diff --git a/ale/drivers/__init__.py b/ale/drivers/__init__.py
index dbb2609c2187acba56264efb50fba1e92e1499d0..a9bc1f89aa1bc9405924211b57a672cf7800fd8a 100644
--- a/ale/drivers/__init__.py
+++ b/ale/drivers/__init__.py
@@ -26,8 +26,7 @@ from abc import ABC
__disabled_drivers__ = ["ody_drivers",
"hayabusa2_drivers",
"juno_drivers",
- "tgo_drivers",
- "msi_drivers"]
+ "tgo_drivers"]
# dynamically load drivers
__all__ = [os.path.splitext(os.path.basename(d))[0] for d in glob(os.path.join(os.path.dirname(__file__), '*_drivers.py'))]
diff --git a/ale/drivers/msi_drivers.py b/ale/drivers/msi_drivers.py
index bd58647641fbabfb18408e63ec4fa6947f65d299..edafe7e3e59a58ec2e1d8bd4a053174a76cd3602 100644
--- a/ale/drivers/msi_drivers.py
+++ b/ale/drivers/msi_drivers.py
@@ -29,6 +29,10 @@ class MsiIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, NoDistortion, Dr
"""
lookup_table = {"MSI": "NEAR EARTH ASTEROID RENDEZVOUS"}
return lookup_table[super().instrument_id]
+
+ @property
+ def center_ephemeris_time(self):
+ return self.ephemeris_start_time + self.exposure_duration / 2.0
@property
def sensor_name(self):
@@ -52,41 +56,7 @@ class MsiIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, NoDistortion, Dr
: int
ISIS sensor model version
"""
- return 1
-
- @property
- def spacecraft_clock_start_count(self):
- """
- The spacecraft clock start count, frequently used to determine the start time
- of the image.
-
- Returns
- -------
- : str
- spacecraft clock start count
- """
- if "SpacecraftClockStartCount" in self.label["IsisCube"]["Instrument"]:
- return str(
- self.label["IsisCube"]["Instrument"]["SpacecraftClockStartCount"])
- else:
- return None
-
- @property
- def spacecraft_clock_stop_count(self):
- """
- The spacecraft clock stop count, frequently used to determine the stop time
- of the image.
-
- Returns
- -------
- : str
- spacecraft clock stop count
- """
- if "SpacecraftClockStopCount" in self.label["IsisCube"]["Instrument"]:
- return str(
- self.label["IsisCube"]["Instrument"]["SpacecraftClockStopCount"])
- else:
- return None
+ return 2
@property
def ikid(self):
diff --git a/tests/pytests/data/isds/msi_isd.json b/tests/pytests/data/isds/msi_isd.json
new file mode 100644
index 0000000000000000000000000000000000000000..e84dbf1226f8d9428bb2d70f9324e4abf5dd8a3c
--- /dev/null
+++ b/tests/pytests/data/isds/msi_isd.json
@@ -0,0 +1,262 @@
+{
+ "isis_camera_version": 2,
+ "image_lines": 412,
+ "image_samples": 537,
+ "name_platform": "NEAR EARTH ASTEROID RENDEZVOUS",
+ "name_sensor": "MULTI-SPECTRAL IMAGER",
+ "reference_height": {
+ "maxheight": 1000,
+ "minheight": -1000,
+ "unit": "m"
+ },
+ "name_model": "USGS_ASTRO_FRAME_SENSOR_MODEL",
+ "center_ephemeris_time": 4750816.53996159,
+ "radii": {
+ "semimajor": 17.0,
+ "semiminor": 5.5,
+ "unit": "km"
+ },
+ "body_rotation": {
+ "time_dependent_frames": [
+ 2000433,
+ 1
+ ],
+ "ck_table_start_time": 4750816.53996159,
+ "ck_table_end_time": 4750816.53996159,
+ "ck_table_original_size": 1,
+ "ephemeris_times": [
+ 4750816.53996159
+ ],
+ "quaternions": [
+ [
+ -0.21742791831046224,
+ -0.5915927720196109,
+ 0.04469058688780722,
+ -0.7750779598704606
+ ]
+ ],
+ "angular_velocities": [
+ [
+ 0.00031013516468020774,
+ 6.225262045195156e-05,
+ 9.803883131191956e-05
+ ]
+ ],
+ "reference_frame": 1
+ },
+ "instrument_pointing": {
+ "time_dependent_frames": [
+ -93000,
+ 1
+ ],
+ "ck_table_start_time": 4750816.53996159,
+ "ck_table_end_time": 4750816.53996159,
+ "ck_table_original_size": 1,
+ "ephemeris_times": [
+ 4750816.53996159
+ ],
+ "quaternions": [
+ [
+ -0.6037146505713888,
+ -0.2184429492380255,
+ 0.26555847710047836,
+ 0.7192287493237002
+ ]
+ ],
+ "angular_velocities": [
+ [
+ -1.0366620787684243e-05,
+ 2.9058844213815335e-05,
+ -8.620710132728253e-06
+ ]
+ ],
+ "reference_frame": 1,
+ "constant_frames": [
+ -93001,
+ -93000
+ ],
+ "constant_rotation": [
+ -0.0014422521585655882,
+ 6.97819591591179e-07,
+ 0.9999989599535712,
+ -0.00048384015636002327,
+ -0.9999998829493447,
+ 0.0,
+ 0.9999988429030378,
+ -0.00048383965314379655,
+ 0.0014422523273822038
+ ]
+ },
+ "naif_keywords": {
+ "BODY2000433_RADII": [
+ 17.0,
+ 5.5,
+ 5.5
+ ],
+ "BODY_FRAME_CODE": 2000433,
+ "BODY_CODE": 2000433,
+ "INS-93001_PIXEL_PITCH": 0.016,
+ "INS-93001_LT_SURFACE_CORRECT": "FALSE",
+ "INS-93001_SWAP_OBSERVER_TARGET": "TRUE",
+ "INS-93001_TRANSX": [
+ 0.0,
+ 0.016,
+ 0.0
+ ],
+ "INS-93001_TRANSY": [
+ 0.0,
+ 0.0,
+ -0.016
+ ],
+ "INS-93001_LIGHTTIME_CORRECTION": "LT+S",
+ "INS-93001_FOV_BOUNDARY_CORNERS": [
+ 1.0,
+ 0.019744857140000002,
+ 0.02575366124,
+ 1.0,
+ -0.019744857140000002,
+ 0.02575366124,
+ 1.0,
+ -0.019744857140000002,
+ -0.02575366124,
+ 1.0
+ ],
+ "TKFRAME_-93001_UNITS": "DEGREES",
+ "INS-93001_FOCAL_LENGTH": 166.85,
+ "INS-93001_FOV_FRAME": "NEAR_MSI",
+ "FRAME_-93001_NAME": "NEAR_MSI",
+ "TKFRAME_-93001_AXES": [
+ 2.0,
+ 1.0,
+ 2.0
+ ],
+ "TKFRAME_-93001_SPEC": "ANGLES",
+ "INS-93001_BORESIGHT_SAMPLE": 269.0,
+ "INS-93001_ITRANSL": [
+ 0.0,
+ 0.0,
+ -62.5
+ ],
+ "INS-93001_K1": -7e-05,
+ "INS-93001_ITRANSS": [
+ 0.0,
+ 62.5,
+ 0.0
+ ],
+ "FRAME_-93001_CLASS_ID": -93001.0,
+ "INS-93001_PLATFORM_ID": -93000.0,
+ "INS-93001_BORESIGHT_LINE": 206.5,
+ "INS-93001_FRAME_ID": -93001.0,
+ "TKFRAME_-93001_RELATIVE": "NEAR_SC_BUS_PRIME",
+ "INS-93001_BORESIGHT": [
+ 1.0,
+ 0.0,
+ 0.0
+ ],
+ "TKFRAME_-93001_ANGLES": [
+ 90.0,
+ -179.972278,
+ -0.082635
+ ],
+ "FRAME_-93001_CENTER": -93.0,
+ "FRAME_-93001_CLASS": 4.0,
+ "INS-93001_FOV_SHAPE": "POLYGON",
+ "FRAME_2000433_NAME": "EROS_FIXED",
+ "FRAME_2000433_CLASS_ID": 2000433.0,
+ "BODY2000433_POLE_DEC": [
+ 17.22,
+ 0.0,
+ 0.0
+ ],
+ "BODY2000433_PM": [
+ 326.07,
+ 1639.38864745,
+ 0.0
+ ],
+ "FRAME_2000433_CENTER": 2000433.0,
+ "BODY2000433_LONG_AXIS": 0.0,
+ "OBJECT_2000433_FRAME": "EROS_FIXED",
+ "FRAME_2000433_CLASS": 2.0,
+ "BODY2000433_POLE_RA": [
+ 11.35,
+ 0.0,
+ 0.0
+ ]
+ },
+ "detector_sample_summing": 1,
+ "detector_line_summing": 1,
+ "focal_length_model": {
+ "focal_length": 166.85
+ },
+ "detector_center": {
+ "line": 206.5,
+ "sample": 269.0
+ },
+ "focal2pixel_lines": [
+ 0.0,
+ 0.0,
+ -62.5
+ ],
+ "focal2pixel_samples": [
+ 0.0,
+ 62.5,
+ 0.0
+ ],
+ "optical_distortion": {
+ "radial": {
+ "coefficients": [
+ 0.0,
+ 0.0,
+ 0.0
+ ]
+ }
+ },
+ "starting_detector_line": 0,
+ "starting_detector_sample": 0,
+ "instrument_position": {
+ "spk_table_start_time": 4750816.53996159,
+ "spk_table_end_time": 4750816.53996159,
+ "spk_table_original_size": 1,
+ "ephemeris_times": [
+ 4750816.53996159
+ ],
+ "positions": [
+ [
+ 69.13367389282288,
+ -276.40770781355167,
+ 222.2546049363491
+ ]
+ ],
+ "velocities": [
+ [
+ 0.0007228575310681364,
+ -0.00018739946234992287,
+ -0.0005859505443755211
+ ]
+ ],
+ "reference_frame": 1
+ },
+ "sun_position": {
+ "spk_table_start_time": 4750816.53996159,
+ "spk_table_end_time": 4750816.53996159,
+ "spk_table_original_size": 1,
+ "ephemeris_times": [
+ 4750816.53996159
+ ],
+ "positions": [
+ [
+ 122682357.26743293,
+ 156146522.97922137,
+ 110874367.26208726
+ ]
+ ],
+ "velocities": [
+ [
+ -16.298773023439573,
+ 15.981064278673381,
+ 6.140837444633245
+ ]
+ ],
+ "reference_frame": 1
+ }
+}
\ No newline at end of file
diff --git a/tests/pytests/data/m0126888978f7_2p/eros_fixed.tf b/tests/pytests/data/m0126888978f7_2p/eros_fixed.tf
new file mode 100755
index 0000000000000000000000000000000000000000..fcb03eee63fcf62484bdb3796150762552c6e217
--- /dev/null
+++ b/tests/pytests/data/m0126888978f7_2p/eros_fixed.tf
@@ -0,0 +1,74 @@
+KPL/FK
+
+EROS Body-Fixed Frame Definition Kernel
+===============================================================================
+
+ This frame kernel contains asteroid EROS body-fixed frame definition.
+
+
+Version and Date
+--------------------------------------------------------
+
+ Version 1.0 -- June 18, 2002 -- Boris Semenov
+
+ Initial release.
+
+
+References
+--------------------------------------------------------
+
+ 1. ``Frames Required Reading''
+
+ 2. ``PCK Required Reading''
+
+
+Contact Information
+--------------------------------------------------------
+
+ Boris V. Semenov, NAIF/JPL, (818)-354-8136, bsemenov@spice.jpl.nasa.gov
+
+
+Implementation Notes
+--------------------------------------------------------
+
+ This file is used by the SPICE system as follows: programs that make
+ use of this frame kernel must `load' the kernel, normally during program
+ initialization. Loading the kernel associates data items with their
+ names in a data structure called the `kernel pool'. The SPICELIB
+ routine FURNSH loads a kernel file into the pool as shown below.
+
+ CALL FURNSH ( frame_kernel_name )
+
+ This file was created and may be updated with a text editor or word
+ processor.
+
+
+EROS Body-Fixed Frame
+--------------------------------------------------------
+
+ This kernel file defines asteroid EROS body-frame, EROS_FIXED, with the
+ frame ID code 2000433 in the same as any other PCK frame:
+
+ * +Z along asteroid's North pole;
+
+ * +X along asteroid's prime meridian;
+
+ * +Y complements to the right hand frame;
+
+ * the origin of this frame is at the center of the asteroid ellipsoid.
+
+ As for any PCK frame orientation of this frame is computed by evaluating
+ corresponding rotation constants provided in a PCK file.
+
+ \begindata
+
+ FRAME_EROS_FIXED = 2000433
+ FRAME_2000433_NAME = 'EROS_FIXED'
+ FRAME_2000433_CLASS = 2
+ FRAME_2000433_CLASS_ID = 2000433
+ FRAME_2000433_CENTER = 2000433
+
+ OBJECT_2000433_FRAME = 'EROS_FIXED'
+
+ \begintext
+
diff --git a/tests/pytests/data/m0126888978f7_2p/m0126888978f7_2p_isis.lbl b/tests/pytests/data/m0126888978f7_2p/m0126888978f7_2p_isis.lbl
new file mode 100644
index 0000000000000000000000000000000000000000..a2513564884b767a3c5003fd0414078039c997b4
--- /dev/null
+++ b/tests/pytests/data/m0126888978f7_2p/m0126888978f7_2p_isis.lbl
@@ -0,0 +1,360 @@
+Object = IsisCube
+ Object = Core
+ StartByte = 65537
+ Format = Tile
+ TileSamples = 179
+ TileLines = 412
+
+ Group = Dimensions
+ Samples = 537
+ Lines = 412
+ Bands = 1
+ End_Group
+
+ Group = Pixels
+ Type = Real
+ ByteOrder = Lsb
+ Base = 0.0
+ Multiplier = 1.0
+ End_Group
+ End_Object
+
+ Group = Instrument
+ SpacecraftName = "NEAR EARTH ASTEROID RENDEZVOUS"
+ InstrumentId = MSI
+ TargetName = EROS
+ StartTime = 2000-02-25T11:39:11.972
+ StopTime = 2000-02-25T11:39:12.737
+ SpacecraftClockStartCount = 126888978154
+ SpacecraftClockStopCount = 126888978919
+ ExposureDuration = 765.00 <ms>
+ OriginalSpacecraftClockStartCount = 126888978.154
+ OriginalSpacecraftClockStopCount = 126888978.919
+ DpuDeckTemperature = 286.50 <K>
+ End_Group
+
+ Group = Archive
+ DataSetId = NEAR-A-MSI-2-EDR-EROS/ORBIT-V1.0
+ ProducerFullName = "Howard W. Taylor"
+ ProductId = M0126888978F7_2P.LBL
+ ProductVersionId = 1.01
+ InstrumentHostName = "NEAR EARTH ASTEROID RENDEZVOUS"
+ InstrumentName = "MULTI-SPECTRAL IMAGER"
+ InstrumentId = MSI
+ TargetName = EROS
+ End_Group
+
+ Group = BandBin
+ FilterNumber = 7
+ Center = 1050 <nm>
+ End_Group
+
+ Group = Kernels
+ NaifFrameCode = -93001
+ LeapSecond = $base/kernels/lsk/naif0012.tls
+ TargetAttitudeShape = $base/kernels/pck/pck00009.tpc
+ TargetPosition = (Table, $base/kernels/spk/de405.bsp,
+ $near/kernels/tspk/erosephem_1999004_2002181.-
+ bsp)
+ InstrumentPointing = (Table, $near/kernels/ck/near_2000056_v01.bc,
+ $near/kernels/fk/eros_fixed.tf)
+ Instrument = $near/kernels/ik/msi15.ti
+ SpacecraftClock = $near/kernels/sclk/near_171.tsc
+ InstrumentPosition = (Table,
+ $near/kernels/spk/near_erosorbit_nav_v1.bsp)
+ InstrumentAddendum = $near/kernels/iak/msiAddendum002.ti
+ ShapeModel = Null
+ InstrumentPositionQuality = Reconstructed
+ InstrumentPointingQuality = Reconstructed
+ CameraVersion = 2
+ Source = isis
+ End_Group
+End_Object
+
+Object = Label
+ Bytes = 65536
+End_Object
+
+Object = Table
+ Name = InstrumentPointing
+ StartByte = 955685
+ Bytes = 64
+ Records = 1
+ ByteOrder = Lsb
+ TimeDependentFrames = (-93000, 1)
+ ConstantFrames = (-93001, -93000)
+ ConstantRotation = (-0.0014422521585655, 6.97819591591201e-07,
+ 0.99999895995357, -4.83840156360023e-04,
+ -0.99999988294934, 2.96266649392629e-20,
+ 0.99999884290304, -4.83839653143796e-04,
+ 0.0014422523273821)
+ CkTableStartTime = 4750816.5399616
+ CkTableEndTime = 4750816.5399616
+ CkTableOriginalSize = 1
+ FrameTypeCode = 3
+ Description = "Created by spiceinit"
+ Kernels = ($near/kernels/ck/near_2000056_v01.bc,
+ $near/kernels/fk/eros_fixed.tf)
+
+ Group = Field
+ Name = J2000Q0
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q1
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q2
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q3
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV1
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV2
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV3
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = ET
+ Type = Double
+ Size = 1
+ End_Group
+End_Object
+
+Object = Table
+ Name = InstrumentPosition
+ StartByte = 955749
+ Bytes = 56
+ Records = 1
+ ByteOrder = Lsb
+ CacheType = Linear
+ SpkTableStartTime = 4750816.5399616
+ SpkTableEndTime = 4750816.5399616
+ SpkTableOriginalSize = 1.0
+ Description = "Created by spiceinit"
+ Kernels = $near/kernels/spk/near_erosorbit_nav_v1.bsp
+
+ Group = Field
+ Name = J2000X
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Y
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Z
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000XV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000YV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000ZV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = ET
+ Type = Double
+ Size = 1
+ End_Group
+End_Object
+
+Object = Table
+ Name = BodyRotation
+ StartByte = 955805
+ Bytes = 64
+ Records = 1
+ ByteOrder = Lsb
+ TimeDependentFrames = (2000433, 1)
+ CkTableStartTime = 4750816.5399616
+ CkTableEndTime = 4750816.5399616
+ CkTableOriginalSize = 1
+ FrameTypeCode = 2
+ PoleRa = (11.35, 0.0, 0.0)
+ PoleDec = (17.22, 0.0, 0.0)
+ PrimeMeridian = (326.07, 1639.38864745, 0.0)
+ Description = "Created by spiceinit"
+ Kernels = ($base/kernels/spk/de405.bsp,
+ $near/kernels/tspk/erosephem_1999004_2002181.bsp,
+ $base/kernels/pck/pck00009.tpc)
+ SolarLongitude = 128.86157495957
+
+ Group = Field
+ Name = J2000Q0
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q1
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q2
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Q3
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV1
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV2
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = AV3
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = ET
+ Type = Double
+ Size = 1
+ End_Group
+End_Object
+
+Object = Table
+ Name = SunPosition
+ StartByte = 955869
+ Bytes = 56
+ Records = 1
+ ByteOrder = Lsb
+ CacheType = Linear
+ SpkTableStartTime = 4750816.5399616
+ SpkTableEndTime = 4750816.5399616
+ SpkTableOriginalSize = 1.0
+ Description = "Created by spiceinit"
+ Kernels = ($base/kernels/spk/de405.bsp,
+ $near/kernels/tspk/erosephem_1999004_2002181.bsp)
+
+ Group = Field
+ Name = J2000X
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Y
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000Z
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000XV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000YV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = J2000ZV
+ Type = Double
+ Size = 1
+ End_Group
+
+ Group = Field
+ Name = ET
+ Type = Double
+ Size = 1
+ End_Group
+End_Object
+
+Object = History
+ Name = IsisCube
+ StartByte = 955925
+ Bytes = 2374
+End_Object
+
+Object = OriginalLabel
+ Name = IsisCube
+ StartByte = 950513
+ Bytes = 3700
+End_Object
+
+Object = NaifKeywords
+ BODY_CODE = 2000433
+ BODY2000433_RADII = (17.0, 5.5, 5.5)
+ BODY_FRAME_CODE = 2000433
+ INS-93001_SWAP_OBSERVER_TARGET = TRUE
+ INS-93001_LIGHTTIME_CORRECTION = LT+S
+ INS-93001_LT_SURFACE_CORRECT = FALSE
+ INS-93001_FOCAL_LENGTH = 166.85
+ INS-93001_PIXEL_PITCH = 0.016
+ CLOCK_ET_-93_126888978154_COMPUTED = c7d9130a781f5241
+ INS-93001_TRANSX = (0.0, 0.016, 0.0)
+ INS-93001_TRANSY = (0.0, 0.0, -0.016)
+ INS-93001_ITRANSS = (0.0, 62.5, 0.0)
+ INS-93001_ITRANSL = (0.0, 0.0, -62.5)
+ INS-93001_BORESIGHT_LINE = 206.5
+ INS-93001_BORESIGHT_SAMPLE = 269.0
+ INS-93001_K1 = -7.0e-05
+End_Object
+End
diff --git a/tests/pytests/data/m0126888978f7_2p/m0126888978f7_2p_isis_0.xsp b/tests/pytests/data/m0126888978f7_2p/m0126888978f7_2p_isis_0.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..f52c440444c2816ad86552272e50ae69f9e28d61
--- /dev/null
+++ b/tests/pytests/data/m0126888978f7_2p/m0126888978f7_2p_isis_0.xsp
@@ -0,0 +1,349 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 39
+'DE-0405LE-0405 '
+'487A6E6327010C^6'
+'487B62498D6844^6'
+'A'
+'0'
+'1'
+'2'
+39
+'3E9F4^6'
+'A8C^5'
+'-FAF69711F973F^5'
+'1B040790EAA859^4'
+'1407735D138EB7^2'
+'-1C20EE357141B5^0'
+'161DB0AB0D6AB9^-1'
+'D16B8E75BB4C88^-2'
+'-E1B788935BE38^-3'
+'-523DC685402F08^-3'
+'9AF1A80B8ABE7^-4'
+'20C0065140191^-4'
+'-607B5E5BE58EC8^-5'
+'-6C19BA5393A91^5'
+'-1E01120F14F486^4'
+'114AABF00A32C3^2'
+'-97244237F78F78^-1'
+'-46B12B2249A62^-1'
+'445226BFA96264^-2'
+'1C5AB705F8B5AE^-2'
+'-2DA28246DA3F72^-3'
+'-B433317744DE6^-4'
+'1C06E7FE23256A^-4'
+'466CBC4A90F1B^-5'
+'-26D9CBBF3263F4^5'
+'-D8C6F8590CCCE^3'
+'6E5DBF15D8D208^1'
+'-21774C66C920CE^-1'
+'-287BBA70012978^-1'
+'E82D54CC40BF9^-3'
+'109D18E9E8BAFF^-2'
+'-FD8B11B750906^-4'
+'-7053530533B69^-4'
+'B92EA3F7F02DD8^-5'
+'2FA05C53CAF6A4^-5'
+'34134^6'
+'1518^6'
+'23^2'
+'1^1'
+END_ARRAY 1 39
+BEGIN_ARRAY 2 88
+'asteroid segment '
+'487A6E6327010C^6'
+'487B62498D6844^6'
+'1E8631'
+'A'
+'1'
+'E'
+88
+'B^1'
+'48698^6'
+'487D08^6'
+'1388^4'
+'-74FD1221EB8FC4^7'
+'13E592649BA652^5'
+'8A625440CDA^1'
+'-5F00BAA8^-2'
+'1009F^-5'
+'1CF8^-6'
+'B5D4^-6'
+'-4314^-6'
+'DD1B8^-6'
+'-2BE48^-6'
+'5243E^-6'
+'-94EB29DBB4C5C8^7'
+'-1381D21A85F599^5'
+'B027F74AC9E^1'
+'1480EFA2^-2'
+'-1D2D2^-5'
+'2FDA^-6'
+'F796^-6'
+'-1C7C8^-6'
+'14869^-5'
+'-29BDA^-6'
+'233FB^-6'
+'-69BD47D07BD478^7'
+'-77ED36A0B0CBF8^4'
+'7D14E4DD898^1'
+'-57DD166^-3'
+'-FC7C^-6'
+'1288^-6'
+'A6C3^-6'
+'-3081^-6'
+'B703^-6'
+'-44C5C^-6'
+'3C843^-6'
+'104CA761B9E9BD^2'
+'1C574FF9DC609^-1'
+'-1D2F64C7ED2C^-4'
+'7F2595E8^-8'
+'5DE^-C'
+'-2D38^-C'
+'-E9F^-C'
+'7C19^-C'
+'-214E9^-B'
+'52A14^-C'
+'1D6B6^-C'
+'-FFAF01921E46^1'
+'2413A75E2801F4^-1'
+'64C617CE33C^-5'
+'-A1EB596^-8'
+'55C04^-B'
+'211E^-C'
+'18A2C^-B'
+'-3C85^-C'
+'17C23^-B'
+'-4698C^-C'
+'47866^-C'
+'-623E6F28B05E68^1'
+'199DE10C19123B^-1'
+'-1AFEB28D592^-5'
+'-450BD7E4^-8'
+'34B7C^-B'
+'1C33^-C'
+'69E8^-C'
+'69^-E'
+'7B46^-C'
+'-9FA2^-D'
+'-B88D^-D'
+'48698^6'
+'0^0'
+'1^1'
+'47^2'
+'0^0'
+'3^1'
+'46^2'
+'1^1'
+'0^0'
+'0^0'
+'0^0'
+'1^1'
+'1^1'
+'0^0'
+'0^0'
+'44^2'
+'1^1'
+'11^2'
+END_ARRAY 2 88
+BEGIN_ARRAY 3 158
+'spacecraft segment '
+'487A6E6327010C^6'
+'487B62498D6844^6'
+'-5D'
+'1E8631'
+'1'
+'E'
+158
+'B^1'
+'487858^6'
+'4879CF^6'
+'177^3'
+'4460B277530A44^2'
+'45753A545BB1^0'
+'-18B7B5782^-3'
+'-4C800D8^-6'
+'-1CC8^-9'
+'18DC^-9'
+'3^-B'
+'8^-B'
+'-9E^-B'
+'67^-B'
+'-C38^-B'
+'-1143349C17F348^3'
+'-123E4EEDC066^0'
+'5F2C6C21A^-3'
+'305588^-6'
+'14B4^-8'
+'-1D2^-9'
+'F7^-A'
+'82^-A'
+'934^-A'
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+'32^-A'
+'DEDAEF1E4A1048^2'
+'-380A31E7DC88^0'
+'-4E9A085FA^-3'
+'23188C^-6'
+'-7973^-8'
+'79^-A'
+'-398^-A'
+'-248^-A'
+'-304^-A'
+'82^-B'
+'-10E^-A'
+'2F6AA62F07459^-2'
+'-437EDDB1ED^-5'
+'-1394D291B8^-7'
+'-92DC68^-B'
+'B28F24^-B'
+'DC918^-C'
+'9BDDE^-C'
+'611B6^-C'
+'3C18A^-C'
+'172228^-C'
+'B8C8E^-D'
+'-C7443261246658^-3'
+'103E3258D9734^-4'
+'C5F3FAEA4^-8'
+'7D26F63^-A'
+'-41D9A5^-B'
+'C3C85D^-B'
+'8ED6598^-B'
+'5833CA^-B'
+'369A014^-B'
+'1500048^-B'
+'A80272^-C'
+'-2641AB01121EFA^-2'
+'-D6A2BA088B0C^-5'
+'8FC27561^-8'
+'-29A390E^-9'
+'135E2^-B'
+'-293866^-B'
+'-238044^-B'
+'-15ED5^-B'
+'-D9237^-C'
+'-53889C^-C'
+'-29C0C2^-C'
+'487B46^6'
+'487CBD^6'
+'177^3'
+'44EB9084CBE57C^2'
+'4568D02A8DC2^0'
+'-18F0D7DA2^-3'
+'-4B9B578^-6'
+'1A378^-8'
+'15C4^-9'
+'-B4^-B'
+'-18^-B'
+'-C8^-B'
+'3C8^-B'
+'-8AC^-B'
+'-1145796C1DBCA4^3'
+'-120EAF801708^0'
+'5F517AB78^-3'
+'319E16^-6'
+'-2562^-8'
+'-2FE^-9'
+'5^-B'
+'-58^-B'
+'D4^-B'
+'-12E^-A'
+'15C^-A'
+'DE6AB3724FD8C^2'
+'-383178D94064^0'
+'-4E8286F74^-3'
+'1C035A^-6'
+'-5728^-8'
+'212^-9'
+'-E8^-B'
+'2^-B'
+'-2F8^-A'
+'E4^-B'
+'-226^-A'
+'2F622C908FB124^-2'
+'-441AD7F54498^-5'
+'-135A64566^-7'
+'8EDBF4C^-A'
+'929EA8^-B'
+'-2F444^-C'
+'-10E64^-C'
+'-9B3A^-D'
+'-609A^-D'
+'-24B2^-D'
+'-12A86^-D'
+'-C53C074F159E68^-3'
+'10448418ADFD^-4'
+'CB24E2B8A^-8'
+'-CE21275^-A'
+'-16503EC^-A'
+'-215303^-B'
+'-19A7168^-B'
+'-FF3D2^-C'
+'-9DFDD4^-C'
+'-3CC4EA^-C'
+'-1E61E7^-C'
+'-265C7B3C30F68A^-2'
+'-D6627EA16F9^-5'
+'72CC54888^-8'
+'-1DC1460C^-9'
+'E360D8^-B'
+'8632E^-C'
+'1894C^-C'
+'102AE^-C'
+'A0EB^-D'
+'3DB0C^-D'
+'1F152^-D'
+'487858^6'
+'487B46^6'
+'0^0'
+'1^1'
+'8D^2'
+'0^0'
+'3^1'
+'8B^2'
+'2^1'
+'0^0'
+'0^0'
+'0^0'
+'1^1'
+'2^1'
+'0^0'
+'0^0'
+'44^2'
+'1^1'
+'11^2'
+END_ARRAY 3 158
+TOTAL_ARRAYS 3
+ ~NAIF/SPC BEGIN COMMENTS~
+; ../sliced_kernels/m0126888978f7_2p_isis_0.bsp LOG FILE
+
+; Created 2024-03-04/14:19:21.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /Volumes/Blueman_2/isis_data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = ../sliced_kernels/m0126888978f7_2p_isis_0.bsp
+ SOURCE_SPK_KERNEL = /Volumes/Blueman_2/isis_data/base/kernels/spk/de405.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 10
+ BEGIN_TIME = 2000 FEB 25 11:24:30.202
+ END_TIME = 2000 FEB 25 11:28:34.102
+SOURCE_SPK_KERNEL = /Volumes/Blueman_2/isis_data/near/kernels/tspk/erosephem_1999004_2002181.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 2000433
+ BEGIN_TIME = 2000 FEB 25 11:24:30.202
+ END_TIME = 2000 FEB 25 11:28:34.102
+SOURCE_SPK_KERNEL = /Volumes/Blueman_2/isis_data/near/kernels/spk/near_erosorbit_nav_v1.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -93
+ BEGIN_TIME = 2000 FEB 25 11:24:30.202
+ END_TIME = 2000 FEB 25 11:28:34.102
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/m0126888978f7_2p/m0126888978f7_2p_isis_1.xsp b/tests/pytests/data/m0126888978f7_2p/m0126888978f7_2p_isis_1.xsp
new file mode 100644
index 0000000000000000000000000000000000000000..f6757b32596fb9cf351b51fd4854591228605f2c
--- /dev/null
+++ b/tests/pytests/data/m0126888978f7_2p/m0126888978f7_2p_isis_1.xsp
@@ -0,0 +1,349 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE '
+BEGIN_ARRAY 1 39
+'DE-0405LE-0405 '
+'487D682845BC08^6'
+'487E58EC1CC718^6'
+'A'
+'0'
+'1'
+'2'
+39
+'3E9F4^6'
+'A8C^5'
+'-FAF69711F973F^5'
+'1B040790EAA859^4'
+'1407735D138EB7^2'
+'-1C20EE357141B5^0'
+'161DB0AB0D6AB9^-1'
+'D16B8E75BB4C88^-2'
+'-E1B788935BE38^-3'
+'-523DC685402F08^-3'
+'9AF1A80B8ABE7^-4'
+'20C0065140191^-4'
+'-607B5E5BE58EC8^-5'
+'-6C19BA5393A91^5'
+'-1E01120F14F486^4'
+'114AABF00A32C3^2'
+'-97244237F78F78^-1'
+'-46B12B2249A62^-1'
+'445226BFA96264^-2'
+'1C5AB705F8B5AE^-2'
+'-2DA28246DA3F72^-3'
+'-B433317744DE6^-4'
+'1C06E7FE23256A^-4'
+'466CBC4A90F1B^-5'
+'-26D9CBBF3263F4^5'
+'-D8C6F8590CCCE^3'
+'6E5DBF15D8D208^1'
+'-21774C66C920CE^-1'
+'-287BBA70012978^-1'
+'E82D54CC40BF9^-3'
+'109D18E9E8BAFF^-2'
+'-FD8B11B750906^-4'
+'-7053530533B69^-4'
+'B92EA3F7F02DD8^-5'
+'2FA05C53CAF6A4^-5'
+'34134^6'
+'1518^6'
+'23^2'
+'1^1'
+END_ARRAY 1 39
+BEGIN_ARRAY 2 88
+'asteroid segment '
+'487D682845BC08^6'
+'487E58EC1CC718^6'
+'1E8631'
+'A'
+'1'
+'E'
+88
+'B^1'
+'48698^6'
+'487D08^6'
+'1388^4'
+'-74FD1221EB8FC4^7'
+'13E592649BA652^5'
+'8A625440CDA^1'
+'-5F00BAA8^-2'
+'1009F^-5'
+'1CF8^-6'
+'B5D4^-6'
+'-4314^-6'
+'DD1B8^-6'
+'-2BE48^-6'
+'5243E^-6'
+'-94EB29DBB4C5C8^7'
+'-1381D21A85F599^5'
+'B027F74AC9E^1'
+'1480EFA2^-2'
+'-1D2D2^-5'
+'2FDA^-6'
+'F796^-6'
+'-1C7C8^-6'
+'14869^-5'
+'-29BDA^-6'
+'233FB^-6'
+'-69BD47D07BD478^7'
+'-77ED36A0B0CBF8^4'
+'7D14E4DD898^1'
+'-57DD166^-3'
+'-FC7C^-6'
+'1288^-6'
+'A6C3^-6'
+'-3081^-6'
+'B703^-6'
+'-44C5C^-6'
+'3C843^-6'
+'104CA761B9E9BD^2'
+'1C574FF9DC609^-1'
+'-1D2F64C7ED2C^-4'
+'7F2595E8^-8'
+'5DE^-C'
+'-2D38^-C'
+'-E9F^-C'
+'7C19^-C'
+'-214E9^-B'
+'52A14^-C'
+'1D6B6^-C'
+'-FFAF01921E46^1'
+'2413A75E2801F4^-1'
+'64C617CE33C^-5'
+'-A1EB596^-8'
+'55C04^-B'
+'211E^-C'
+'18A2C^-B'
+'-3C85^-C'
+'17C23^-B'
+'-4698C^-C'
+'47866^-C'
+'-623E6F28B05E68^1'
+'199DE10C19123B^-1'
+'-1AFEB28D592^-5'
+'-450BD7E4^-8'
+'34B7C^-B'
+'1C33^-C'
+'69E8^-C'
+'69^-E'
+'7B46^-C'
+'-9FA2^-D'
+'-B88D^-D'
+'48698^6'
+'0^0'
+'1^1'
+'47^2'
+'0^0'
+'3^1'
+'46^2'
+'1^1'
+'0^0'
+'0^0'
+'0^0'
+'1^1'
+'1^1'
+'0^0'
+'0^0'
+'44^2'
+'1^1'
+'11^2'
+END_ARRAY 2 88
+BEGIN_ARRAY 3 158
+'spacecraft segment '
+'487D682845BC08^6'
+'487E58EC1CC718^6'
+'-5D'
+'1E8631'
+'1'
+'E'
+158
+'B^1'
+'487B46^6'
+'487CBD^6'
+'177^3'
+'44EB9084CBE57C^2'
+'4568D02A8DC2^0'
+'-18F0D7DA2^-3'
+'-4B9B578^-6'
+'1A378^-8'
+'15C4^-9'
+'-B4^-B'
+'-18^-B'
+'-C8^-B'
+'3C8^-B'
+'-8AC^-B'
+'-1145796C1DBCA4^3'
+'-120EAF801708^0'
+'5F517AB78^-3'
+'319E16^-6'
+'-2562^-8'
+'-2FE^-9'
+'5^-B'
+'-58^-B'
+'D4^-B'
+'-12E^-A'
+'15C^-A'
+'DE6AB3724FD8C^2'
+'-383178D94064^0'
+'-4E8286F74^-3'
+'1C035A^-6'
+'-5728^-8'
+'212^-9'
+'-E8^-B'
+'2^-B'
+'-2F8^-A'
+'E4^-B'
+'-226^-A'
+'2F622C908FB124^-2'
+'-441AD7F54498^-5'
+'-135A64566^-7'
+'8EDBF4C^-A'
+'929EA8^-B'
+'-2F444^-C'
+'-10E64^-C'
+'-9B3A^-D'
+'-609A^-D'
+'-24B2^-D'
+'-12A86^-D'
+'-C53C074F159E68^-3'
+'10448418ADFD^-4'
+'CB24E2B8A^-8'
+'-CE21275^-A'
+'-16503EC^-A'
+'-215303^-B'
+'-19A7168^-B'
+'-FF3D2^-C'
+'-9DFDD4^-C'
+'-3CC4EA^-C'
+'-1E61E7^-C'
+'-265C7B3C30F68A^-2'
+'-D6627EA16F9^-5'
+'72CC54888^-8'
+'-1DC1460C^-9'
+'E360D8^-B'
+'8632E^-C'
+'1894C^-C'
+'102AE^-C'
+'A0EB^-D'
+'3DB0C^-D'
+'1F152^-D'
+'487E34^6'
+'487FAB^6'
+'177^3'
+'457655A1930698^2'
+'455C49B27439^0'
+'-1928CA81B8^-3'
+'-495B4C8^-6'
+'31218^-8'
+'E78^-A'
+'-E4^-B'
+'18^-B'
+'-AC^-B'
+'588^-B'
+'D8^-C'
+'-1147B8471129B7^3'
+'-11DEFDEC83F6^0'
+'5F73D5918^-3'
+'29AC78^-6'
+'-581^-8'
+'-216^-9'
+'38^-A'
+'-28^-B'
+'4FC^-A'
+'-192^-A'
+'312^-A'
+'DDFA29434C7BD8^2'
+'-3858B5274BA6^0'
+'-4E6F17E7E^-3'
+'1849C^-6'
+'-251B^-8'
+'2ED^-9'
+'-13^-A'
+'1^-B'
+'-25C^-A'
+'104^-A'
+'-176^-A'
+'2F599FA210FCEE^-2'
+'-44B39685AC98^-5'
+'-12C71D4948^-7'
+'10C070BC^-9'
+'61C764^-B'
+'-325C8^-C'
+'-DCE^-E'
+'4^-F'
+'-5C^-F'
+'428^-F'
+'-222^-F'
+'-C3331730DD21D^-3'
+'104A6004CB708^-4'
+'AAA37806A^-8'
+'-1DFE058E^-9'
+'-E44B84^-B'
+'5AAD4^-C'
+'1E9A8^-D'
+'-72^-F'
+'2EC^-F'
+'-A8^-10'
+'199^-F'
+'-2677442D4FABBC^-2'
+'-D62D5C553F34^-5'
+'638FF8968^-8'
+'-CADA7F8^-A'
+'13DEEDC^-A'
+'3067C^-C'
+'-26AC^-D'
+'-45^-F'
+'5B^-F'
+'-234^-F'
+'322^-F'
+'487B46^6'
+'487E34^6'
+'0^0'
+'1^1'
+'8D^2'
+'0^0'
+'3^1'
+'8B^2'
+'2^1'
+'0^0'
+'0^0'
+'0^0'
+'1^1'
+'2^1'
+'0^0'
+'0^0'
+'44^2'
+'1^1'
+'11^2'
+END_ARRAY 3 158
+TOTAL_ARRAYS 3
+ ~NAIF/SPC BEGIN COMMENTS~
+; ../sliced_kernels/m0126888978f7_2p_isis_1.bsp LOG FILE
+
+; Created 2024-03-04/14:19:21.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /Volumes/Blueman_2/isis_data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = ../sliced_kernels/m0126888978f7_2p_isis_1.bsp
+ SOURCE_SPK_KERNEL = /Volumes/Blueman_2/isis_data/base/kernels/spk/de405.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 10
+ BEGIN_TIME = 2000 FEB 25 11:37:11.972
+ END_TIME = 2000 FEB 25 11:41:12.737
+SOURCE_SPK_KERNEL = /Volumes/Blueman_2/isis_data/near/kernels/tspk/erosephem_1999004_2002181.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = 2000433
+ BEGIN_TIME = 2000 FEB 25 11:37:11.972
+ END_TIME = 2000 FEB 25 11:41:12.737
+SOURCE_SPK_KERNEL = /Volumes/Blueman_2/isis_data/near/kernels/spk/near_erosorbit_nav_v1.bsp
+ INCLUDE_COMMENTS = NO
+ BODIES = -93
+ BEGIN_TIME = 2000 FEB 25 11:37:11.972
+ END_TIME = 2000 FEB 25 11:41:12.737
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/m0126888978f7_2p/msi15.ti b/tests/pytests/data/m0126888978f7_2p/msi15.ti
new file mode 100755
index 0000000000000000000000000000000000000000..fcca88e134a03d238a2d9a4a269e30b4adf334f6
--- /dev/null
+++ b/tests/pytests/data/m0126888978f7_2p/msi15.ti
@@ -0,0 +1,183 @@
+KPL/IK
+
+NEAR MultiSpectral Imager (MSI) instrument and frame kernel file
+----------------------------------------------------------------
+
+ Version 1.5b by Jeannie Backer, USGS Astrogeology, 01 March 2013.
+
+ Altered the NEAR_MSI to NEAR_SC_BUS_PRIME frame rotation to include a
+ second rotation.
+
+ Version 1.5 by Jeff Bytof, NAIF/JPL, 10 March 2000.
+
+ Removed tab characters from file. Corrected comments.
+
+
+ Version 1.4 by Jeff Bytof, NAIF/JPL, 1 March 2000.
+
+ Corrected field of view orientation by swapping Y and Z
+ vector component values in INS-93001_FOV_BOUNDARY_CORNERS.
+
+
+ Version 1.3 by Jeff Bytof, NAIF/JPL, 14 August 1998.
+
+ (1) Modified the Euler angles needed to move the NEAR_MSI reference frame
+ into the NEAR_SC_BUS_PRIME frame. Calibrated boresight data provided
+ by Yanping Guo (JHU/APL), dated 13 August 1998, is as follows:
+
+ -----------------------------------------------------
+ Instrument Zenith Angle off Azimuth Angle off
+ +Z S/C Axis (deg) +X' S/C Axis (deg)
+ ----------------- ------------------
+ MSI 89.917365 -0.0277221
+ -----------------------------------------------------
+
+ The zenith angle is measured from the spacecraft +Z axis to the
+ instrument boresight, and the azimuth angle is measured
+ counterclockwise from the spacecraft +X' axis to the boresight.
+
+ The NEAR_MSI boresight is defined to be identical +X unit vector
+ of its reference frame.
+
+ Using the Euler angles given in this kernel, the components of
+ the NEAR_MSI frame relative to the NEAR_SC_BUS_PRIME frame
+ are found by the SPICE subroutine SXFORM to be as follows:
+
+ X: .9999988429 -.0004838414 .0014422523
+ Y: .0004838419 .9999998829 .0000000000
+ Z: -.0014422522 .0000006978 .9999989600
+
+ This indicates that the NEAR_MSI boresight points towards
+ (.9999988429, -.0004838414, .0014422523) as measured in the
+ NEAR_SC_BUS_PRIME frame.
+
+ (2) Corrected the SPICE file ID word to KPL/IK.
+
+
+ Version 1.2 (prototype) by JAB, NAIF/JPL, September 11, 1997
+
+ SC_BUS frame definitions were swapped with SC_BUS_PRIME,
+ to follow the NEAR project's use of the code -93000 for the
+ SC_BUS_PRIME frame.
+
+ Version 1.1 (prototype) by BVS, NAIF/JPL, August 11, 1997
+
+ The frame definitions were changed to reflect correct
+ transformation sense specified by FRAMES.REQ document
+ released in SPICE toolkit N0047.
+
+ Version 1.0 (prototype) by BVS, NAIF/JPL, April 16, 1997
+
+ Spacecraft frame definitions. Required to support automatic
+ frame transformations. Two frames are defined for NEAR s/c:
+
+ - s/c frame (or s/c technological frame);
+ - s/c prime frame; rotated -135 degrees around Z
+ relative to the s/c frame;
+
+ Orientation of the first frame is provided in CK files relative
+ to some inertial or non-inertial frame; orientation of the second
+ frame is a constant from the first frame offset specified in
+ the frame definition.
+
+ Note that these definitions are duplicated in IK files for all
+ other NEAR instruments.
+
+ Note that angles in the frame definitions are specified for "from
+ instrument to base (relative to) frame" transformation.
+
+\begindata
+
+ FRAME_NEAR_SC_BUS_PRIME = -93000
+ FRAME_-93000_NAME = 'NEAR_SC_BUS_PRIME'
+ FRAME_-93000_CLASS = 3
+ FRAME_-93000_CLASS_ID = -93000
+ FRAME_-93000_CENTER = -93
+ CK_-93000_SCLK = -93
+ CK_-93000_SPK = -93
+
+ FRAME_NEAR_SC_BUS = -93100
+ FRAME_-93100_NAME = 'NEAR_SC_BUS'
+ FRAME_-93100_CLASS = 4
+ FRAME_-93100_CLASS_ID = -93100
+ FRAME_-93100_CENTER = -93
+ TKFRAME_-93100_SPEC = 'ANGLES'
+ TKFRAME_-93100_RELATIVE = 'NEAR_SC_BUS_PRIME'
+ TKFRAME_-93100_ANGLES = ( -135.0, 0.0, 0.0 )
+ TKFRAME_-93100_AXES = ( 3, 2, 1 )
+ TKFRAME_-93100_UNITS = 'DEGREES'
+
+\begintext
+
+ MSI instrument frame definition. Required to support automatic
+ frame transformations. Orientation of this frame is a constant
+ offset from s/c prime frame specified in the frame definition.
+
+ Note that angles in the frame definitions are specified for "from
+ instrument to base (relative to) frame" transformation.
+
+ Original rotation:
+ TKFRAME_-93001_ANGLES = ( 0.0277221, 0.082635, 0.0 )
+ TKFRAME_-93001_AXES = ( 3, 2, 1 )
+ TKFRAME_-93001_AXES = ( 1, 2, 3 )
+ TKFRAME_-93001_UNITS = 'DEGREES'
+
+ Second rotation:
+ TKFRAME_-93001_ANGLES = ( 0.0, 180.0, -90.0 )
+ TKFRAME_-93001_AXES = ( 3, 1, 2 )
+ TKFRAME_-93001_UNITS = 'DEGREES'
+
+ Combined (orginal and second) rotations:
+ TKFRAME_-93001_ANGLES = ( 90.0, -179.972278, -0.082635 )
+ TKFRAME_-93001_AXES = ( 2, 1, 2 )
+ TKFRAME_-93001_UNITS = 'DEGREES'
+
+\begindata
+
+ FRAME_NEAR_MSI = -93001
+ FRAME_-93001_NAME = 'NEAR_MSI'
+ FRAME_-93001_CLASS = 4
+ FRAME_-93001_CLASS_ID = -93001
+ FRAME_-93001_CENTER = -93
+ TKFRAME_-93001_SPEC = 'ANGLES'
+ TKFRAME_-93001_RELATIVE = 'NEAR_SC_BUS_PRIME'
+ TKFRAME_-93001_ANGLES = ( 90.0, -179.972278, -0.082635 )
+ TKFRAME_-93001_AXES = ( 2, 1, 2 )
+ TKFRAME_-93001_UNITS = 'DEGREES'
+
+\begintext
+
+
+ Instrument FOV shape/orientation definitions. Conform to
+ specification in the header of the GETFOV subroutine.
+ Corner directions are given counterclockwise as seen from
+ boresight.
+
+ FOV corner directions are defined assuming that:
+
+ - FOV has rectangular shape with its sides along Z and Y
+ axes of the instruments frame;
+ - FOV angular size in Y direction is 2.2623 degrees;
+ in Z direction -- 2.9505 degrees;
+ - boresight vector intersect FOV exactly in the center of
+ the rectangle;
+
+\begindata
+
+
+ INS-93001_FOV_FRAME = 'NEAR_MSI'
+ INS-93001_FOV_SHAPE = 'POLYGON'
+ INS-93001_BORESIGHT = (
+ 1.0 0.0 0.0
+ )
+\begindata
+
+ INS-93001_FOV_BOUNDARY_CORNERS = (
+ 1.0 0.019744857140 0.025753661240
+ 1.0 -0.019744857140 0.025753661240
+ 1.0 -0.019744857140 -0.025753661240
+ 1.0 0.019744857140 -0.025753661240
+ )
+
+\begintext
+
diff --git a/tests/pytests/data/m0126888978f7_2p/msiAddendum002.ti b/tests/pytests/data/m0126888978f7_2p/msiAddendum002.ti
new file mode 100755
index 0000000000000000000000000000000000000000..22ce63c56dbbe91cc4f7fa3987958b704bcbb0bc
--- /dev/null
+++ b/tests/pytests/data/m0126888978f7_2p/msiAddendum002.ti
@@ -0,0 +1,65 @@
+\begintext
+
+ This kernel is used by the ISIS software to supply required keywords for
+ the ISIS NEAR/MSI camera model. This kernel is furnished to the NAIF SPICE
+ pool as one of the very last kernels. This allows it to overide keywords
+ from other kernels.
+
+ History:
+
+ 2013-02-08 Unknown - Original Version 001.
+ 2021-03-23 Kris Becker - Version 002. Added observer/target and light time
+ correction specs
+
+
+From the following lines, we can determine that
+focal length is 166.85 in mm and 10428.125 in pixels. Thus,
+pixel resolution is 10428.125/166.85 = 166.85 pix/mm and
+pixel pitch is 1/62.5 = 0.016 mm/pix.
+The following lines were found in the document
+/usgs/cpkgs/isis2/lsb/isisd/data/mission.sav:
+
+
+
+Near_1 MSI 166.85mm pixel-0.027x0.016mm raw size=244lx537s
+ F/L CENTER UNDISTORTED DISTORTED WEIGHT
+ MISSION CAMERA FILTER PIXELS LINE SAMP NL NS NL NS C
+ _______________________________|X_________|___________|_________|_____|_____|____|____|____|____|_____|
+
+NEAR_1 MSI ALL 10428.125 206.5 269. 412 537 412 537 1.
+
+
+K1 was found in isis2 spi_distorccd.F
+
+Move these out of the data section
+#INS-93900_FRAME_ID = -93900
+#INS-93901_FRAME_ID = -93901
+
+\begindata
+INS-93001_PLATFORM_ID = -93000
+INS-93001_FRAME_ID = -93001
+
+INS-93001_K1 = -0.00007
+INS-93001_FOCAL_LENGTH = 166.85
+INS-93001_PIXEL_PITCH = 0.016
+
+INS-93001_BORESIGHT_SAMPLE = 269.0
+INS-93001_BORESIGHT_LINE = 206.5
+
+INS-93001_TRANSX = ( 0.0, 0.016, 0.0 )
+INS-93001_TRANSY = ( 0.0, 0.0, -0.016 )
+INS-93001_ITRANSS = ( 0.0, 62.5, 0.0 )
+INS-93001_ITRANSL = ( 0.0, 0.0, -62.5 )
+
+\begintext
+
+This section defines observer/target orientation and light time settings
+
+\begindata
+
+INS-93001_SWAP_OBSERVER_TARGET = 'TRUE'
+INS-93001_LIGHTTIME_CORRECTION = 'LT+S'
+INS-93001_LT_SURFACE_CORRECT = 'FALSE'
+
+\begintext
+
diff --git a/tests/pytests/data/m0126888978f7_2p/naif0012.tls b/tests/pytests/data/m0126888978f7_2p/naif0012.tls
new file mode 100755
index 0000000000000000000000000000000000000000..e1afdee1b626e01a3f1b04ef8a43154e83972e56
--- /dev/null
+++ b/tests/pytests/data/m0126888978f7_2p/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/m0126888978f7_2p/near_171.tsc b/tests/pytests/data/m0126888978f7_2p/near_171.tsc
new file mode 100755
index 0000000000000000000000000000000000000000..ac1806c5b2669630592d3fb96bc33f4ce82f9fad
--- /dev/null
+++ b/tests/pytests/data/m0126888978f7_2p/near_171.tsc
@@ -0,0 +1,252 @@
+KPL/SCLK
+\begintext
+
+LABEL_START
+FILENAME ="near_171.tsc"
+MISSION_NAME ="NEAR"
+ORGANIZATION = "JHU/APL"
+AUTHOR ="SCLK update program"
+CONTACT ="david.tillman@jhuapl.edu"
+TYPE ="SCLK"
+CREATION_DATE ="12-Feb-2001"
+TARGET ="N/A"
+START_UTC ="1996-02-17T20:43:29"
+END_UTC ="N/A"
+END_DET_UTC ="N/A"
+
+SOURCE_FILES ={de403.bsp,
+eros9845.bsp,
+near_1998356_2000045_v01.bsp,
+near_2000045_2000125_v02.bsp,
+near_2000121_2000189_v01_noburn.bsp,
+near_2000181_2000242_v01.bsp,
+near_2000223_2000270_v01.bsp,
+near_2000265_2000298_v01.bsp,
+near_2000294_2000309_v01_noburn.bsp,
+near_2000302_2000341_v01.bsp,
+near_2000336_2001028_v01.bsp,
+near_2001026_2001043_v01.bsp,
+near_2001035_2001043_v01.bsp,
+naif0007.tls,
+pck00006.tpc,
+near_170.tsc}
+
+MERGED_FILES ="N/A"
+
+NUMBER_VERTICES ="N/A"
+NUMBER_PLATES ="N/A"
+
+DESCRIPTION ="
+
+This kernel uses a least-squares fit to the clock data from Nov. 1996
+to December 1997, using a constant drift rate of -0.0164 seconds/day.
+Coefficients covering the period January 1998 through end of mission
+are produced by the SCLK Kernel Update utility on an automatic basis.
+
+This kernel also includes the effects of time changes sent to the
+spacecraft clock during a test on May 30, 1997, and during the
+Mathilde flyby on June 27, 1997. All of these time changes were
+cancelled by later time changes, so that the spacecraft clock was
+set back to its original timeline.
+
+For the final touchdown of NEAR on Eros on 12 Feb 2001, the clock
+was set backwards 17 seconds. A new partition was added to
+reflect this.
+
+This will be the final kernel produced for the NEAR mission. "
+
+LABEL_END
+FREE FORM COMMENTS:
+
+
+Specification for a type 1 SCLK...
+Model the SCLK against the time system TDT (terrestrial
+dynamical time) TIME_SYSTEM = 2; variable names
+indicate NEAR (ID -93).
+
+
+
+This kernel was rebuilt on Tue Dec 8 20:22:10 1998
+starting from encoded SCLK: 59023003498 as build number: 1
+
+
+This kernel was rebuilt on Thu Jan 28 14:59:12 1999
+starting from encoded SCLK: 92272635009 as build number: 2
+
+\begindata
+SCLK_KERNEL_ID = ( @2001-02-12T19:00:03 )
+SCLK_DATA_TYPE_93 = ( 1 )
+SCLK01_TIME_SYSTEM_93 = ( 2 )
+
+
+\begintext
+For NEAR, Use a single field which represents milliseconds past
+mission start time; moduli set well beyond end of mission.
+
+\begindata
+SCLK01_N_FIELDS_93 = ( 1 )
+SCLK01_MODULI_93 = ( 2.0e+12 )
+SCLK01_OFFSETS_93 = ( 0 )
+SCLK01_OUTPUT_DELIM_93 = ( 1 )
+
+
+\begintext
+Supply the partition information. If needed,
+(e.g., switch to backup bus controller occurs), can
+add additional records (lines) to following variables to
+define new partitions; generally, the start of the
+new partition should coincide with the end of the
+previous one.
+
+\begindata
+SCLK_PARTITION_START_93 = ( 0.0000000000e+00
+ 4.0409661942e+10
+ 4.0429229946e+10
+ 4.2793916398e+10
+ 4.2808703400e+10
+ 4.2831583405e+10
+ 1.5741315200e+11
+ )
+
+SCLK_PARTITION_END_93 = ( 4.0409721942e+10
+ 4.0429169946e+10
+ 4.2793906398e+10
+ 4.2808704400e+10
+ 4.2831592405e+10
+ 1.5741316900e+11
+ 2.0000000000e+12
+ )
+
+\begintext
+Finally, define coefficients for starting MET (millisec),
+starting TDT (expressed in terms of date/time string
+@dd-mmm-yyyy-HH:MM:SS) and rate of change between the
+spacecraft clock and TDT, having the following property:
+
+ rate = TDT (sec) / most significant count (millisec)
+
+For NEAR, the most significant count corresponds to 1/1000 of
+a second, giving a rate of 0.001 sec/millisec in the absence
+of clock drift; in general, rate is related to the MET drift
+rate of the spacecraft clock (in millisec/sec) as follows:
+
+ rate = {1+MET drift rate (millisec/sec)/1000} / 1000
+
+The following are preliminary data; additional records (lines) should
+be added as needed to account for changes in clock drift over time;
+the new records must ensure a continuous and monotonically
+increasing relationship between MET and TDT.
+
+\begindata
+SCLK01_COEFFICIENTS_93 = (
+
+0.0000000000e+00 @17-FEB-1996-20:44:30.960 9.9999980900e-04
+4.0409721942e+10 @30-MAY-1997-13:39:45.184 9.9999980900e-04
+4.0429229946e+10 @30-MAY-1997-19:04:53.184 9.9999980900e-04
+4.2793906398e+10 @27-JUN-1997-03:56:09.184 9.9999980900e-04
+4.2808694400e+10 @27-JUN-1997-08:02:37.184 9.9999980900e-04
+4.2831583405e+10 @27-JUN-1997-14:24:06.184 9.9999980900e-04
+6.0125985000e+10 @13-JAN-1998-18:24:04.310 9.9999979941e-04
+6.0212390000e+10 @14-JAN-1998-18:24:09.280 9.9999965456e-04
+6.0515927000e+10 @18-JAN-1998-06:43:06.180 9.9999967129e-04
+6.0760157000e+10 @21-JAN-1998-02:33:36.105 9.9999969185e-04
+6.1092948000e+10 @24-JAN-1998-23:00:07.008 9.9999970879e-04
+6.1253334000e+10 @26-JAN-1998-19:33:12.956 9.9999967631e-04
+6.1373467000e+10 @28-JAN-1998-04:55:25.916 9.9999966669e-04
+6.1594465000e+10 @30-JAN-1998-18:18:43.841 9.9999966090e-04
+6.6859033000e+10 @01-APR-1998-16:41:29.880 9.9999962751e-04
+7.2308626000e+10 @03-JUN-1998-18:28:01.519 9.9999975022e-04
+7.4721547000e+10 @01-JUL-1998-16:43:21.823 9.9999971165e-04
+7.5132721000e+10 @06-JUL-1998-10:56:15.686 9.9999966728e-04
+7.5328509000e+10 @08-JUL-1998-17:19:23.626 9.9999969335e-04
+7.7738193000e+10 @05-AUG-1998-14:40:46.895 9.9999969645e-04
+7.8777422000e+10 @17-AUG-1998-15:21:15.572 9.9999968889e-04
+7.8952916000e+10 @19-AUG-1998-16:06:09.527 9.9999974263e-04
+7.9588468000e+10 @27-AUG-1998-00:38:41.368 9.9999975051e-04
+8.0154353000e+10 @02-SEP-1998-13:50:06.221 9.9999974042e-04
+8.1317059000e+10 @16-SEP-1998-00:48:31.925 9.9999974566e-04
+8.1805260000e+10 @21-SEP-1998-16:25:12.798 9.9999973960e-04
+8.2139807000e+10 @25-SEP-1998-13:20:59.695 9.9999969034e-04
+8.2432241000e+10 @28-SEP-1998-22:34:53.609 9.9999970785e-04
+8.3004321000e+10 @05-OCT-1998-13:29:33.450 9.9999972196e-04
+8.3637554000e+10 @12-OCT-1998-21:23:26.279 9.9999972994e-04
+8.4815021000e+10 @26-OCT-1998-12:27:52.954 9.9999972383e-04
+8.5429701000e+10 @02-NOV-1998-15:12:32.778 9.9999971380e-04
+8.5598364000e+10 @04-NOV-1998-14:03:35.735 9.9999974401e-04
+8.6208312000e+10 @11-NOV-1998-15:29:23.584 9.9999975251e-04
+8.6810662000e+10 @18-NOV-1998-14:48:33.426 9.9999973864e-04
+8.7836239000e+10 @30-NOV-1998-11:41:30.153 9.9999973342e-04
+8.8228097000e+10 @05-DEC-1998-00:32:28.043 9.9999971986e-04
+8.8438735000e+10 @07-DEC-1998-11:03:05.977 9.9999968567e-04
+8.8723522000e+10 @10-DEC-1998-18:09:32.894 9.9999970990e-04
+8.9167446000e+10 @15-DEC-1998-21:28:16.770 9.9999972121e-04
+8.9826627000e+10 @23-DEC-1998-12:34:37.577 9.9999970657e-04
+9.0351015000e+10 @29-DEC-1998-14:14:25.418 9.9999969656e-04
+9.0508753000e+10 @31-DEC-1998-10:03:23.364 9.9999965725e-04
+9.0804879000e+10 @03-JAN-1999-20:18:49.254 9.9999963003e-04
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diff --git a/tests/pytests/data/m0126888978f7_2p/near_2000056_v01_0_sliced_-93000.xc b/tests/pytests/data/m0126888978f7_2p/near_2000056_v01_0_sliced_-93000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..3afd503ca94ea0283b690b2367388b31a7e50fa0
--- /dev/null
+++ b/tests/pytests/data/m0126888978f7_2p/near_2000056_v01_0_sliced_-93000.xc
@@ -0,0 +1,2011 @@
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+'1D8B223BF7^A'
+'1D8B223FDF^A'
+'1D8B2243C7^A'
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+'1D8B224B97^A'
+'1D8B224F7F^A'
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+'1D8B225B37^A'
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+'1D8B226B3C^A'
+'1D8B20346F^A'
+'1D8B21B727^A'
+'1D8B1EB27F^A'
+'1^1'
+'F8^2'
+END_ARRAY 1 1989
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /Users/acpaquette/repos/ale/tests/pytests/data/m0126888978f7_2p/m0126888978f7_2p_isis.lbl
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/m0126888978f7_2p/near_2000056_v01_1_sliced_-93000.xc b/tests/pytests/data/m0126888978f7_2p/near_2000056_v01_1_sliced_-93000.xc
new file mode 100644
index 0000000000000000000000000000000000000000..5c564af8efc313c28743598b5908db2d09561562
--- /dev/null
+++ b/tests/pytests/data/m0126888978f7_2p/near_2000056_v01_1_sliced_-93000.xc
@@ -0,0 +1,1971 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK '
+'2'
+'6'
+'/project/near/SDC_ops/PROD/ALLHDF.001_00442_Feb_27_100_18:33'
+BEGIN_ARRAY 1 1949
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+'1D8B2A522A^A'
+'1^1'
+'F3^2'
+END_ARRAY 1 1949
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /Users/acpaquette/repos/ale/tests/pytests/data/m0126888978f7_2p/m0126888978f7_2p_isis.lbl
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/m0126888978f7_2p/pck00009.tpc b/tests/pytests/data/m0126888978f7_2p/pck00009.tpc
new file mode 100755
index 0000000000000000000000000000000000000000..bfadaab2b26817327189ff3173e9609f49dedc9d
--- /dev/null
+++ b/tests/pytests/data/m0126888978f7_2p/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/test_msi_drivers.py b/tests/pytests/test_msi_drivers.py
new file mode 100644
index 0000000000000000000000000000000000000000..adb248d3cf98f8e10bef5c41488c67aeb6a36aa1
--- /dev/null
+++ b/tests/pytests/test_msi_drivers.py
@@ -0,0 +1,49 @@
+import json
+import os
+import pytest
+import unittest
+
+import ale
+from conftest import get_image_label, get_isd, get_image_kernels, convert_kernels, compare_dicts
+from ale.drivers.msi_drivers import MsiIsisLabelNaifSpiceDriver
+
+from conftest import get_image_label
+from unittest.mock import patch
+
+@pytest.fixture(scope='module')
+def test_kernels():
+ kernels = get_image_kernels('m0126888978f7_2p')
+ updated_kernels, binary_kernels = convert_kernels(kernels)
+ yield updated_kernels
+ for kern in binary_kernels:
+ os.remove(kern)
+
+@pytest.mark.parametrize("label_type", ['isis'])
+def test_msi_load(test_kernels, label_type):
+ label_file = get_image_label('m0126888978f7_2p', label_type)
+ isd_str = ale.loads(label_file, props={'kernels': test_kernels}, verbose=True)
+ isd_obj = json.loads(isd_str)
+ compare_dict = get_isd('msi')
+ print(json.dumps(isd_obj, indent=2))
+ assert compare_dicts(isd_obj, compare_dict) == []
+
+class test_msi_isis_naif(unittest.TestCase):
+ def setUp(self):
+ label = get_image_label("m0126888978f7_2p", "isis")
+ self.driver = MsiIsisLabelNaifSpiceDriver(label)
+
+ def test_instrument_id(self):
+ assert self.driver.instrument_id == "NEAR EARTH ASTEROID RENDEZVOUS"
+
+ def test_center_ephemeris_time(self):
+ with patch('ale.drivers.msi_drivers.MsiIsisLabelNaifSpiceDriver.ephemeris_start_time', 12345) as ephemeris_start_time:
+ assert self.driver.center_ephemeris_time == 12345.3825
+
+ def test_sensor_name(self):
+ assert self.driver.sensor_name == "MULTI-SPECTRAL IMAGER"
+
+ def test_sensor_model_version(self):
+ assert self.driver.sensor_model_version == 2
+
+ def test_ikid(self):
+ assert self.driver.ikid == -93001