TKFRAME_-32104_AXES = ( 3, 1, 2 )
+ TKFRAME_-32104_UNITS = 'DEGREES'
+
+
+ FRAME_VG2_UVSOCC = -32105
+ FRAME_-32105_NAME = 'VG2_UVSOCC'
+ FRAME_-32105_CLASS = 4
+ FRAME_-32105_CLASS_ID = -32105
+ FRAME_-32105_CENTER = -32
+ TKFRAME_-32105_SPEC = 'ANGLES'
+ TKFRAME_-32105_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32105_ANGLES = ( 0.0, 0.0, -19.26 )
+ TKFRAME_-32105_AXES = ( 3, 1, 2 )
+ TKFRAME_-32105_UNITS = 'DEGREES'
+
+
+ FRAME_VG2_IRIS = -32106
+ FRAME_-32106_NAME = 'VG2_IRIS'
+ FRAME_-32106_CLASS = 4
+ FRAME_-32106_CLASS_ID = -32106
+ FRAME_-32106_CENTER = -32
+ TKFRAME_-32106_SPEC = 'ANGLES'
+ TKFRAME_-32106_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32106_ANGLES = ( 0.0, 0.009 , 0.016 )
+ TKFRAME_-32106_AXES = ( 3, 1, 2 )
+ TKFRAME_-32106_UNITS = 'DEGREES'
+
+
+ FRAME_VG2_IRISOCC = -32107
+ FRAME_-32107_NAME = 'VG2_IRISOCC'
+ FRAME_-32107_CLASS = 4
+ FRAME_-32107_CLASS_ID = -32107
+ FRAME_-32107_CENTER = -32
+ TKFRAME_-32107_SPEC = 'ANGLES'
+ TKFRAME_-32107_RELATIVE = 'VG2_SCAN_PLATFORM'
+ TKFRAME_-32107_ANGLES = ( 0.0, 0.0, -20.8 )
+ TKFRAME_-32107_AXES = ( 3, 1, 2 )
+ TKFRAME_-32107_UNITS = 'DEGREES'
+
+\begintext
diff --git a/tests/pytests/data/c2065801/voyagerAddendum004.ti b/tests/pytests/data/c2065801/voyagerAddendum004.ti
new file mode 100644
index 0000000000000000000000000000000000000000..1bab47031b34785ada4f0c3ef4609cb27bd82215
--- /dev/null
+++ b/tests/pytests/data/c2065801/voyagerAddendum004.ti
@@ -0,0 +1,36 @@
+\begindata
+INS-32101_SPK_TIME_BIAS = 0.0
+INS-32101_CK_TIME_BIAS = 0.0
+INS-32101_CK_TIME_TOLERANCE = 2000
+INS-32101_PIXEL_PITCH = 0.011789473651194
+INS-32101_FOCAL_LENGTH = 1503.49
+
+INS-32101_TRANSX = ( 0.0, 0.011789473651194, 0.0)
+INS-32101_TRANSY = ( 0.0, 0.0, 0.011789473651194)
+INS-32101_ITRANSS = ( 0.0, 84.8214288089711, 0.0)
+INS-32101_ITRANSL = ( 0.0, 0.0, 84.8214288089711)
+INS-32101_PLATFORM_ID = -32001
+
+INS-32102_SPK_TIME_BIAS = 0.0
+INS-32102_CK_TIME_BIAS = 0.0
+INS-32102_CK_TIME_TOLERANCE = 2000
+INS-32102_PIXEL_PITCH = 0.0116661644275479
+INS-32102_FOCAL_LENGTH = 200.770
+
+INS-32102_TRANSX = ( 0.0, 0.0116661644275479, 0.0)
+INS-32102_TRANSY = ( 0.0, 0.0, 0.0116661644275479)
+INS-32102_ITRANSS = ( 0.0, 85.7179757931961, 0.0)
+INS-32102_ITRANSL = ( 0.0, 0.0, 85.7179757931961)
+INS-32102_PLATFORM_ID = -32002
+
+\begintext
+These are the parameters for writing c-kernels. Isis will create ck
+with the same frame endpoints as the mission ck. For Voyager 2 the ck
+instrument frame is VG1_SCAN_PLATFORM (-32100) and the ck reference frame
+is B1950 (2).
+
+\begindata
+INS-32101_CK_FRAME_ID=-32100
+INS-32101_CK_REFERENCE_ID=2
+INS-32102_CK_FRAME_ID=-32100
+INS-32102_CK_REFERENCE_ID=2
diff --git a/tests/pytests/test_mro_drivers.py b/tests/pytests/test_mro_drivers.py
index f671a228dcd6fc64d528992bcc709772676ab6c9..205051f12855770da200d2bc55481f1869da4ac1 100644
--- a/tests/pytests/test_mro_drivers.py
+++ b/tests/pytests/test_mro_drivers.py
@@ -235,12 +235,12 @@ def isis_compare_dict():
[0.42064763, 0.18624551, -0.2397057 , 0.85493237],
[0.42065923, 0.18630667, -0.23967382, 0.85492228],
[0.42067144, 0.18636687, -0.23964185, 0.85491211]],
- 'AngularVelocity': [[-6.157101679378247e-06, 0.0009352034475077121, -0.00011941673357358669],
- [-6.887942908783687e-06, 0.0009356318276404807, -0.00011800670313459697],
- [-1.0577832791680011e-05, 0.000937142301898857, -0.0001101520178027217],
- [-8.088753082470754e-06, 0.0009320299674209734, -0.00011098361545849514],
- [-8.410068339567782e-06, 0.0009332739373169815, -0.0001116179282972322],
- [-7.579826199031287e-06, 0.000938872225704521, -0.00011122572722581592]]},
+ 'AngularVelocity': [[-5.797334508173795e-05, 0.0009339642673794059, -0.00011512424986625757],
+ [-5.872001786769966e-05, 0.0009343455952639878, -0.00011371124132355403],
+ [-6.244619825703372e-05, 0.000935616649435616, -0.00010584418382022431],
+ [-5.965469273385757e-05, 0.0009306551165985512, -0.00010670063014175982],
+ [-6.001692495046523e-05, 0.0009318842753552843, -0.00010732755544866732],
+ [-5.9466333983691536e-05, 0.0009375199811173681, -0.00010690951512741344]]},
'BodyRotation': {'TimeDependentFrames': [10014, 1],
'CkTableStartTime': 297088762.24158406,
'CkTableEndTime': 297088762.9923841,
@@ -252,12 +252,12 @@ def isis_compare_dict():
[-0.8371138430875174, 0.2996946060241849, 0.1072028198209324, 0.44489449564328926],
[-0.8371114754203602, 0.2996951765357392, 0.10720122489401934, 0.44489895061910595],
[-0.8371091077303039, 0.29969574703861046, 0.10719962996461516, 0.4449034055807993]],
- 'AngularVelocity': [[6.178371695520371e-06, 4.2327129042393283e-05, 5.652013216046471e-05],
- [6.178822211046791e-06, 4.232706327946714e-05, 5.652013216046188e-05],
- [6.179272726027232e-06, 4.232699751172339e-05, 5.652013216045904e-05],
- [6.179723239999644e-06, 4.232693173922947e-05, 5.652013216045621e-05],
- [6.18017375357995e-06, 4.2326865961895454e-05, 5.6520132160453345e-05],
- [6.180624266306148e-06, 4.2326800179788824e-05, 5.6520132160450506e-05]]},
+ 'AngularVelocity': [[3.16238646979841e-05, -2.880432898124293e-05, 5.6520131658726165e-05],
+ [3.1623864697983686e-05, -2.880432898124763e-05, 5.652013165872402e-05],
+ [3.162386469798325e-05, -2.880432898125237e-05, 5.652013165872185e-05],
+ [3.162386469798283e-05, -2.880432898125708e-05, 5.6520131658719694e-05],
+ [3.1623864697982405e-05, -2.8804328981261782e-05, 5.6520131658717505e-05],
+ [3.162386469798195e-05, -2.88043289812665e-05, 5.652013165871536e-05]]},
'InstrumentPosition': {'SpkTableStartTime': 297088762.24158406,
'SpkTableEndTime': 297088762.9923841,
'SpkTableOriginalSize': 6,
diff --git a/tests/pytests/test_voyager_drivers.py b/tests/pytests/test_voyager_drivers.py
index df42e77ade99b597c04ca8aef01e2e6443846866..1ecb2c37bb71a3eac5f25146c71999e259abc72f 100644
--- a/tests/pytests/test_voyager_drivers.py
+++ b/tests/pytests/test_voyager_drivers.py
@@ -8,94 +8,303 @@ import numpy as np
import spiceypy as spice
import ale
-from ale.drivers.mro_drivers import MroCtxPds3LabelNaifSpiceDriver, MroCtxIsisLabelNaifSpiceDriver, MroCtxIsisLabelIsisSpiceDriver
from conftest import get_image_kernels, convert_kernels, get_image_label, compare_dicts
-@pytest.fixture()
-def isis_compare_dict():
- return {
- 'CameraVersion': 1,
- 'NaifKeywords': {
- "BODY502_RADII": [1564.13, 1561.23, 1560.93],
- "BODY_FRAME_CODE": 10024,
- "BODY_CODE": 502,
- "FRAME_-32101_CLASS_ID": -32101.0,
- "TKFRAME_-32101_AXES": [1.0,2.0,3.0],
- "TKFRAME_-32101_SPEC": "ANGLES",
- "INS-32101_CK_REFERENCE_ID": 2.0,
- "TKFRAME_-32101_ANGLES": [0.0,0.0,0.0],
- "FRAME_-32101_CENTER": -32.0,
- "INS-32101_PLATFORM_ID": -32001.0,
- "TKFRAME_-32101_RELATIVE": "VG2_SCAN_PLATFORM",
- "INS-32101_FOCAL_LENGTH": 1503.49,
- "INS-32101_TRANSX": [0.0,0.011789473651194,0.0],
- "FRAME_-32101_CLASS": 4.0,
- "INS-32101_TRANSY": [0.0,0.0,0.011789473651194],
- "INS-32101_BORESIGHT": [0.0,0.0,1.0],
- "INS-32101_PIXEL_PITCH": 0.011789473651194,
- "INS-32101_FOV_SHAPE": "RECTANGLE",
- "INS-32101_ITRANSL": [0.0,0.0,84.8214288089711],
- "INS-32101_ITRANSS": [0.0,84.8214288089711,0.0],
- "INS-32101_FOV_BOUNDARY_CORNERS": [0.003700098,0.003700098,1.0,-0.003700098,0.003700098,1.0,-0.003700098,-0.003700098,1.0,0.003700098],
- "INS-32101_CK_FRAME_ID": -32100.0,
- "TKFRAME_-32101_UNITS": "DEGREES",
- "INS-32101_FOV_FRAME": "VG2_ISSNA",
- "INS-32101_CK_TIME_TOLERANCE": 2000.0,
- "INS-32101_SPK_TIME_BIAS": 0.0,
- "INS-32101_CK_TIME_BIAS": 0.0,
- "FRAME_-32101_NAME": "VG2_ISSNA",
- "BODY502_POLE_RA": [268.08,-0.009,0.0],
- "BODY502_NUT_PREC_DEC": [0.0,0.0,0.0,0.468,0.026,0.007,0.002],
- "BODY502_POLE_DEC": [64.51,0.003,0.0],
- "BODY502_NUT_PREC_PM": [0.0,0.0,0.0,-0.98,-0.054,-0.014,-0.008],
- "BODY502_LONG_AXIS": 0.0,
- "BODY502_PM": [36.022,101.3747235,0.0],
- "BODY502_NUT_PREC_RA": [0.0,0.0,0.0,1.086,0.06,0.015,0.009]
- },
- 'InstrumentPointing': {'TimeDependentFrames': [-32100, 2, 1],
- 'ConstantFrames': [-32101, -32100],
- 'ConstantRotation': (1.0, 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 0.0, 1.0),
- 'CkTableStartTime': -646346832.89712,
- 'CkTableEndTime': -646346832.89712,
- 'CkTableOriginalSize': 1,
- 'EphemerisTimes': [-646346832.89712],
- 'Quaternions': [[0.34057881936764,0.085849252725072,0.69748691965044,-0.62461825983655]],
- 'AngularVelocity': [[0.0, 0.0, 0.0]]},
- 'BodyRotation': {'TimeDependentFrames': [10024, 1],
- 'CkTableStartTime': -646346832.89712,
- 'CkTableEndTime': -646346832.89712,
- 'CkTableOriginalSize': 1,
- 'EphemerisTimes': [-646346832.89712],
- 'Quaternions': [[-0.029536576144092695, 0.010097306192904288, 0.22183794661925513, -0.9745837883512549]],
- 'AngularVelocity': [[-6.713536787324419e-07, -8.842601122842458e-06, 1.845852958470088e-05]]},
- 'InstrumentPosition': {'SpkTableStartTime': -646346832.89712,
- 'SpkTableEndTime': -646346832.89712,
- 'SpkTableOriginalSize': 1,
- 'EphemerisTimes': [-646346832.89712],
- 'Positions': [[133425.48293894,184605.07752753,-3162.2190909154]],
- 'Velocities': [[-10.722770423744,2.0367821121285,-0.64314600586812]]},
- 'SunPosition': {'SpkTableStartTime': -646346832.8971245,
- 'SpkTableEndTime': -646346832.8971245,
- 'SpkTableOriginalSize': 1,
- 'EphemerisTimes': [-646346832.8971245],
- 'Positions': [[588004836.49532,-489060608.67696,-224000895.4511]],
- 'Velocities': [[9.1115543713942,-4.4506204607189,-2.785930492615]]}}
+image_dict = {
+ # Voyager 2 NAC
+ 'c2065022': {
+ 'isis': {
+ 'CameraVersion': 1,
+ 'NaifKeywords': {'BODY502_RADII': [1564.13, 1561.23, 1560.93],
+ 'BODY502_POLE_RA': [268.08,-0.009,0.0],
+ 'BODY502_NUT_PREC_DEC': [0.0,0.0,0.0,0.468,0.026,0.007,0.002],
+ 'BODY502_POLE_DEC': [64.51,0.003,0.0],
+ 'BODY502_NUT_PREC_PM': [0.0,0.0,0.0,-0.98,-0.054,-0.014,-0.008],
+ 'BODY502_LONG_AXIS': 0.0,
+ 'BODY502_PM': [36.022,101.3747235,0.0],
+ 'BODY502_NUT_PREC_RA': [0.0,0.0,0.0,1.086,0.06,0.015,0.009],
+ 'BODY_FRAME_CODE': 10024,
+ 'BODY_CODE': 502,
+ 'FRAME_-32101_CLASS_ID': -32101.0,
+ 'TKFRAME_-32101_AXES': [1.0, 2.0, 3.0],
+ 'TKFRAME_-32101_SPEC': 'ANGLES',
+ 'INS-32101_CK_REFERENCE_ID': 2.0,
+ 'TKFRAME_-32101_ANGLES': [0.0, 0.0, 0.0],
+ 'FRAME_-32101_CENTER': -32.0,
+ 'INS-32101_PLATFORM_ID': -32001.0,
+ 'TKFRAME_-32101_RELATIVE': 'VG2_SCAN_PLATFORM',
+ 'INS-32101_FOCAL_LENGTH': 1503.49,
+ 'INS-32101_TRANSX': [0.0, 0.011789473651194, 0.0],
+ 'FRAME_-32101_CLASS': 4.0,
+ 'INS-32101_TRANSY': [0.0, 0.0, 0.011789473651194],
+ 'INS-32101_BORESIGHT': [0.0, 0.0, 1.0],
+ 'INS-32101_PIXEL_PITCH': 0.011789473651194,
+ 'INS-32101_FOV_SHAPE': 'RECTANGLE',
+ 'INS-32101_ITRANSL': [0.0, 0.0, 84.8214288089711],
+ 'INS-32101_ITRANSS': [0.0, 84.8214288089711, 0.0],
+ 'INS-32101_FOV_BOUNDARY_CORNERS': [0.003700098, 0.003700098, 1.0, -0.003700098, 0.003700098, 1.0, -0.003700098, -0.003700098, 1.0, 0.003700098],
+ 'INS-32101_CK_FRAME_ID': -32100.0,
+ 'TKFRAME_-32101_UNITS': 'DEGREES',
+ 'INS-32101_FOV_FRAME': 'VG2_ISSNA',
+ 'INS-32101_CK_TIME_TOLERANCE': 2000.0,
+ 'INS-32101_SPK_TIME_BIAS': 0.0,
+ 'INS-32101_CK_TIME_BIAS': 0.0,
+ 'FRAME_-32101_NAME': 'VG2_ISSNA'},
+ 'InstrumentPointing': {'TimeDependentFrames': [-32100, 2, 1],
+ 'ConstantFrames': [-32101, -32100],
+ 'ConstantRotation': (1.0, 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 0.0, 1.0),
+ 'CkTableStartTime': -646346832.89712,
+ 'CkTableEndTime': -646346832.89712,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-646346832.89712],
+ 'Quaternions': [[0.34057881936764,0.085849252725072,0.69748691965044,-0.62461825983655]],
+ 'AngularVelocity' : [[0, 0, 0]]},
+ 'BodyRotation': {'TimeDependentFrames': [10024, 1],
+ 'CkTableStartTime': -646346832.89712,
+ 'CkTableEndTime': -646346832.89712,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-646346832.89712],
+ 'Quaternions': [[-0.029536576144092695, 0.010097306192904288, 0.22183794661925513, -0.9745837883512549]],
+ 'AngularVelocity' : [[-1.3462902248136902e-07, -8.86702528492048e-06, 1.8458530884981245e-05]]},
+ 'InstrumentPosition': {'SpkTableStartTime': -646346832.89712,
+ 'SpkTableEndTime': -646346832.89712,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': [-646346832.89712],
+ 'Positions': [[133425.48293894,184605.07752753,-3162.2190909154]],
+ 'Velocities': [[-10.722770423744,2.0367821121285,-0.64314600586812]]},
+ 'SunPosition': {'SpkTableStartTime': -646346832.8971245,
+ 'SpkTableEndTime': -646346832.8971245,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': [-646346832.8971245],
+ 'Positions': [[588004836.49532,-489060608.67696,-224000895.4511]],
+ 'Velocities': [[9.1115543713942,-4.4506204607189,-2.785930492615]]}}},
+ # Voyage 2 WAC
+ 'c2065801' : {
+ 'isis' : {
+ 'CameraVersion': 1,
+ 'NaifKeywords': {'BODY599_RADII': [71492.0, 71492.0, 66854.0],
+ 'BODY599_PM': [284.95, 870.536642, 0.0],
+ 'BODY599_LONG_AXIS' : 0.0,
+ 'BODY599_NUT_PREC_DEC' : [0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0],
+ 'BODY599_NUT_PREC_PM' : [0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0],
+ 'BODY599_POLE_RA' : [268.056595,-0.006499,0.0],
+ 'BODY599_POLE_DEC' : [64.495303,0.002413,0.0],
+ 'BODY599_NUT_PREC_RA': [0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0],
+ 'BODY_FRAME_CODE': 10015,
+ 'BODY_CODE': 599,
+ 'INS-32102_FOV_SHAPE': 'RECTANGLE',
+ 'INS-32102_PLATFORM_ID': -32002.0,
+ 'FRAME_-32102_CLASS': 4.0,
+ 'INS-32102_CK_REFERENCE_ID': 2.0,
+ 'INS-32102_FOV_FRAME': 'VG2_ISSWA',
+ 'FRAME_-32102_CLASS_ID': -32102.0,
+ 'TKFRAME_-32102_ANGLES': [0.171102, 0.0068, -0.0308],
+ 'FRAME_-32102_CENTER': -32.0,
+ 'INS-32102_PIXEL_PITCH': 0.0116661644275479,
+ 'TKFRAME_-32102_RELATIVE': 'VG2_SCAN_PLATFORM',
+ 'TKFRAME_-32102_UNITS': 'DEGREES',
+ 'INS-32102_CK_FRAME_ID': -32100.0,
+ 'INS-32102_TRANSX': [0.0, 0.0116661644275479, 0.0],
+ 'INS-32102_TRANSY': [0.0, 0.0, 0.0116661644275479],
+ 'INS-32102_CK_TIME_BIAS': 0.0,
+ 'INS-32102_SPK_TIME_BIAS': 0.0,
+ 'INS-32102_FOV_BOUNDARY_CORNERS': [0.02765, 0.02765, 1.0, -0.02765, 0.02765, 1.0, -0.02765, -0.02765, 1.0, 0.02765],
+ 'FRAME_-32102_NAME': 'VG2_ISSWA',
+ 'TKFRAME_-32102_AXES': [3.0, 1.0, 2.0],
+ 'TKFRAME_-32102_SPEC': 'ANGLES',
+ 'INS-32102_BORESIGHT': [0.0, 0.0, 1.0],
+ 'INS-32102_ITRANSL': [0.0, 0.0, 85.7179757931961],
+ 'INS-32102_ITRANSS': [0.0, 85.7179757931961, 0.0],
+ 'INS-32102_CK_TIME_TOLERANCE': 2000.0,
+ 'INS-32102_FOCAL_LENGTH': 200.77},
+ 'InstrumentPointing': {'TimeDependentFrames': [-32100, 2, 1],
+ 'ConstantFrames': [-32102, -32100],
+ 'ConstantRotation': [0.9999953963536, -0.0029863521854557, -5.37561379938284e-04, 0.0029862887971166, 0.99999553398688, -1.18682388856997e-04, 5.37913406593448e-04, 1.17076528958573e-04, 0.99999984847112],
+ 'CkTableStartTime': -646324849.03313,
+ 'CkTableEndTime': -646324849.03313,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-646324849.03313],
+ 'Quaternions': [[0.3495693057711,0.14569395751119,0.75146963877355,-0.54024804785301]],
+ 'AngularVelocity' : [[0, 0, 0]]},
+ 'BodyRotation': {'TimeDependentFrames': [10015, 1],
+ 'CkTableStartTime': -646324849.03313,
+ 'CkTableEndTime': -646324849.03313,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-646324849.03313],
+ 'Quaternions': [[-0.030328300733922,-6.20657627848567e-04,-0.22073570825636,0.97486181382761]],
+ 'AngularVelocity' : [[-2.5673165155352e-06,-7.56760295952808e-05,1.58716581044019e-04]]},
+ 'InstrumentPosition': {'SpkTableStartTime': -646324849.03313,
+ 'SpkTableEndTime': -646324849.03313,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': [-646324849.03313],
+ 'Positions': [[505791.09778057,503456.65486597,125565.58221925]],
+ 'Velocities': [[-15.323164993758,12.206477922116,4.8955647678902]]},
+ 'SunPosition': {'SpkTableStartTime': -646324849.03313,
+ 'SpkTableEndTime': -646324849.03313,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': [-646324849.03313],
+ 'Positions': [[588848865.61045,-488873362.10683,-223920792.29514]],
+ 'Velocities': [[8.9726279013895,8.4018607734375,3.3830218514148]]}}},
+ # Voyager 1 NAC
+ 'c1637937' : {
+ 'isis' : {
+ 'CameraVersion': 1,
+ 'NaifKeywords': {
+ 'BODY599_RADII': [71492.0, 71492.0, 66854.0],
+ 'BODY599_PM': [284.95, 870.536642, 0.0],
+ 'BODY599_LONG_AXIS' : 0.0,
+ 'BODY599_NUT_PREC_DEC' : [0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0],
+ 'BODY599_NUT_PREC_PM' : [0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0],
+ 'BODY599_POLE_RA' : [268.056595,-0.006499,0.0],
+ 'BODY599_POLE_DEC' : [64.495303,0.002413,0.0],
+ 'BODY599_NUT_PREC_RA': [0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0],
+ 'BODY_FRAME_CODE': 10015,
+ 'BODY_CODE': 599,
+ 'INS-31101_CK_REFERENCE_ID': 2.0,
+ 'INS-31101_FOV_FRAME': 'VG1_ISSNA',
+ 'FRAME_-31101_CLASS_ID': -31101.0,
+ 'FRAME_-31101_CLASS': 4.0,
+ 'INS-31101_FOCAL_LENGTH': 1500.19,
+ 'INS-31101_FOV_BOUNDARY_CORNERS': [0.003700098, 0.003700098, 1.0, -0.003700098, 0.003700098, 1.0, -0.003700098, -0.003700098, 1.0, 0.003700098],
+ 'INS-31101_SPK_TIME_BIAS': 0.0,
+ 'TKFRAME_-31101_RELATIVE': 'VG1_SCAN_PLATFORM',
+ 'INS-31101_PIXEL_PITCH': 0.0117894735849433,
+ 'TKFRAME_-31101_UNITS': 'DEGREES',
+ 'INS-31101_CK_FRAME_ID': -31100.0,
+ 'TKFRAME_-31101_ANGLES': [0.0, 0.0, 0.0],
+ 'INS-31101_BORESIGHT': [0.0, 0.0, 1.0],
+ 'FRAME_-31101_CENTER': -31.0,
+ 'FRAME_-31101_NAME': 'VG1_ISSNA',
+ 'TKFRAME_-31101_AXES': [1.0, 2.0, 3.0],
+ 'TKFRAME_-31101_SPEC': 'ANGLES',
+ 'INS-31101_ITRANSL': [0.0, 0.0, 84.8214292856238],
+ 'INS-31101_FOV_SHAPE': 'RECTANGLE',
+ 'INS-31101_ITRANSS': [0.0, 84.8214292856238, 0.0],
+ 'INS-31101_CK_TIME_TOLERANCE': 2000.0,
+ 'INS-31101_CK_TIME_BIAS': 0.0,
+ 'INS-31101_TRANSX': [0.0, 0.0117894735849433, 0.0],
+ 'INS-31101_TRANSY': [0.0, 0.0, 0.0117894735849433],
+ 'INS-31101_PLATFORM_ID': -31001.0
+ },
+ 'InstrumentPointing': {'TimeDependentFrames': [-31100, 2, 1],
+ 'ConstantFrames': [-31101, -31100],
+ 'ConstantRotation': [1.0, 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 0.0, 1.0],
+ 'CkTableStartTime': -657272652.12756,
+ 'CkTableEndTime': -657272652.12756,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-657272652.12756],
+ 'Quaternions': [[0.72031433366582,0.41050497282467,0.50142106290735,-0.24740623612725]],
+ 'AngularVelocity' : [[0, 0, 0]]},
+ 'BodyRotation': {'TimeDependentFrames': [10015, 1],
+ 'CkTableStartTime': -657272652.12756,
+ 'CkTableEndTime': -657272652.12756,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-657272652.12756],
+ 'Quaternions': [[-0.94178424117164,0.21107549573449,-0.06459036849449,0.25360927127957]],
+ 'AngularVelocity' : [[-2.56727928293352e-06,-7.56761359620731e-05,1.58716530917873e-04]]},
+ 'InstrumentPosition': {'SpkTableStartTime': -657272652.12756,
+ 'SpkTableEndTime': -657272652.12756,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': [-657272652.12756],
+ 'Positions': [[621054.17544251,-237768.22251899,-133459.63687226]],
+ 'Velocities': [[-9.0157282204086,18.601529664095,7.8879197923768]]},
+ 'SunPosition': {'SpkTableStartTime': -657272652.12756,
+ 'SpkTableEndTime': -657272652.12756,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': [-657272652.12756],
+ 'Positions': [[481854496.7487,-572645660.67701,-257224015.26585]],
+ 'Velocities': [[10.526843107335,6.8566245058164,2.6826355466889]]}}},
+ # Voyager 1 WAC
+ 'c1638610' : {
+ 'isis' : {
+ 'CameraVersion': 1,
+ 'NaifKeywords': {
+ 'BODY599_RADII': [71492.0, 71492.0, 66854.0],
+ 'BODY599_PM': [284.95, 870.536642, 0.0],
+ 'BODY599_LONG_AXIS' : 0.0,
+ 'BODY599_NUT_PREC_DEC' : [0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0],
+ 'BODY599_NUT_PREC_PM' : [0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0],
+ 'BODY599_POLE_RA' : [268.056595,-0.006499,0.0],
+ 'BODY599_POLE_DEC' : [64.495303,0.002413,0.0],
+ 'BODY599_NUT_PREC_RA': [0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0],
+ 'BODY_FRAME_CODE': 10015,
+ 'BODY_CODE': 599,
+ 'INS-31102_CK_REFERENCE_ID': 2.0,
+ 'INS-31102_BORESIGHT': [0.0, 0.0, 1.0],
+ 'INS-31102_ITRANSL': [0.0, 0.0, 84.74864939016786],
+ 'INS-31102_ITRANSS': [0.0, 84.74864939016786, 0.0],
+ 'TKFRAME_-31102_UNITS': 'DEGREES',
+ 'INS-31102_FOV_BOUNDARY_CORNERS': [0.02765, 0.02765, 1.0, -0.02765, 0.02765, 1.0, -0.02765, -0.02765, 1.0, 0.02765],
+ 'INS-31102_TRANSX': [0.0, 0.0117995980726038, 0.0],
+ 'INS-31102_TRANSY': [0.0, 0.0, 0.0117995980726038],
+ 'INS-31102_PIXEL_PITCH': 0.0117995980726038,
+ 'INS-31102_FOV_SHAPE': 'RECTANGLE',
+ 'FRAME_-31102_CLASS_ID': -31102.0,
+ 'INS-31102_CK_FRAME_ID': -31100.0,
+ 'FRAME_-31102_NAME': 'VG1_ISSWA',
+ 'TKFRAME_-31102_RELATIVE': 'VG1_SCAN_PLATFORM',
+ 'INS-31102_FOV_FRAME': 'VG1_ISSWA',
+ 'TKFRAME_-31102_AXES': [3.0, 1.0, 2.0],
+ 'TKFRAME_-31102_SPEC': 'ANGLES',
+ 'INS-31102_CK_TIME_BIAS': 0.0,
+ 'FRAME_-31102_CLASS': 4.0,
+ 'INS-31102_CK_TIME_TOLERANCE': 2000.0,
+ 'INS-31102_FOCAL_LENGTH': 200.465,
+ 'INS-31102_PLATFORM_ID': -31002.0,
+ 'TKFRAME_-31102_ANGLES': [0.275, -0.0247, 0.0315],
+ 'FRAME_-31102_CENTER': -31.0,
+ 'INS-31102_SPK_TIME_BIAS': 0.0
+ },
+ 'InstrumentPointing': {'TimeDependentFrames': [-31100, 2, 1],
+ 'ConstantFrames': [-31102, -31100],
+ 'ConstantRotation': [0.9999883294118, -0.0047998732944479, 5.49778635595958e-04, 0.0047996365689827, 0.99998838875498, 4.31096311889819e-04, -5.51841459656287e-04, -4.28452543098038e-04, 0.99999975594968],
+ 'CkTableStartTime': -657253835.36655,
+ 'CkTableEndTime': -657253835.36655,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-657253835.36655],
+ 'Quaternions': [[0.46307604735879,0.24654067983613,0.71505811639587,-0.4620283083588]],
+ 'AngularVelocity' : [[0, 0, 0]]},
+ 'BodyRotation': {'TimeDependentFrames': [10015, 1],
+ 'CkTableStartTime': -657253835.36655,
+ 'CkTableEndTime': -657253835.36655,
+ 'CkTableOriginalSize': 1,
+ 'EphemerisTimes': [-657253835.36655],
+ 'Quaternions': [[-0.33145588393446,0.082010450701863,0.2049367374262,-0.91728524278656]],
+ 'AngularVelocity' : [[-2.56727935591209e-06,-7.56761357895015e-05,1.58716530998994e-04]]},
+ 'InstrumentPosition': {'SpkTableStartTime': -657253835.36655,
+ 'SpkTableEndTime': -657253835.36655,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': [-657253835.36655],
+ 'Positions': [[383694.55065317,122950.66054569,23540.017308183]],
+ 'Velocities': [[-17.802074028598,18.817691029493,8.540401625345]]},
+ 'SunPosition': {'SpkTableStartTime': -657253835.36655,
+ 'SpkTableEndTime': -657253835.36655,
+ 'SpkTableOriginalSize': 1,
+ 'EphemerisTimes': [-657253835.36655],
+ 'Positions': [[482052551.97723,-572516618.3529,-257173526.65669]],
+ 'Velocities': [[10.524141391076,6.8590005124774,2.6836839348482]]}}}}
@pytest.fixture(scope='module')
def test_kernels():
- kernels = get_image_kernels('c2065022')
- updated_kernels, binary_kernels = convert_kernels(kernels)
+ updated_kernels = {}
+ binary_kernels = {}
+ for image in image_dict.keys():
+ kernels = get_image_kernels(image)
+ updated_kernels[image], binary_kernels[image] = convert_kernels(kernels)
yield updated_kernels
- for kern in binary_kernels:
- os.remove(kern)
+ for kern_list in binary_kernels.values():
+ for kern in kern_list:
+ os.remove(kern)
@pytest.mark.parametrize("label_type", ['isis3'])
@pytest.mark.parametrize("formatter", ['isis'])
-def test_voyager_load(test_kernels, label_type, formatter, isis_compare_dict):
- label_file = get_image_label('c2065022', label_type)
+@pytest.mark.parametrize("image", image_dict.keys())
+def test_voyager_load(test_kernels, label_type, formatter, image):
+ label_file = get_image_label(image, label_type)
- usgscsm_isd_str = ale.loads(label_file, props={'kernels': test_kernels}, formatter=formatter)
+ usgscsm_isd_str = ale.loads(label_file, props={'kernels': test_kernels[image]}, formatter=formatter)
usgscsm_isd_obj = json.loads(usgscsm_isd_str)
print(json.dumps(usgscsm_isd_obj, indent=2))
- assert compare_dicts(usgscsm_isd_obj, isis_compare_dict) == []
+
+ assert compare_dicts(usgscsm_isd_obj, image_dict[image][formatter]) == []