From 8aa3b10ade682d45ccafe539057f7c6c0ede4fa8 Mon Sep 17 00:00:00 2001
From: Jacob Cain <115182890+jrcain-usgs@users.noreply.github.com>
Date: Fri, 26 May 2023 15:23:56 -0700
Subject: [PATCH] Hayabusa NIRS (#532)

* Changed hirise comment

* Added NIRS driver

* added nirs test isd

* Added NIRS Tests

* added NIRS test kernels

* added NIRS changelog entry

* remove projection/geotransform in truth ISD
---
 CHANGELOG.md                                  |    3 +-
 ale/drivers/hayabusa_drivers.py               |   70 +-
 .../2392975548_lvl3_0.ale_0.xsp               |  151 +
 .../2392975548_lvl3_0.ale_1.xsp               |  965 +++++
 .../2392975548_lvl3_0_isis.lbl                |  401 ++
 .../data/2392975548_lvl3_0/hayabusa.tsc       | 3462 ++++++++++++++++
 .../data/2392975548_lvl3_0/hayabusa_hp.tf     |  392 ++
 ...itokawarendezvous_v02n_0_sliced_-130000.xc |   56 +
 ...itokawarendezvous_v02n_1_sliced_-130000.xc |  120 +
 .../data/2392975548_lvl3_0/itokawa_fixed.tf   |   94 +
 .../2392975548_lvl3_0/itokawa_gaskell_n3.tpc  |  115 +
 .../data/2392975548_lvl3_0/naif0012.tls       |  152 +
 .../pytests/data/2392975548_lvl3_0/nirs10.ti  |  184 +
 .../data/2392975548_lvl3_0/nirsAddendum002.ti |   34 +
 .../data/2392975548_lvl3_0/pck00009.tpc       | 3639 +++++++++++++++++
 tests/pytests/data/isds/hayabusanirs_isd.json |  260 ++
 tests/pytests/test_hayabusa_drivers.py        |   48 +-
 17 files changed, 10141 insertions(+), 5 deletions(-)
 create mode 100644 tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_0.xsp
 create mode 100644 tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_1.xsp
 create mode 100644 tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0_isis.lbl
 create mode 100755 tests/pytests/data/2392975548_lvl3_0/hayabusa.tsc
 create mode 100755 tests/pytests/data/2392975548_lvl3_0/hayabusa_hp.tf
 create mode 100644 tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_0_sliced_-130000.xc
 create mode 100644 tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_1_sliced_-130000.xc
 create mode 100755 tests/pytests/data/2392975548_lvl3_0/itokawa_fixed.tf
 create mode 100755 tests/pytests/data/2392975548_lvl3_0/itokawa_gaskell_n3.tpc
 create mode 100755 tests/pytests/data/2392975548_lvl3_0/naif0012.tls
 create mode 100755 tests/pytests/data/2392975548_lvl3_0/nirs10.ti
 create mode 100755 tests/pytests/data/2392975548_lvl3_0/nirsAddendum002.ti
 create mode 100755 tests/pytests/data/2392975548_lvl3_0/pck00009.tpc
 create mode 100644 tests/pytests/data/isds/hayabusanirs_isd.json

diff --git a/CHANGELOG.md b/CHANGELOG.md
index 595f0ff..9bc002d 100644
--- a/CHANGELOG.md
+++ b/CHANGELOG.md
@@ -52,4 +52,5 @@ release.
 - Msi IsisLabelNaifSpice Driver [#511](https://github.com/DOI-USGS/ale/pull/511)
 - MGS MOC WAC IsisLabelNaifSpice driver, tests, and test data [#516](https://github.com/DOI-USGS/ale/pull/516)
 - Chandrayaan1_mrffr IsisLabelNaifSpice driver, tests and test data [#519](https://github.com/DOI-USGS/ale/pull/519)
-- MGS MOC Narrow Angle IsisLabelNaifSpice driver, tests, and test data [#517](https://github.com/DOI-USGS/ale/pull/517)
\ No newline at end of file
+- MGS MOC Narrow Angle IsisLabelNaifSpice driver, tests, and test data [#517](https://github.com/DOI-USGS/ale/pull/517)
+- Hayabusa NIRS IsisLabelNaifSpice driver, tests and test data [#532](https://github.com/DOI-USGS/ale/pull/532)
\ No newline at end of file
diff --git a/ale/drivers/hayabusa_drivers.py b/ale/drivers/hayabusa_drivers.py
index c4a2614..04b28b8 100644
--- a/ale/drivers/hayabusa_drivers.py
+++ b/ale/drivers/hayabusa_drivers.py
@@ -1,3 +1,4 @@
+import spiceypy as spice
 from ale.base.data_naif import NaifSpice
 from ale.base.label_isis import IsisLabel
 from ale.base.type_sensor import Framer
@@ -22,7 +23,7 @@ class HayabusaAmicaIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, Radial
     @property
     def sensor_model_version(self):
         """
-        The ISIS Sensor model number for HiRise in ISIS. This is likely just 1
+        The ISIS Sensor model number for Hayabusa Amica in ISIS. This is likely just 1
 
         Returns
         -------
@@ -41,4 +42,69 @@ class HayabusaAmicaIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, Radial
         : str
           Name of the sensor
         """
-        return self.instrument_id
\ No newline at end of file
+        return self.instrument_id
+    
+class HayabusaNirsIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, NoDistortion, Driver):
+
+    @property
+    def instrument_id(self):
+        """
+        Returns the ID of the instrument
+
+        Returns
+        -------
+        : str
+          Name of the instrument
+        """
+        lookup_table = {'NIRS': 'HAYABUSA_NIRS'}
+        return lookup_table[super().instrument_id]
+
+    @property
+    def sensor_model_version(self):
+        """
+        The ISIS Sensor model number for Hayabusa Nirs in ISIS. This is likely just 1
+
+        Returns
+        -------
+        : int
+          ISIS sensor model version
+        """
+        return 1
+
+    @property
+    def sensor_name(self):
+        """
+        Returns the name of the instrument
+
+        Returns
+        -------
+        : str
+          Name of the sensor
+        """
+        return self.instrument_id
+    
+    @property
+    def ephemeris_stop_time(self):
+        """
+        Returns the exposure duration of the instrument
+
+        Returns
+        -------
+        : str
+          Exposure Duration
+        """
+        
+        return spice.scs2e(self.spacecraft_id, self.spacecraft_clock_stop_count)
+    
+    @property
+    def exposure_duration(self):
+        """
+        Returns the exposure duration of the instrument
+
+        Returns
+        -------
+        : str
+          Exposure Duration
+        """
+        
+        return self.ephemeris_stop_time - self.ephemeris_start_time
\ No newline at end of file
diff --git a/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_0.xsp b/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_0.xsp
new file mode 100644
index 0000000..0356b32
--- /dev/null
+++ b/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_0.xsp
@@ -0,0 +1,151 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE                                                    '
+BEGIN_ARRAY 1 33
+'ITOKAWA                                 '
+'AC1FE9B5AB9B2^7'
+'AC1FFCFB61E0C^7'
+'1EE6B7'
+'A'
+'1'
+'2'
+33
+'AC164C^7'
+'2A3^5'
+'-96164580E2F96^7'
+'-98AFDA22EDFAC8^5'
+'7F8792164BF8^4'
+'8E57FFDE00C6^2'
+'-23C2C8BC^0'
+'-18BFAFA64^-1'
+'-2E9FC^-3'
+'-199848^-5'
+'E^-7'
+'3265DFC23373^7'
+'-480F9DC9F93DDC^6'
+'-2ACF5A5F69F^4'
+'7ABC039D108^2'
+'FE2237B8^0'
+'CCCE755^-2'
+'-11C8C^-3'
+'-507E4^-5'
+'-68^-7'
+'1ACE10954DD2DE^7'
+'-1FD5B586354A57^6'
+'-16C533CA1634^4'
+'3291BBCE2D5^2'
+'7247BDBD8^0'
+'66BB89F8^-2'
+'-692A^-4'
+'-231B4^-5'
+'-28^-7'
+'ABEC1C^7'
+'546^5'
+'1D^2'
+'1^1'
+END_ARRAY 1 33
+BEGIN_ARRAY 2 16
+'HAYABUSA Traj. by HJSC; with NAIF mods  '
+'AC1FE9B5AB9B2^7'
+'AC1FFCFB61E0C^7'
+'-82'
+'1EE6B7'
+'1'
+'9'
+16
+'FD0D130C3E5CF8^1'
+'-32CEAB825B452A^1'
+'-1C8AE979EBDB0B^1'
+'18997317907C75^-3'
+'-11922DF762C049^-4'
+'-DDCD8152470B9^-5'
+'10C1B09DB1E9EB^2'
+'-337AB8D362FE0C^1'
+'-1D12A714AB578D^1'
+'160C4781A00001^-3'
+'-5E8A965C^-5'
+'-74440DFD^-5'
+'AC164E001A362^7'
+'AC2018B41E4B28^7'
+'1^1'
+'2^1'
+END_ARRAY 2 16
+BEGIN_ARRAY 3 39
+'DE-0403LE-0403                          '
+'AC1FE9B5AB9B2^7'
+'AC1FFCFB61E0C^7'
+'A'
+'0'
+'1'
+'2'
+39
+'ACA9F4^7'
+'A8C^5'
+'95D530B0708338^5'
+'-954848CD8FCCC8^3'
+'-1237A4B9E50726^2'
+'27BC5CD97A7B14^0'
+'-A008B2350BB548^-2'
+'-D2B620BE6E8188^-3'
+'1CCEE01A24443C^-3'
+'-2DD8F01365A4FA^-4'
+'36287C4B50D55A^-5'
+'-1FE65DFD04A91B^-6'
+'-6A58460956428^-7'
+'36DF7F7552069^5'
+'1C5529660F3CE4^4'
+'-A946527ED81378^1'
+'9A0E242217DF6^-1'
+'16FE20CDC8E56B^-1'
+'-1292E9468DA1ED^-2'
+'BAEA14DDB07C4^-4'
+'6342B3BBC0991C^-5'
+'-2DB7DC8B183E78^-5'
+'628F2A73E43B98^-6'
+'-B29DC397F7128^-7'
+'1327760ADD39C3^5'
+'C31C168F8BEC^3'
+'-42418DABAB8A8^1'
+'E630651E16D2E^-2'
+'BD018994D52C78^-2'
+'-878B623FBBAAB^-3'
+'35FD3ECDACEEC2^-4'
+'81103383568628^-5'
+'-1E099CC4A97B08^-5'
+'38632AEF23BA6^-6'
+'-544DDE19114234^-7'
+'AC0134^7'
+'1518^6'
+'23^2'
+'1^1'
+END_ARRAY 3 39
+TOTAL_ARRAYS 3
+ ~NAIF/SPC BEGIN COMMENTS~
+
+; Created 2023-05-05/16:06:04.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = ~/remotedata/isis_data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = ~/data/isistestdata/hayabusa/nirs/out/2392975548_lvl3_0.ale_0.bsp
+SOURCE_SPK_KERNEL = ~/remotedata/isis_data/hayabusa/kernels/tspk/sb_25143_140.bsp
+    INCLUDE_COMMENTS = NO
+    BODIES           = 2025143
+    BEGIN_TIME       = 2005 SEP 20 10:55:23.172
+    END_TIME         = 2005 SEP 20 11:00:31.529
+SOURCE_SPK_KERNEL = ~/remotedata/isis_data/hayabusa/kernels/spk/hay_osbj_050911_051118_v1n.bsp
+    INCLUDE_COMMENTS = NO
+    BODIES           = -130
+    BEGIN_TIME       = 2005 SEP 20 10:55:23.172
+    END_TIME         = 2005 SEP 20 11:00:31.529
+SOURCE_SPK_KERNEL = ~/remotedata/isis_data/hayabusa/kernels/tspk/de403s.bsp
+    INCLUDE_COMMENTS = NO
+    BODIES           = 10
+    BEGIN_TIME       = 2005 SEP 20 10:55:23.172
+    END_TIME         = 2005 SEP 20 11:00:31.529
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_1.xsp b/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_1.xsp
new file mode 100644
index 0000000..a7b0e8a
--- /dev/null
+++ b/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0.ale_1.xsp
@@ -0,0 +1,965 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/SPK '
+'2'
+'6'
+'SPKMERGE                                                    '
+BEGIN_ARRAY 1 33
+'ITOKAWA                                 '
+'AC200CC268059^7'
+'AC201FED9F515^7'
+'1EE6B7'
+'A'
+'1'
+'2'
+33
+'AC164C^7'
+'2A3^5'
+'-96164580E2F96^7'
+'-98AFDA22EDFAC8^5'
+'7F8792164BF8^4'
+'8E57FFDE00C6^2'
+'-23C2C8BC^0'
+'-18BFAFA64^-1'
+'-2E9FC^-3'
+'-199848^-5'
+'E^-7'
+'3265DFC23373^7'
+'-480F9DC9F93DDC^6'
+'-2ACF5A5F69F^4'
+'7ABC039D108^2'
+'FE2237B8^0'
+'CCCE755^-2'
+'-11C8C^-3'
+'-507E4^-5'
+'-68^-7'
+'1ACE10954DD2DE^7'
+'-1FD5B586354A57^6'
+'-16C533CA1634^4'
+'3291BBCE2D5^2'
+'7247BDBD8^0'
+'66BB89F8^-2'
+'-692A^-4'
+'-231B4^-5'
+'-28^-7'
+'ABEC1C^7'
+'546^5'
+'1D^2'
+'1^1'
+END_ARRAY 1 33
+BEGIN_ARRAY 2 829
+'HAYABUSA Traj. by HJSC; with NAIF mods  '
+'AC200CC268059^7'
+'AC201FED9F515^7'
+'-82'
+'1EE6B7'
+'1'
+'9'
+829
+'FD0D130C3E5CF8^1'
+'-32CEAB825B452A^1'
+'-1C8AE979EBDB0B^1'
+'18997317907C75^-3'
+'-11922DF762C049^-4'
+'-DDCD8152470B9^-5'
+'10C1B09DB1E9EB^2'
+'-337AB8D362FE0C^1'
+'-1D12A714AB578D^1'
+'160C4781A00001^-3'
+'-5E8A965C^-5'
+'-74440DFD^-5'
+'10C1B1FE766205^2'
+'-337AB931ED9468^1'
+'-1D12A788EF658A^1'
+'160C3F30FFFFFF^-3'
+'-5E881D10000004^-5'
+'-7442AE24^-5'
+'10C1B35F3A5515^2'
+'-337AB99075B178^1'
+'-1D12A7FD3213AE^1'
+'160C36CEBFFFFF^-3'
+'-5E85D882^-5'
+'-74415FE6^-5'
+'10C1B4BFFDC201^2'
+'-337AB9EEFB89FA^1'
+'-1D12A871737394^1'
+'160C2E7E2^-3'
+'-5E835F3^-5'
+'-7440000C000004^-5'
+'10C1B620C0A9E3^2'
+'-337ABA4D7EE92A^1'
+'-1D12A8E5B373A^1'
+'160C262D5FFFFF^-3'
+'-5E810910000004^-5'
+'-743EB1CBFFFFFC^-5'
+'10C1B781830CB9^2'
+'-337ABAABFFF23A^1'
+'-1D12A959F2256C^1'
+'160C1DDCCFFFFF^-3'
+'-5E7EA153FFFFFC^-5'
+'-743D405D^-5'
+'10C1B8E244EA86^2'
+'-337ABB0A7E938E^1'
+'-1D12A9CE2F65C9^1'
+'160C157A8FFFFF^-3'
+'-5E7C4B32^-5'
+'-743C03B4^-5'
+'10C1BA4306422F^2'
+'-337ABB68FADEC^1'
+'-1D12AA426B697D^1'
+'160C0D29CFFFFF^-3'
+'-5E79D1E1FFFFFC^-5'
+'-743A9244^-5'
+'10C1BBA3C714CC^2'
+'-337ABBC774B0A2^1'
+'-1D12AAB6A5FBC1^1'
+'160C04C7B^-3'
+'-5E778D56^-5'
+'-74394404^-5'
+'10C1BD04876147^2'
+'-337ABC25EC3DF8^1'
+'-1D12AB2ADF3FC5^1'
+'1611A2D2578ACA^-3'
+'-5E8D487F040C04^-5'
+'-7455BDCB13218C^-5'
+'10C1BE654729D^2'
+'-337ABC846151FE^1'
+'-1D12AB9F173589^1'
+'160BF4263FFFFF^-3'
+'-5E72BDE1FFFFFC^-5'
+'-74368453^-5'
+'10C1BFC6066C34^2'
+'-337ABCE2D40FE^1'
+'-1D12AC134DB9DC^1'
+'160BEBC42^-3'
+'-5E705627FFFFFC^-5'
+'-743547ABFFFFFC^-5'
+'10C1C126C52876^2'
+'-337ABD41446608^1'
+'-1D12AC87830188^1'
+'160BE385^-3'
+'-5E6E0006^-5'
+'-7433D63AFFFFFC^-5'
+'10C1C2878360C6^2'
+'-337ABD9FB2660E^1'
+'-1D12ACFBB6D7C3^1'
+'160BDB22C^-3'
+'-5E6B984A^-5'
+'-743287FAFFFFFC^-5'
+'10C1C3E84112F2^2'
+'-337ABDFE1DFE58^1'
+'-1D12AD6FE95FBE^1'
+'160BD2D2200002^-3'
+'-5E693094000004^-5'
+'-743139BB^-5'
+'10C1C548FE4014^2'
+'-337ABE5C872EEC^1'
+'-1D12ADE41A9979^1'
+'160BCA6FE00001^-3'
+'-5E66C8D6000004^-5'
+'-742FC84B^-5'
+'10C1C6A9BAE712^2'
+'-337ABEBAEDF7C2^1'
+'-1D12AE584A61C4^1'
+'160BC21F3^-3'
+'-5E6472B6^-5'
+'-742E8BA2000004^-5'
+'10C1C80A770905^2'
+'-337ABF19526A78^1'
+'-1D12AECC78ED66^1'
+'160BB9CEA^-3'
+'-5E620AFC^-5'
+'-742D1A33^-5'
+'10C1C96B32A5EF^2'
+'-337ABF77B47574^1'
+'-1D12AF40A60799^1'
+'160BB17DDFFFFF^-3'
+'-5E5FB4D6^-5'
+'-742BCBF2^-5'
+'10C1CACBEDBDCD^2'
+'-337ABFD6142A4A^1'
+'-1D12AFB4D1D38B^1'
+'160BA91BAFFFFF^-3'
+'-5E5D4D22^-5'
+'-742A7DB2^-5'
+'10C1CC2CA84F88^2'
+'-337AC03471776C^1'
+'-1D12B028FC513D^1'
+'160BA0CB000001^-3'
+'-5E5AE564^-5'
+'-74290C42^-5'
+'10C1CD8D625C38^2'
+'-337AC092CC5CD^1'
+'-1D12B09D255D7F^1'
+'160B987A4FFFFF^-3'
+'-5E588F42^-5'
+'-7427CF9A^-5'
+'10C1CEEE1BE3DD^2'
+'-337AC0F124EC12^1'
+'-1D12B1114D2D19^1'
+'160B9018200002^-3'
+'-5E562789FFFFFC^-5'
+'-74265E2B^-5'
+'10C1D04ED4E55F^2'
+'-337AC14F7B139C^1'
+'-1D12B185738B44^1'
+'160B87C77^-3'
+'-5E53BFCE^-5'
+'-74250FE9000004^-5'
+'10C1D1AF8D61D6^2'
+'-337AC1ADCED36A^1'
+'-1D12B1F9989B2D^1'
+'160B7F76D00001^-3'
+'-5E5169AA000004^-5'
+'-7423C1A8FFFFFC^-5'
+'10C1D310455943^2'
+'-337AC20C203D14^1'
+'-1D12B26DBC5CD6^1'
+'160B77147FFFFF^-3'
+'-5E4F01F2000004^-5'
+'-7422503A000004^-5'
+'10C1D470FCCA8B^2'
+'-337AC26A6F3F06^1'
+'-1D12B2E1DEAD1^1'
+'160B6EC3EFFFFE^-3'
+'-5E4C9A3A000004^-5'
+'-742101F8^-5'
+'10C1D5D1B3B6CA^2'
+'-337AC2C8BBD94^1'
+'-1D12B355FFAF08^1'
+'160B66734^-3'
+'-5E4A4416^-5'
+'-741FB3B9^-5'
+'10C1D7326A1DFE^2'
+'-337AC327061D56^1'
+'-1D12B3CA1F62C1^1'
+'160B5E228FFFFF^-3'
+'-5E47DC5C^-5'
+'-741E53E2^-5'
+'10C1D893200027^2'
+'-337AC3854DF9B2^1'
+'-1D12B43E3DB6A3^1'
+'160B55C04FFFFF^-3'
+'-5E4574A2^-5'
+'-741CF409000004^-5'
+'10C1D9F3D55C2C^2'
+'-337AC3E3936E54^1'
+'-1D12B4B25AAAAC^1'
+'160B4D6FB00001^-3'
+'-5E431E80000004^-5'
+'-741BA5C6FFFFFC^-5'
+'10C1DB548A3327^2'
+'-337AC441D68CD4^1'
+'-1D12B526765073^1'
+'160B451EFFFFFF^-3'
+'-5E40B6C4^-5'
+'-741A45F1000004^-5'
+'10C1DCB53E8517^2'
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+'AC201CE4161A08^7'
+'AC201CF4161A08^7'
+'AC201D04161A08^7'
+'AC201D14161A08^7'
+'AC201D24161A08^7'
+'AC201D34161A08^7'
+'AC201D44161A08^7'
+'AC201D54161A08^7'
+'AC201D64161A08^7'
+'AC201D74161A08^7'
+'AC201D84161A08^7'
+'AC201D94161A08^7'
+'AC201DA4161A08^7'
+'AC201DB4161A08^7'
+'AC201DC4161A08^7'
+'AC201DD4161A08^7'
+'AC201DE4161A08^7'
+'AC201DF4161A08^7'
+'AC201E04161A08^7'
+'AC201E14161A08^7'
+'AC201E24161A08^7'
+'AC201E34161A08^7'
+'AC201E44161A08^7'
+'AC201E5412017^7'
+'AC201E6412017^7'
+'AC201E7412017^7'
+'AC201E8412017^7'
+'AC201E9412017^7'
+'AC201EA412017^7'
+'AC201EB412017^7'
+'AC201EC412017^7'
+'AC201ED412017^7'
+'AC201EE412017^7'
+'AC201EF412017^7'
+'AC201F0412017^7'
+'AC201F1412017^7'
+'AC201F2412017^7'
+'AC201F3412017^7'
+'AC201F4412017^7'
+'AC201F5412017^7'
+'AC201F6412017^7'
+'AC201F7412017^7'
+'AC201F8412017^7'
+'AC201F9412017^7'
+'AC201FA412017^7'
+'AC201FB412017^7'
+'AC201FC412017^7'
+'AC201FD412017^7'
+'AC201FE412017^7'
+'AC201FF412017^7'
+'AC201ED412017^7'
+'1^1'
+'76^2'
+END_ARRAY 2 829
+BEGIN_ARRAY 3 39
+'DE-0403LE-0403                          '
+'AC200CC268059^7'
+'AC201FED9F515^7'
+'A'
+'0'
+'1'
+'2'
+39
+'ACA9F4^7'
+'A8C^5'
+'95D530B0708338^5'
+'-954848CD8FCCC8^3'
+'-1237A4B9E50726^2'
+'27BC5CD97A7B14^0'
+'-A008B2350BB548^-2'
+'-D2B620BE6E8188^-3'
+'1CCEE01A24443C^-3'
+'-2DD8F01365A4FA^-4'
+'36287C4B50D55A^-5'
+'-1FE65DFD04A91B^-6'
+'-6A58460956428^-7'
+'36DF7F7552069^5'
+'1C5529660F3CE4^4'
+'-A946527ED81378^1'
+'9A0E242217DF6^-1'
+'16FE20CDC8E56B^-1'
+'-1292E9468DA1ED^-2'
+'BAEA14DDB07C4^-4'
+'6342B3BBC0991C^-5'
+'-2DB7DC8B183E78^-5'
+'628F2A73E43B98^-6'
+'-B29DC397F7128^-7'
+'1327760ADD39C3^5'
+'C31C168F8BEC^3'
+'-42418DABAB8A8^1'
+'E630651E16D2E^-2'
+'BD018994D52C78^-2'
+'-878B623FBBAAB^-3'
+'35FD3ECDACEEC2^-4'
+'81103383568628^-5'
+'-1E099CC4A97B08^-5'
+'38632AEF23BA6^-6'
+'-544DDE19114234^-7'
+'AC0134^7'
+'1518^6'
+'23^2'
+'1^1'
+END_ARRAY 3 39
+TOTAL_ARRAYS 3
+ ~NAIF/SPC BEGIN COMMENTS~
+; ~/data/isistestdata/hayabusa/nirs/out/2392975548_lvl3_0.ale_1.bsp LOG FILE
+
+; Created 2023-05-05/16:06:10.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = ~/remotedata/isis_data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = ~/data/isistestdata/hayabusa/nirs/out/2392975548_lvl3_0.ale_1.bsp
+SOURCE_SPK_KERNEL = ~/remotedata/isis_data/hayabusa/kernels/tspk/sb_25143_140.bsp
+    INCLUDE_COMMENTS = NO
+    BODIES           = 2025143
+    BEGIN_TIME       = 2005 SEP 20 11:04:43.968
+    END_TIME         = 2005 SEP 20 11:09:50.669
+SOURCE_SPK_KERNEL = ~/remotedata/isis_data/hayabusa/kernels/spk/hay_osbj_050911_051118_v1n.bsp
+    INCLUDE_COMMENTS = NO
+    BODIES           = -130
+    BEGIN_TIME       = 2005 SEP 20 11:04:43.968
+    END_TIME         = 2005 SEP 20 11:09:50.669
+SOURCE_SPK_KERNEL = ~/remotedata/isis_data/hayabusa/kernels/tspk/de403s.bsp
+    INCLUDE_COMMENTS = NO
+    BODIES           = 10
+    BEGIN_TIME       = 2005 SEP 20 11:04:43.968
+    END_TIME         = 2005 SEP 20 11:09:50.669
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0_isis.lbl b/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0_isis.lbl
new file mode 100644
index 0000000..98b3250
--- /dev/null
+++ b/tests/pytests/data/2392975548_lvl3_0/2392975548_lvl3_0_isis.lbl
@@ -0,0 +1,401 @@
+Object = IsisCube
+  Object = Core
+    StartByte   = 65537
+    Format      = Tile
+    TileSamples = 1
+    TileLines   = 1
+
+    Group = Dimensions
+      Samples = 1
+      Lines   = 1
+      Bands   = 64
+    End_Group
+
+    Group = Pixels
+      Type       = Real
+      ByteOrder  = Lsb
+      Base       = 0.0
+      Multiplier = 1.0
+    End_Group
+  End_Object
+
+  Group = Instrument
+    SpacecraftName            = HAYABUSA
+    InstrumentId              = NIRS
+    SpacecraftClockStartCount = 1/2392973413.133
+    SpacecraftClockStopCount  = 1/2392975548.000
+    StartTime                 = 2005-09-20T11:06:43
+    StopTime                  = 2005-09-20T11:07:50
+    TotalIntegrationTime      = 13.10720 <SECOND>
+    IntegrationTime           = 25.6 <msec>
+    TargetName                = ITOKAWA
+  End_Group
+
+  Group = Archive
+    Pixel0Wavelength       = 787.16 <nm>
+    WavelengthInterval     = 23.56 <nm>
+    StackingEndTime        = 2392975548 <decimal>
+    SWHistMode             = Pixel
+    SWLIDARMode            = Normal
+    SWFLashMode            = Normal
+    SWRawMode              = STACK
+    SWDeviationOutput      = ON
+    SWMinMaxOutput         = ON
+    HWPower                = ON
+    HWChopper              = ON
+    HWChopperMode          = CHOP
+    HWTEC                  = ON
+    HWTECModeV             = "CLOSE:-9.5 deg" <V>
+    HWTECModeC             = -9.5 <C>
+    HWLamp                 = OFF
+    HWLED                  = OFF
+    DarkCurrentSubtraction = YES
+    YearDoy                = 2005263
+  End_Group
+
+  Group = BandBin
+    Width        = 0.02356 <micrometers>
+    Unit         = Micrometers
+    FilterNumber = (1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17,
+                    18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32,
+                    33, 34, 35, 36, 37, 38, 39, 40, 41, 42, 43, 44, 45, 46, 47,
+                    48, 49, 50, 51, 52, 53, 54, 55, 56, 57, 58, 59, 60, 61, 62,
+                    63, 64)
+    Center       = (0.7636, 0.78716, 0.81072, 0.83428, 0.85784, 0.8814,
+                    0.90496, 0.92852, 0.95208, 0.97564, 0.9992, 1.02276,
+                    1.04632, 1.06988, 1.09344, 1.117, 1.14056, 1.16412,
+                    1.18768, 1.21124, 1.2348, 1.25836, 1.28192, 1.30548,
+                    1.32904, 1.3526, 1.37616, 1.39972, 1.42328, 1.44684,
+                    1.4704, 1.49396, 1.51752, 1.54108, 1.56464, 1.5882,
+                    1.61176, 1.63532, 1.65888, 1.68244, 1.706, 1.72956,
+                    1.75312, 1.77668, 1.80024, 1.8238, 1.84736, 1.87092,
+                    1.89448, 1.91804, 1.9416, 1.96516, 1.98872, 2.01228,
+                    2.03584, 2.0594, 2.08296, 2.10652, 2.13008, 2.15364,
+                    2.1772, 2.20076, 2.22432, 2.24788)
+  End_Group
+
+  Group = Kernels
+    NaifFrameCode             = -130200
+    LeapSecond                = $base/kernels/lsk/naif0012.tls
+    TargetAttitudeShape       = ($base/kernels/pck/pck00009.tpc,
+                                 $hayabusa/kernels/pck/itokawa_gaskell_n3.tpc)
+    TargetPosition            = (Table, $hayabusa/kernels/tspk/de403s.bsp,
+                                 $hayabusa/kernels/tspk/sb_25143_140.bsp)
+    InstrumentPointing        = (Table,
+                                 $hayabusa/kernels/ck/hayabusa_itokawarendezvo-
+                                 us_v02n.bc,
+                                 $hayabusa/kernels/fk/hayabusa_hp.tf,
+                                 $hayabusa/kernels/fk/itokawa_fixed.tf)
+    Instrument                = $hayabusa/kernels/ik/nirs10.ti
+    SpacecraftClock           = $hayabusa/kernels/sclk/hayabusa.tsc
+    InstrumentPosition        = (Table,
+                                 $hayabusa/kernels/spk/hay_osbj_050911_051118_-
+                                 v1n.bsp)
+    InstrumentAddendum        = $hayabusa/kernels/iak/nirsAddendum002.ti
+    ShapeModel                = Null
+    InstrumentPositionQuality = Reconstructed
+    InstrumentPointingQuality = Reconstructed
+    CameraVersion             = 1
+    Source                    = isis
+  End_Group
+
+  Group = MissionData
+    PhaseAngle       = 8.38 <DEGREE>
+    IncidenceAngle   = 59.38 <DEGREE>
+    EmissionAngle    = 60.91 <DEGREE>
+    CenterLatitude   = 36.23 <DEGREE>
+    CenterLongitude  = 345.79 <DEGREE>
+    CornersLatitude  = (N/A, 29.62 <DEGREE>, 30.33 <DEGREE>, N/A)
+    CornersLongitude = (N/A, 346.92 <DEGREE>, 336.00 <DEGREE>, N/A)
+  End_Group
+End_Object
+
+Object = Label
+  Bytes = 65536
+End_Object
+
+Object = Table
+  Name                = InstrumentPointing
+  StartByte           = 72978
+  Bytes               = 64
+  Records             = 1
+  ByteOrder           = Lsb
+  TimeDependentFrames = (-130000, 1)
+  ConstantFrames      = (-130200, -130201, -130000)
+  ConstantRotation    = (4.16716354675321e-08, 0.99999999978068,
+                         2.09439095658742e-05, 0.99999802059666,
+                         6.12322187538694e-17, -0.0019896740344835,
+                         -0.0019896740340471, 2.09439510224007e-05,
+                         -0.99999802037734)
+  CkTableStartTime    = 180486501.50057
+  CkTableEndTime      = 180486501.50057
+  CkTableOriginalSize = 1
+  FrameTypeCode       = 3
+  Description         = "Created by spiceinit"
+  Kernels             = ($hayabusa/kernels/ck/hayabusa_itokawarendezvous_v02n-
+                         .bc, $hayabusa/kernels/fk/hayabusa_hp.tf,
+                         $hayabusa/kernels/fk/itokawa_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            = 73042
+  Bytes                = 56
+  Records              = 1
+  ByteOrder            = Lsb
+  CacheType            = Linear
+  SpkTableStartTime    = 180486501.50057
+  SpkTableEndTime      = 180486501.50057
+  SpkTableOriginalSize = 1.0
+  Description          = "Created by spiceinit"
+  Kernels              = $hayabusa/kernels/spk/hay_osbj_050911_051118_v1n.bsp
+
+  Group = Field
+    Name = J2000X
+    Type = Double
+    Size = 1
+  End_Group
+
+  Group = Field
+    Name = J2000Y
+    Type = Double
+    Size = 1
+  End_Group
+
+  Group = Field
+    Name = J2000Z
+    Type = Double
+    Size = 1
+  End_Group
+
+  Group = Field
+    Name = J2000XV
+    Type = Double
+    Size = 1
+  End_Group
+
+  Group = Field
+    Name = J2000YV
+    Type = Double
+    Size = 1
+  End_Group
+
+  Group = Field
+    Name = J2000ZV
+    Type = Double
+    Size = 1
+  End_Group
+
+  Group = Field
+    Name = ET
+    Type = Double
+    Size = 1
+  End_Group
+End_Object
+
+Object = Table
+  Name                = BodyRotation
+  StartByte           = 73098
+  Bytes               = 64
+  Records             = 1
+  ByteOrder           = Lsb
+  TimeDependentFrames = (2025143, 1)
+  CkTableStartTime    = 180486501.50057
+  CkTableEndTime      = 180486501.50057
+  CkTableOriginalSize = 1
+  FrameTypeCode       = 2
+  PoleRa              = (90.02564, 0.0, 0.0)
+  PoleDec             = (-67.02704, 0.0, 0.0)
+  PrimeMeridian       = (129.73, 712.1437611, 0.0)
+  Description         = "Created by spiceinit"
+  Kernels             = ($hayabusa/kernels/tspk/de403s.bsp,
+                         $hayabusa/kernels/tspk/sb_25143_140.bsp,
+                         $base/kernels/pck/pck00009.tpc,
+                         $hayabusa/kernels/pck/itokawa_gaskell_n3.tpc)
+  SolarLongitude      = 104.40427844844
+
+  Group = Field
+    Name = J2000Q0
+    Type = Double
+    Size = 1
+  End_Group
+
+  Group = Field
+    Name = J2000Q1
+    Type = Double
+    Size = 1
+  End_Group
+
+  Group = Field
+    Name = J2000Q2
+    Type = Double
+    Size = 1
+  End_Group
+
+  Group = Field
+    Name = J2000Q3
+    Type = Double
+    Size = 1
+  End_Group
+
+  Group = Field
+    Name = AV1
+    Type = Double
+    Size = 1
+  End_Group
+
+  Group = Field
+    Name = AV2
+    Type = Double
+    Size = 1
+  End_Group
+
+  Group = Field
+    Name = AV3
+    Type = Double
+    Size = 1
+  End_Group
+
+  Group = Field
+    Name = ET
+    Type = Double
+    Size = 1
+  End_Group
+End_Object
+
+Object = Table
+  Name                 = SunPosition
+  StartByte            = 73162
+  Bytes                = 56
+  Records              = 1
+  ByteOrder            = Lsb
+  CacheType            = Linear
+  SpkTableStartTime    = 180486501.50057
+  SpkTableEndTime      = 180486501.50057
+  SpkTableOriginalSize = 1.0
+  Description          = "Created by spiceinit"
+  Kernels              = ($hayabusa/kernels/tspk/de403s.bsp,
+                          $hayabusa/kernels/tspk/sb_25143_140.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 = 73218
+  Bytes     = 1384
+End_Object
+
+Object = OriginalLabel
+  Name      = IsisCube
+  StartByte = 66287
+  Bytes     = 6691
+End_Object
+
+Object = NaifKeywords
+  BODY_CODE                               = 2025143
+  BODY2025143_RADII                       = (0.274, 0.156, 0.138)
+  BODY_FRAME_CODE                         = 2025143
+  INS-130200_SWAP_OBSERVER_TARGET         = TRUE
+  INS-130200_LIGHTTIME_CORRECTION         = NONE
+  INS-130200_LT_SURFACE_CORRECT           = FALSE
+  INS-130200_FOCAL_LENGTH                 = 0.0272
+  INS-130200_PIXEL_PITCH                  = 0.047472922
+  CLOCK_ET_-130_1/2392973413.133_COMPUTED = 0fe04c880284a541
+  CLOCK_ET_-130_1/2392975548.000_COMPUTED = 1fb5b30d0384a541
+  INS-130200_TRANSX                       = (0.0, 0.0, -0.047472922)
+  INS-130200_TRANSY                       = (0.0, 0.047472922, 0.0)
+  INS-130200_ITRANSS                      = (0.0, 0.0, 21.064639754005)
+  INS-130200_ITRANSL                      = (0.0, -21.064639754005, 0.0)
+  INS-130200_BORESIGHT_LINE               = 0.0
+  INS-130200_BORESIGHT_SAMPLE             = 0.0
+End_Object
+End
diff --git a/tests/pytests/data/2392975548_lvl3_0/hayabusa.tsc b/tests/pytests/data/2392975548_lvl3_0/hayabusa.tsc
new file mode 100755
index 0000000..6db182f
--- /dev/null
+++ b/tests/pytests/data/2392975548_lvl3_0/hayabusa.tsc
@@ -0,0 +1,3462 @@
+KPL/SCLK
+
+\beginlabel
+PDS_VERSION_ID               = PDS3
+RECORD_TYPE                  = STREAM
+RECORD_BYTES                 = "N/A"
+^SPICE_KERNEL                = "hayabusa.tsc"
+MISSION_NAME                 = HAYABUSA
+SPACECRAFT_NAME              = HAYABUSA
+DATA_SET_ID                  = "HAY-A-SPICE-6-V1.0"
+KERNEL_TYPE_ID               = SCLK
+PRODUCT_ID                   = "hayabusa.tsc"
+PRODUCT_CREATION_TIME        = 2009-11-30T13:50:43
+PRODUCER_ID                  = JAXA
+MISSION_PHASE_NAME           = "N/A"
+PRODUCT_VERSION_TYPE         = ACTUAL
+PLATFORM_OR_MOUNTING_NAME    = "N/A"
+START_TIME                   = "N/A"
+STOP_TIME                    = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT  = "N/A"
+TARGET_NAME                  = "25143 ITOKAWA"
+INSTRUMENT_NAME              = "N/A"
+NAIF_INSTRUMENT_ID           = "N/A"
+SOURCE_PRODUCT_ID            = "N/A"
+NOTE                         = "See comments in the file for details"
+OBJECT                       = SPICE_KERNEL
+  INTERCHANGE_FORMAT         = ASCII
+  KERNEL_TYPE                = CLOCK_COEFFICIENTS
+  DESCRIPTION                = "SPICE Spacecraft Clock Kernel (SCLK) file
+containing clock correlation data for the Hayabusa on-board clock, created
+by the Hayabusa Joint Science Team. "
+END_OBJECT                   = SPICE_KERNEL
+\endlabel
+
+
+Hayabusa SCLK File
+===========================================================================
+
+   This file is a SPICE spacecraft clock (SCLK) kernel containing the
+   data necessary to convert between Hayabusa spacecraft on-board clock
+   time and ephemeris time.
+
+
+Production/History of this SCLK file
+--------------------------------------------------------
+
+   This file was produced by Dr. Naru Hirata of the Hayabusa Joint 
+   Science Team. 
+   
+   Although the SCLK_KERNEL_ID provided in the data section of the file
+   is set to September 6, 2005, the set of data included in the file
+   suggests that the file was created on or shortly after November 28,
+   2005.
+
+   The comments were added to the file by Boris Semenov, NAIF/JPL on
+   September 22, 2009, during preparation of Hayabusa SPICE data for
+   formal archiving in PDS. When the comments were added to the file,
+   the original file name (hayabusa.tsc) was not changed because no
+   data in the file were modified.
+
+
+Usage
+--------------------------------------------------------
+
+   This file must be loaded into the user's program by a call to the
+   FURNSH subroutine in order to use the SPICELIB SCLK family of
+   subroutines to convert Hayabusa spacecraft on-board clock to ET and
+   vice versa.
+
+
+SCLK Format
+--------------------------------------------------------
+
+   The on-board clock, the conversion for which is provided by this
+   SCLK file, consists of two fields:
+
+       MMMMMMMMMMM:FFF
+
+   where:
+
+       MMMMMMMMMMM -- count of major on-board clock ticks (131086 ... 
+                      39062500000); the nominal duration of one major
+                      on-board clock tick is approximately 1/32 of a
+                      second
+
+       FFF         -- count of minor on-board clock ticks (0 ... 255);
+                      the nominal duration of one minor on-board clock
+                      tick is approximately 1/8192 of a second
+
+
+Inquiries
+--------------------------------------------------------
+
+   If you have any questions regarding this file contact
+
+      Naru Hirata
+      naru@u-aizu.ac.jp
+      Department of Computer Software
+      The University of Aizu, Japan
+
+   or 
+
+      Boris V. Semenov
+      (818) 354-8136
+      Boris.Semenov@jpl.nasa.gov
+
+
+Kernel Data
+--------------------------------------------------------
+
+\begintext
+
+DESCRIPTION =" 
+
+This file contains the data necessary to convert between Hayabusa
+spacecraft clock time and ephemeris time. "
+ 
+
+\begindata
+
+SCLK_KERNEL_ID            = ( @2005-09-06 )
+
+SCLK_DATA_TYPE_130        = ( 1 )
+SCLK01_TIME_SYSTEM_130    = ( 1 )
+SCLK01_N_FIELDS_130       = ( 2 )
+SCLK01_MODULI_130         = ( 4294967296 256)
+SCLK01_OFFSETS_130        = ( 0 0)
+SCLK01_OUTPUT_DELIM_130   = ( 2 )
+SCLK_PARTITION_START_130  = ( 0.0000000000000E+00 )
+SCLK_PARTITION_END_130    = ( 1.0000000000000E+13 )
+
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+
+
+)
+\begintext
diff --git a/tests/pytests/data/2392975548_lvl3_0/hayabusa_hp.tf b/tests/pytests/data/2392975548_lvl3_0/hayabusa_hp.tf
new file mode 100755
index 0000000..fd7d0fd
--- /dev/null
+++ b/tests/pytests/data/2392975548_lvl3_0/hayabusa_hp.tf
@@ -0,0 +1,392 @@
+KPL/FK
+
+\beginlabel
+PDS_VERSION_ID               = PDS3
+RECORD_TYPE                  = STREAM
+RECORD_BYTES                 = "N/A"
+^SPICE_KERNEL                = "hayabusa_hp.tf"
+MISSION_NAME                 = HAYABUSA
+SPACECRAFT_NAME              = HAYABUSA
+DATA_SET_ID                  = "HAY-A-SPICE-6-V1.0"
+KERNEL_TYPE_ID               = FK
+PRODUCT_ID                   = "hayabusa_hp.tf"
+PRODUCT_CREATION_TIME        = 2009-11-30T13:50:41
+PRODUCER_ID                  = JAXA
+MISSION_PHASE_NAME           = "N/A"
+PRODUCT_VERSION_TYPE         = ACTUAL
+PLATFORM_OR_MOUNTING_NAME    = "N/A"
+START_TIME                   = "N/A"
+STOP_TIME                    = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT  = "N/A"
+TARGET_NAME                  = "25143 ITOKAWA"
+INSTRUMENT_NAME              = "N/A"
+NAIF_INSTRUMENT_ID           = "N/A"
+SOURCE_PRODUCT_ID            = "N/A"
+NOTE                         = "See comments in the file for details"
+OBJECT                       = SPICE_KERNEL
+  INTERCHANGE_FORMAT         = ASCII
+  KERNEL_TYPE                = FRAMES
+  DESCRIPTION                = "SPICE Frames Kernel (FK) file containing
+the definitions of the Hayabusa spacecraft frame and mission-specific
+dynamic frames, created by the Hayabusa Joint Science Team. The original
+name of this file was HAYABUSA_HP.TF. "
+END_OBJECT                   = SPICE_KERNEL
+\endlabel
+
+
+Hayabusa Frames Definition Kernel
+===========================================================================
+
+   This frame kernel contains a set of frame definitions for the 
+   Hayabusa mission. It also contains NAIF name-ID mappings for 
+   Hayabusa instruments.
+   
+
+Version and Date
+---------------------------------------------------------------------------
+
+   Version 1.0 -- Sep. 22, 2009 -- Boris Semenov, NAIF/JPL.
+
+      Lowercased file name (HAYABUSA_HP.TF -> hayabusa_hp.tf);
+
+      Corrected spacecraft name to be consistent with the duplicate
+      definitions provided in IKs (HAYABUSA_SC_BUS ->
+      HAYABUSA_SC_BUS_PRIME);
+
+      Added name-ID mapping keywords for science instruments;
+
+      Added comments describing frames defined in the IK and 
+      Itokawa FK;
+
+      Added other miscellaneous comments.
+
+   Version 1.0 -- Sep. 19, 2005 -- Naru Hirata, Aizu Univ.
+
+
+Hayabusa NAIF IDs
+---------------------------------------------------------------------------
+
+   The following names and NAIF ID codes are assigned to the Hayabusa 
+   spacecraft, its structures, and science instruments:
+
+      NAME                                    NAIF ID
+      -----------------------------------------------
+      HAYABUSA                                   -130
+      HAYABUSA_AMICA                          -130102
+      HAYABUSA_NIRS                           -130200
+      HAYABUSA_LIDAR                          -130300
+      HAYABUSA_XRS                            -130400
+
+   The keywords below implement the Hayabusa name-ID mappings.
+
+      \begindata
+
+         NAIF_BODY_NAME += ( 'HAYABUSA' )
+         NAIF_BODY_CODE += ( -130 )
+
+         NAIF_BODY_NAME += ( 'HAYABUSA_AMICA' )
+         NAIF_BODY_CODE += ( -130102 )
+
+         NAIF_BODY_NAME += ( 'HAYABUSA_NIRS' )
+         NAIF_BODY_CODE += ( -130200 )
+
+         NAIF_BODY_NAME += ( 'HAYABUSA_LIDAR' )
+         NAIF_BODY_CODE += ( -130300 )
+
+         NAIF_BODY_NAME += ( 'HAYABUSA_XRS' )
+         NAIF_BODY_CODE += ( -130400 )
+
+      \begintext
+
+
+Hayabusa Reference Frames
+---------------------------------------------------------------------------
+
+   The following reference frames for Hayabusa spacecraft, its
+   structures, and science instruments are defined in this FK and other
+   Hayabusa kernels (Itokawa FK, PCKs, and IKs):
+
+
+   Itokawa body-fixed frame (defined in a separate FK and PCKs):
+   -------------------------------------------------------------
+
+           Name                  Relative to           Type         Frame ID
+      ======================  =====================  ============   ========
+      ITOKAWA_FIXED           J2000                  PCK             2025143
+
+
+   Hayabusa spacecraft frame (duplicated in the IKs):
+   ----------------------------------------------------
+           
+           Name                  Relative to           Type         Frame ID
+      ======================  =====================  ============   ========
+      HAYABUSA_SC_BUS_PRIME   J2000                  CK              -130000
+
+
+   Hayabusa Science instrument frames (defined in the instrument IK files):
+   ------------------------------------------------------------------------
+
+           Name                  Relative to           Type         Frame ID
+      ======================  =====================  ============   ========
+      HAYABUSA_AMICA_IDEAL    HAYABUSA_SC_BUS_PRIME  FIXED           -130101
+      HAYABUSA_AMICA          HAYABUSA_AMICA         FIXED           -130102
+
+      HAYABUSA_NIRS_IDEAL     HAYABUSA_SC_BUS_PRIME  FIXED           -130201
+      HAYABUSA_NIRS           HAYABUSA_NIRS_IDEAL    FIXED           -130200
+
+      HAYABUSA_LIDAR_IDEAL    HAYABUSA_SC_BUS_PRIME  FIXED           -130301
+      HAYABUSA_LIDAR          HAYABUSA_LIDAR_IDEAL   FIXED           -130300
+
+      HAYABUSA_XRS_IDEAL      HAYABUSA_SC_BUS_PRIME  FIXED           -130410
+      HAYABUSA_XRS            HAYABUSA_XRS_IDEAL     FIXED           -130400
+
+
+   Hayabusa-specific dynamic frames:
+   ---------------------------------
+
+           Name                  Relative to           Type         Frame ID
+      ======================  =====================  ============   ========
+      HAYABUSA_HP_FRAME       J2000                  DYNAMIC         -130900
+      ITOKAWA_-Z_SUN_+X       J2000                  DYNAMIC         -130910
+      EARTH_ITOKAWA_P         J2000                  DYNAMIC         -130920
+   
+
+Hayabusa Reference Frame Tree
+---------------------------------------------------------------------------
+
+
+   This diagram shows the Hayabusa frame tree:
+
+
+                               "J2000" INERTIAL
+         +-----------------------------------------------------------+
+         |                   |         |         |                   |
+         |<-dynamic          |         |         |          dynamic->|
+         |                   |         |         |                   |
+         V                   |         |         |                   V
+    "HAYABUSA_HP_FRAME"      |         |         |        "ITOKAWA_-Z_SUN_+X"
+    -------------------      |         |         |        -------------------
+                             |         |         |
+                             |         |         |
+                    dynamic->|         |         |<-pck
+                             |         |         |
+                             V         |         V
+                 "EARTH_ITOKAWA_P"     |   "ITOKAWA_FIXED"
+                 -----------------     |   ---------------
+                                       |
+                                       |
+                                       |<-ck
+                                       |
+                                       V
+                           "HAYABUSA_SC_BUS_PRIME"
+         +-----------------------------------------------------------+
+         |                   |                   |                   |
+         |                   |<-fixed            |                   |<-fixed
+         |                   |                   |                   |
+         |                   V                   |                   V
+         |         "HAYABUSA_NIRS_IDEAL"         |        "HAYABUSA_XRS_IDEAL"
+         |         ---------------------         |        --------------------
+         |                   |                   |                   |
+         |                   |<-fixed            |                   |<-fixed
+         |                   |                   |                   |
+         |                   V                   |                   V
+         |            "HAYABUSA_NIRS"            |             "HAYABUSA_XRS"
+         |            ---------------            |             --------------
+         |                                       | 
+         |                                       | 
+         |<-fixed                                |<-fixed 
+         |                                       | 
+         V                                       V
+   "HAYABUSA_AMICA_IDEAL"               "HAYABUSA_LIDAR_IDEAL"
+   ----------------------               ----------------------
+         |                                       | 
+         |<-fixed                                |<-fixed 
+         |                                       | 
+         V                                       V
+     "HAYABUSA_AMICA"                      "HAYABUSA_LIDAR"
+     ----------------                      ----------------
+
+
+Itokawa Body-Fixed Frame
+---------------------------------------------------------------------------
+
+   The Itokawa body-fixed frame, ITOKAWA_FIXED, is defined in a 
+   separate FK file (itokawa_fixed.tf). Its definition is also
+   duplicated in some of the Itokawa PCK files.
+
+
+Hayabusa Spacecraft Frame
+---------------------------------------------------------------------------
+
+   The Hayabusa spacecraft frame, HAYABUSA_SC_BUS_PRIME, is defined 
+   as follows:
+
+      - +Z axis is parallel to the nominal HGA boresight;
+
+      - +X axis is parallel to the ion engines thrust vector;
+
+      - +Y axis completes the right-handed frame;
+
+   The Hayabusa spacecraft frame shown on this diagram:
+
+                                      ^
+                                      | HGA Boresight
+                                      |
+
+                                      ^ 
+                                     / \  HGA
+                            --------------------
+                             \                 /
+                              \        +Z     /
+                         --------     ^    ---------
+                         |            |            | Ion Engines
+                         |            |            |_
+                         |            |      +X    |_]  
+                         |            x----->      |_]   ----->
+                        _|          +Y             |     Thrust Vector
+                  NIRS | |                         |
+                          ----| |---------------| |-
+                           | | LIDAR             XRS
+                           | |
+                  Sample   | |        |
+                   horn    | |        |  Science Instrument
+                          /   \       V     Boresights
+
+
+   This frame is defined as a CK-based frame below. The frame
+   definition is also duplicated in Hayabusa science instrument IKs.
+
+      \begindata
+
+         FRAME_HAYABUSA_SC_BUS_PRIME  = -130000
+         FRAME_-130000_NAME           = 'HAYABUSA_SC_BUS_PRIME'
+         FRAME_-130000_CLASS          = 3
+         FRAME_-130000_CLASS_ID       = -130000
+         FRAME_-130000_CENTER         = -130
+         CK_-130000_SCLK              = -130
+         CK_-130000_SPK               = -130
+
+      \begintext
+
+
+Hayabusa Science Instrument Frames
+---------------------------------------------------------------------------
+
+   Hayabusa science instrument frames are defined in the IK files.
+
+
+Hayabusa-Specific Dynamic Frames
+---------------------------------------------------------------------------
+
+   The HAYABUSA_HP_FRAME frame, used as the reference frame in the
+   Hayabusa SPKs produces by JAXA, is defined as follows:
+
+      - +Z axis is along the geometric direction from Itokawa to the
+        Earth
+
+      - +X axis is as close as possible to the geometric direction 
+        from Itokawa to the Sun
+
+      - +Y axis completes the right-handed frame;
+
+   This frame is defined as a two-vector style dynamic frame below.
+   
+      \begindata
+
+         FRAME_HAYABUSA_HP            = -130900
+         FRAME_-130900_NAME           = 'HAYABUSA_HP'
+         FRAME_-130900_CLASS          = 5
+         FRAME_-130900_CLASS_ID       = -130900
+         FRAME_-130900_CENTER         = 2025143
+         FRAME_-130900_RELATIVE       = 'J2000'
+         FRAME_-130900_DEF_STYLE      = 'PARAMETERIZED'
+         FRAME_-130900_FAMILY         = 'TWO-VECTOR'
+         FRAME_-130900_PRI_AXIS       = 'Z'
+         FRAME_-130900_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION'
+         FRAME_-130900_PRI_OBSERVER   = 2025143
+         FRAME_-130900_PRI_TARGET     = 'EARTH'
+         FRAME_-130900_PRI_ABCORR     = 'NONE'
+         FRAME_-130900_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION'
+         FRAME_-130900_SEC_OBSERVER   = 2025143
+         FRAME_-130900_SEC_TARGET     = 'SUN'
+         FRAME_-130900_SEC_AXIS       = 'X'
+         FRAME_-130900_SEC_ABCORR     = 'NONE'
+
+      \begintext
+
+
+   The ITOKAWA_-Z_SUN_+X frame, representing the nominal Itokawa-pointed
+   orientation, is defined as follows:
+
+      - -Z axis is along the geometric direction from Hayabusa to
+        Itokawa
+
+      - +X axis is as close as possible to the geometric direction from
+        Hayabusa to the Sun
+
+      - +Y axis completes the right-handed frame;
+
+   This frame is defined as a two-vector style dynamic frame below.
+
+      \begindata
+
+         FRAME_ITOKAWA_-Z_SUN_+X      = -130910
+         FRAME_-130910_NAME           = 'ITOKAWA_-Z_SUN_+X'
+         FRAME_-130910_CLASS          = 5
+         FRAME_-130910_CLASS_ID       = -130910
+         FRAME_-130910_CENTER         = -130
+         FRAME_-130910_RELATIVE       = 'J2000'
+         FRAME_-130910_DEF_STYLE      = 'PARAMETERIZED'
+         FRAME_-130910_FAMILY         = 'TWO-VECTOR'
+         FRAME_-130910_PRI_AXIS       = '-Z'
+         FRAME_-130910_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION'
+         FRAME_-130910_PRI_OBSERVER   = -130
+         FRAME_-130910_PRI_TARGET     = 2025143
+         FRAME_-130910_PRI_ABCORR     = 'NONE'
+         FRAME_-130910_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION'
+         FRAME_-130910_SEC_OBSERVER   = -130
+         FRAME_-130910_SEC_TARGET     = 'SUN'
+         FRAME_-130910_SEC_AXIS       = 'X'
+         FRAME_-130910_SEC_ABCORR     = 'NONE'
+
+      \begintext
+
+
+   The EARTH_ITOKAWA_P frame is defined as follows:
+
+      - +Z axis is along the geometric direction from the Earth to
+        Itokawa
+
+      - +Y axis is as close as possible to the geometric direction from
+        the Earth to the Sun
+
+      - +X axis completes the right-handed frame;
+
+   This frame is defined as a two-vector style dynamic frame below.
+
+      \begindata
+
+         FRAME_EARTH_ITOKAWA_P        = -130920
+         FRAME_-130920_NAME           = 'EARTH_ITOKAWA_P'
+         FRAME_-130920_CLASS          = 5
+         FRAME_-130920_CLASS_ID       = -130920
+         FRAME_-130920_CENTER         = 399
+         FRAME_-130920_RELATIVE       = 'J2000'
+         FRAME_-130920_DEF_STYLE      = 'PARAMETERIZED'
+         FRAME_-130920_FAMILY         = 'TWO-VECTOR'
+         FRAME_-130920_PRI_AXIS       = 'Z'
+         FRAME_-130920_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION'
+         FRAME_-130920_PRI_OBSERVER   = 'EARTH'
+         FRAME_-130920_PRI_TARGET     = 2025143
+         FRAME_-130920_PRI_ABCORR     = 'NONE'
+         FRAME_-130920_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION'
+         FRAME_-130920_SEC_OBSERVER   = 'EARTH'
+         FRAME_-130920_SEC_TARGET     = 'SUN'
+         FRAME_-130920_SEC_AXIS       = 'Y'
+         FRAME_-130920_SEC_ABCORR     = 'NONE'
+
+     \begintext
+
+
+End of FK file.
diff --git a/tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_0_sliced_-130000.xc b/tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_0_sliced_-130000.xc
new file mode 100644
index 0000000..f7b2965
--- /dev/null
+++ b/tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_0_sliced_-130000.xc
@@ -0,0 +1,56 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK  '
+'2'
+'6'
+'HAYABUSA S/C ATTITUDE                                       '
+BEGIN_ARRAY 1 35
+'HAYABUSA S/C ATTITUDE                   '
+'8EA18B4B85^A'
+'8EA1B1D732^A'
+'-1FBD0'
+'1'
+'3'
+'1'
+35
+'8BA142187DFB4^0'
+'5094EC77B2BA54^0'
+'-AB9C9B9D0EA3D8^0'
+'6479EC1B2DCAB^0'
+'11D7870BA38^-6'
+'1B604FE2ADC806^-4'
+'F53927DE6EB42^-5'
+'8B9DA3138E081^0'
+'509AF6BDB14E44^0'
+'-AB9C01A71924B^0'
+'647B22F732861C^0'
+'66F5C84D53E6B4^-4'
+'33935D6FF25D32^-4'
+'1F60D50AAF5E1B^-4'
+'8BA02C68AAAB6^0'
+'50973E4BF26B14^0'
+'-ABAAAAA97514B^0'
+'64618AAA220764^0'
+'4F6BBFBB42D5C4^-4'
+'-3E92B2B1C6FD12^-4'
+'-1ED85C91CE00A7^-4'
+'8BA8B732ACDAD8^0'
+'508974F1A13A98^0'
+'-ABABB657142FC8^0'
+'645EEF5A4874DC^0'
+'-151CBD15BAEFC9^-4'
+'-3F7E9F1B8893BC^-4'
+'-24B1A7A465C88A^-4'
+'8EA18B4B85^A'
+'8EA197E001AF28^A'
+'8EA1A7E0035DF^A'
+'8EA1B1D732^A'
+'8EA18B4B85^A'
+'1^1'
+'4^1'
+END_ARRAY 1 35
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: ~/data/isistestdata/hayabusa/nirs/2392975548_lvl3_0.ale.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_1_sliced_-130000.xc b/tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_1_sliced_-130000.xc
new file mode 100644
index 0000000..3a581b1
--- /dev/null
+++ b/tests/pytests/data/2392975548_lvl3_0/hayabusa_itokawarendezvous_v02n_1_sliced_-130000.xc
@@ -0,0 +1,120 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK  '
+'2'
+'6'
+'HAYABUSA S/C ATTITUDE                                       '
+BEGIN_ARRAY 1 99
+'HAYABUSA S/C ATTITUDE                   '
+'8EA1D1656C^A'
+'8EA1F7BC19^A'
+'-1FBD0'
+'1'
+'3'
+'1'
+99
+'8BAC935814D8A8^0'
+'5083C19F10C4E^0'
+'-AB9E2D3CF59A9^0'
+'64754652318348^0'
+'-9682518AF744A8^-5'
+'1FA58BF555BE56^-4'
+'1CA5922433E4AA^-4'
+'8BAB729B6C3BF^0'
+'5086CFBE811EC8^0'
+'-AB9DCCB188C75^0'
+'647509CCA04A54^0'
+'-249F661FA151D2^-5'
+'28EC3E88292384^-4'
+'23AEDC32845414^-4'
+'8BA7E8BFD965B8^0'
+'50911E306560F^0'
+'-ABA0598369693^0'
+'646D561A806F1C^0'
+'-15E52076AD6803^-4'
+'3FBED909FDDE9A^-4'
+'-3B6800C64BEC82^-4'
+'8BA64D60463B6^0'
+'50910DF79ABDC8^0'
+'-ABA156AA12E5D^0'
+'646DEE89199C58^0'
+'66F4F4D09DC0F8^-4'
+'5A4BBC498F306^-4'
+'5B5CDE8EEE152C^-4'
+'8BA68AFF460A78^0'
+'50925206F19E^0'
+'-ABA33DC0838DD^0'
+'64695455D4BF1^0'
+'-E132E669A2DA7^-5'
+'4207DF589FEF88^-4'
+'813F19E633FFB8^-5'
+'8BA51EBBBBF1A^0'
+'509389F8880D58^0'
+'-ABA41D67C91B4^0'
+'6468D650F743F^0'
+'9761139106E4D8^-5'
+'-73FB6A0E0D1274^-4'
+'108421FC1634FC^-5'
+'8BA7A7E26CF068^0'
+'5091FA488DE668^0'
+'-ABA23E575AEEC8^0'
+'6469C31902D0A4^0'
+'-F5CB1F11A2E76^-5'
+'-134F53B558F9C3^-5'
+'-2CC181B83629D2^-4'
+'8BA6FB3F420298^0'
+'5091497FB7B408^0'
+'-ABA2798CCE0058^0'
+'646ADBD63FB24^0'
+'7B7B4881DF1D04^-5'
+'103F021EBD174D^-4'
+'5DF0B9C5582628^-4'
+'8BA7DE51E6F11^0'
+'509352A691378C^0'
+'-ABA1EC23CDAC2^0'
+'6468EF9081B74C^0'
+'15E7BFA42574B6^-4'
+'23DD3D29177CF8^-4'
+'-71C6105E09417C^-5'
+'8BA73ED07779C8^0'
+'50933D7267763^0'
+'-ABA2DF4832353^0'
+'64683ED01A11C8^0'
+'-2CDED1E10D9A12^-4'
+'-2D1AD488D940EE^-4'
+'-3248A2CC68A8D8^-4'
+'8BA721F95B5FE^0'
+'50926608EAE174^0'
+'-ABA20C403C6FB^0'
+'646A7C7ED86E08^0'
+'C5AFA258A01D68^-4'
+'-35A9145D304ACC^-4'
+'-301C6E8ED5983E^-5'
+'8BA7D06FB55D68^0'
+'50917A9F782478^0'
+'-ABA264C1149D78^0'
+'6469AF78A4404^0'
+'286EBE0B14597A^-4'
+'-EB91DC08E5A418^-5'
+'132100BC924F5B^-4'
+'8EA1D1656C^A'
+'8EA1D7E00038F^A'
+'8EA1E7E001E7B^A'
+'8EA1E949022BD^A'
+'8EA1EB48FD42F^A'
+'8EA1ED49008B4^A'
+'8EA1EF4903D388^A'
+'8EA1F148FEEAA8^A'
+'8EA1F3490232F8^A'
+'8EA1F548FD4A08^A'
+'8EA1F74900925^A'
+'8EA1F7BC19^A'
+'8EA1D1656C^A'
+'1^1'
+'C^1'
+END_ARRAY 1 99
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: ~/data/isistestdata/hayabusa/nirs/2392975548_lvl3_0.ale.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/2392975548_lvl3_0/itokawa_fixed.tf b/tests/pytests/data/2392975548_lvl3_0/itokawa_fixed.tf
new file mode 100755
index 0000000..1a6630f
--- /dev/null
+++ b/tests/pytests/data/2392975548_lvl3_0/itokawa_fixed.tf
@@ -0,0 +1,94 @@
+KPL/FK
+
+\beginlabel
+PDS_VERSION_ID               = PDS3
+RECORD_TYPE                  = STREAM
+RECORD_BYTES                 = "N/A"
+^SPICE_KERNEL                = "itokawa_fixed.tf"
+MISSION_NAME                 = HAYABUSA
+SPACECRAFT_NAME              = HAYABUSA
+DATA_SET_ID                  = "HAY-A-SPICE-6-V1.0"
+KERNEL_TYPE_ID               = FK
+PRODUCT_ID                   = "itokawa_fixed.tf"
+PRODUCT_CREATION_TIME        = 2009-11-30T13:50:41
+PRODUCER_ID                  = JAXA
+MISSION_PHASE_NAME           = "N/A"
+PRODUCT_VERSION_TYPE         = ACTUAL
+PLATFORM_OR_MOUNTING_NAME    = "N/A"
+START_TIME                   = "N/A"
+STOP_TIME                    = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT  = "N/A"
+TARGET_NAME                  = "25143 ITOKAWA"
+INSTRUMENT_NAME              = "N/A"
+NAIF_INSTRUMENT_ID           = "N/A"
+SOURCE_PRODUCT_ID            = "N/A"
+NOTE                         = "See comments in the file for details"
+OBJECT                       = SPICE_KERNEL
+  INTERCHANGE_FORMAT         = ASCII
+  KERNEL_TYPE                = FRAMES
+  DESCRIPTION                = "SPICE Frames Kernel (FK) file containing
+the definition of the asteroid Itokawa body-fixed frame, created by the
+Hayabusa Joint Science Team. "
+END_OBJECT                   = SPICE_KERNEL
+\endlabel
+
+
+ITOKAWA Body-Fixed Frame Definition Kernel
+===========================================================================
+
+   This frame kernel contains asteroid ITOKAWA body-fixed frame definition.
+
+   
+Version and Date
+--------------------------------------------------------
+
+   Version 1.0 -- May 25, 2004 -- Naru Hirata
+
+      Initial release.
+
+
+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.
+
+
+ITOKAWA Body-Fixed Frame
+--------------------------------------------------------
+
+   This kernel file defines asteroid ITOKAWA body-frame, ITOKAWA_FIXED, with
+   the frame ID code 2025143 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_ITOKAWA_FIXED    =  2025143
+      FRAME_2025143_NAME     = 'ITOKAWA_FIXED'
+      FRAME_2025143_CLASS    =  2
+      FRAME_2025143_CLASS_ID =  2025143
+      FRAME_2025143_CENTER   =  2025143
+
+      OBJECT_2025143_FRAME   = 'ITOKAWA_FIXED'
+
+   \begintext
+
diff --git a/tests/pytests/data/2392975548_lvl3_0/itokawa_gaskell_n3.tpc b/tests/pytests/data/2392975548_lvl3_0/itokawa_gaskell_n3.tpc
new file mode 100755
index 0000000..e8abb4d
--- /dev/null
+++ b/tests/pytests/data/2392975548_lvl3_0/itokawa_gaskell_n3.tpc
@@ -0,0 +1,115 @@
+KPL/PCK
+
+\beginlabel
+PDS_VERSION_ID               = PDS3
+RECORD_TYPE                  = STREAM
+RECORD_BYTES                 = "N/A"
+^SPICE_KERNEL                = "itokawa_gaskell_n3.tpc"
+MISSION_NAME                 = HAYABUSA
+SPACECRAFT_NAME              = HAYABUSA
+DATA_SET_ID                  = "HAY-A-SPICE-6-V1.0"
+KERNEL_TYPE_ID               = PCK
+PRODUCT_ID                   = "itokawa_gaskell_n3.tpc"
+PRODUCT_CREATION_TIME        = 2009-11-30T13:50:42
+PRODUCER_ID                  = "R.GASKELL/PSI"
+MISSION_PHASE_NAME           = "N/A"
+PRODUCT_VERSION_TYPE         = ACTUAL
+PLATFORM_OR_MOUNTING_NAME    = "N/A"
+START_TIME                   = "N/A"
+STOP_TIME                    = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT  = "N/A"
+TARGET_NAME                  = "25143 ITOKAWA"
+INSTRUMENT_NAME              = "N/A"
+NAIF_INSTRUMENT_ID           = "N/A"
+SOURCE_PRODUCT_ID            = "N/A"
+NOTE                         = "See comments in the file for details"
+OBJECT                       = SPICE_KERNEL
+  INTERCHANGE_FORMAT         = ASCII
+  KERNEL_TYPE                = TARGET_CONSTANTS
+  DESCRIPTION                = "SPICE Planetary Constants Kernel (PCK) file
+containing the asteroid Itokawa radii values, body-fixed frame definition,
+and rotation constants derived by Dr. Robert W. Gaskell, PSI. The original
+name of this files was Itokawa_Gaskell_n3.tpc. It contains the rotation
+constants consistent with the Itokawa shape models archived in the PDS data
+set HAY-A-AMICA-5-ITOKAWASHAPE-V1.0. "
+END_OBJECT                   = SPICE_KERNEL
+\endlabel
+
+
+Asteroid Itokawa P_constants (PcK) SPICE kernel file
+===========================================================================
+
+     By Hayabusa Joint Science Team, <unknown date>; miscellaneous comments
+     added by Boris Semenov, NAIF/JPL, on September 24, 2009.
+
+
+Summary
+--------------------------------------------------------
+
+     This PCK file contains Itokawa rotation constants, radii and 
+     the definition of the Itokawa body-fixed frame, ITOKAWA_FIXED.
+
+     The Itokawa rotation constants provided in this PCK are 
+     from the data set catalog file for the Itokawa shape model 
+     data set (HAY-A-AMICA-5-ITOKAWASHAPE-V1.0) by the Dr. Robert W. 
+     Gaskell, PSI.
+
+
+Rotation constants for asteroid Itokawa
+--------------------------------------------------------
+
+     Itokawa rotation constants are provided in the keywords below.   
+ 
+     \begindata
+ 
+        BODY2025143_POLE_RA    = ( 90.02564    0.0              0.0 )
+        BODY2025143_POLE_DEC   = (-67.02704   0.0              0.0 )
+        BODY2025143_PM         = (129.73000   712.14376110          0.0 )
+ 
+     \begintext
+
+
+Radii for asteroid ITOKAWA
+--------------------------------------------------------
+     
+     The Itokawa radii are provided in the keyword below.
+
+     \begindata
+ 
+        BODY2025143_RADII      = ( 0.274  0.156  0.138  )
+ 
+     \begintext
+
+
+ITOKAWA_FIXED Frame Definition
+--------------------------------------------------------
+
+     The ITOKAWA fixed frame is defined in the same as any other PCK
+     frame:
+ 
+        *  +Z along the North pole;
+      
+        *  +X toward the prime meridian;
+      
+        *  +Y completes the right hand frame;
+      
+        *  the origin of this frame is at the center of the body.
+      
+     The orientation of this frame is computed by evaluating
+     corresponding rotation constants provided in this PCK file.
+
+     \begindata
+
+        FRAME_ITOKAWA_FIXED      =  2025143
+        FRAME_2025143_NAME     = 'ITOKAWA_FIXED'
+        FRAME_2025143_CLASS    =  2
+        FRAME_2025143_CLASS_ID =  2025143
+        FRAME_2025143_CENTER   =  2025143
+
+        OBJECT_2025143_FRAME   = 'ITOKAWA_FIXED'
+
+     \begintext
+
+
+End of PCK file.
diff --git a/tests/pytests/data/2392975548_lvl3_0/naif0012.tls b/tests/pytests/data/2392975548_lvl3_0/naif0012.tls
new file mode 100755
index 0000000..e1afdee
--- /dev/null
+++ b/tests/pytests/data/2392975548_lvl3_0/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/2392975548_lvl3_0/nirs10.ti b/tests/pytests/data/2392975548_lvl3_0/nirs10.ti
new file mode 100755
index 0000000..0bf1a61
--- /dev/null
+++ b/tests/pytests/data/2392975548_lvl3_0/nirs10.ti
@@ -0,0 +1,184 @@
+KPL/IK
+
+\beginlabel
+PDS_VERSION_ID               = PDS3
+RECORD_TYPE                  = STREAM
+RECORD_BYTES                 = "N/A"
+^SPICE_KERNEL                = "nirs10.ti"
+MISSION_NAME                 = HAYABUSA
+SPACECRAFT_NAME              = HAYABUSA
+DATA_SET_ID                  = "HAY-A-SPICE-6-V1.0"
+KERNEL_TYPE_ID               = IK
+PRODUCT_ID                   = "nirs10.ti"
+PRODUCT_CREATION_TIME        = 2009-11-30T13:50:42
+PRODUCER_ID                  = JAXA
+MISSION_PHASE_NAME           = "N/A"
+PRODUCT_VERSION_TYPE         = ACTUAL
+PLATFORM_OR_MOUNTING_NAME    = "HAYABUSA SPACECRAFT BUS"
+START_TIME                   = "N/A"
+STOP_TIME                    = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT  = "N/A"
+TARGET_NAME                  = "25143 ITOKAWA"
+INSTRUMENT_NAME              = "NEAR INFRARED SPECTROMETER"
+NAIF_INSTRUMENT_ID           = -130200
+SOURCE_PRODUCT_ID            = "N/A"
+NOTE                         = "See comments in the file for details"
+OBJECT                       = SPICE_KERNEL
+  INTERCHANGE_FORMAT         = ASCII
+  KERNEL_TYPE                = INSTRUMENT
+  DESCRIPTION                = "SPICE I-Kernel (IK) file containing FOV and
+reference frame definitions for the Hayabusa Near InfraRed Spectrometer
+(NIRS) instrument, created by the Hayabusa Joint Science Team. "
+END_OBJECT                   = SPICE_KERNEL
+\endlabel
+
+
+Hayabusa NIRS Instrument and Frame Kernel Kile
+===========================================================================
+
+   This instrument kernel (I-kernel) contains the frames and FOV 
+   definitions for Hayabusa Near-Infrared Spectrometer (NIRS).
+
+
+Version and Date
+---------------------------------------------------------------------------
+
+   Version 1.0 by Boris Semenov, NAIF/JPL 23 Sep. 2009
+
+      Corrected _RELATIVE frame in the _NIRS_IDEAL frame definition
+      (HAYABUSA_SC_BUS -> HAYABUSA_SC_BUS_PRIME). Added miscellaneous
+      comments. File name and version were not changed.
+
+   Version 1.0 by Shinsuke Abe, Kobe Univ. 9 Sep. 2005
+
+   Version 0.0 (prototype) by Masanao Abe, ISAS/JAXA, 4 June 2005
+
+
+Implementation Notes
+---------------------------------------------------------------------------
+
+   Applications that need SPICE I-kernel data must ``load'' the
+   I-kernel file, normally during program initialization. Loading the
+   kernel using the SPICELIB routine FURNSH causes the data items and
+   their associated values present in the kernel to become associated
+   with a data structure called the ``kernel pool''. The application
+   program may then obtain the value(s) for any IK data item using the
+   SPICELIB routines GDPOOL, GIPOOL, GCPOOL. Routine GETFOV may be used
+   if the file contains instrument field-of-view (FOV) specification.
+   The frame definitions information is accessed via any interfaces
+   utilizing SPICE frames subsystem (PXFORM, etc).
+
+   This file was created with, and can be updated with a text editor or
+   word processor.
+
+
+Conventions for Specifying Data
+---------------------------------------------------------------------------
+
+   Instrument data items are specified using ``keyword=value''
+   assignments. All keywords referencing instrument values in this
+   I-kernel start with the characters `INS' followed by the NAIF
+   instrument ID code for NIRS, -130200. The remainder of the keyword
+   is an underscore character followed by the unique name of the data
+   item. For example, NIRS boresight vector is specified by
+
+               INS-130200_BORESIGHT
+
+   The upper bound on the length of all keywords is 32 characters.
+
+
+Hayabusa Spacecraft Frame Definition
+---------------------------------------------------------------------------
+
+   This HAYABUSA_SC_BUS_PRIME frame definition is a copy of the
+   definition provided in the main Hayabusa FK file. It is included in
+   this IK file for historical reasons.
+
+\begindata
+
+   FRAME_HAYABUSA_SC_BUS_PRIME  = -130000
+   FRAME_-130000_NAME        = 'HAYABUSA_SC_BUS_PRIME'
+   FRAME_-130000_CLASS       = 3
+   FRAME_-130000_CLASS_ID    = -130000
+   FRAME_-130000_CENTER      = -130
+   CK_-130000_SCLK           = -130
+   CK_-130000_SPK            = -130
+
+\begintext
+
+
+NIRS Frame Definitions
+---------------------------------------------------------------------------
+
+   Two frames are defined for NIRS: HAYABUSA_NIRS_IDEAL and
+   HAYABUSA_NIRS. 
+
+   The HAYABUSA_NIRS_IDEAL frame incorporates the ideal fixed
+   instrument alignment relative to the spacecraft frame,
+   HAYABUSA_SC_BUS_PRIME. The +Z axis of the HAYABUSA_NIRS_IDEAL frame
+   is along the ideally-mounted instrument boresight.
+
+   The HAYABUSA_NIRS frame incorporates the the actual instrument
+   misalignment relative to its ideal orientation represented by the
+   HAYABUSA_NIRS_IDEAL frame. The +Z axis of this frame is along the
+   actual instrument boresight.
+
+   Both frames are defined as fixed offset frames with their
+   orientation specified using Euler angles.
+ 
+   Note that angles in the frame definitions are specified for "from
+   instrument to base (relative to) frame" transformation.
+
+\begindata
+
+   FRAME_HAYABUSA_NIRS       = -130200
+   FRAME_-130200_NAME        = 'HAYABUSA_NIRS'
+   FRAME_-130200_CLASS       = 4
+   FRAME_-130200_CLASS_ID    = -130200
+   FRAME_-130200_CENTER      = -130
+   TKFRAME_-130200_SPEC      = 'ANGLES'
+   TKFRAME_-130200_RELATIVE  = 'HAYABUSA_NIRS_IDEAL'
+   TKFRAME_-130200_ANGLES    = ( -0.1140, -0.0012,  0.0 ) 
+   TKFRAME_-130200_AXES      = (    1,     2,     3 )
+   TKFRAME_-130200_UNITS     = 'DEGREES'
+
+   FRAME_HAYABUSA_NIRS_IDEAL = -130201
+   FRAME_-130201_NAME        = 'HAYABUSA_NIRS_IDEAL'
+   FRAME_-130201_CLASS       = 4
+   FRAME_-130201_CLASS_ID    = -130201
+   FRAME_-130201_CENTER      = -130
+   TKFRAME_-130201_SPEC      = 'ANGLES'
+   TKFRAME_-130201_RELATIVE  = 'HAYABUSA_SC_BUS_PRIME'
+   TKFRAME_-130201_ANGLES    = (  0.0, 180.0, -90.0 )
+   TKFRAME_-130201_AXES      = (     1,     2,    3 )
+   TKFRAME_-130201_UNITS     = 'DEGREES'
+
+\begintext
+   
+
+NIRS Field-Of-View Definition
+---------------------------------------------------------------------------
+
+   The NIRS FOV is defined using a corner-style definition as a 0.1 by
+   0.1 degree square pyramid centered around the boresight that points
+   along the +Z axis of the HAYABUSA_NIRS frame. The FOV shape is set
+   to 'POLYGON'; it could also have been set to 'RECTANGLE'.  The
+   corner direction vectors are given counterclockwise as seen from
+   boresight.
+ 
+\begindata
+        
+   INS-130200_FOV_FRAME  = 'HAYABUSA_NIRS'
+   INS-130200_FOV_SHAPE  = 'POLYGON'
+   INS-130200_BORESIGHT  = ( 0.0   0.0   1.0 )
+   INS-130200_FOV_BOUNDARY_CORNERS = (
+                                         0.000872664    0.000872664   1.0
+                                        -0.000872664    0.000872664   1.0
+                                        -0.000872664   -0.000872664   1.0
+                                         0.000872664   -0.000872664   1.0
+                                       )
+
+\begintext
+
+End of IK file.
diff --git a/tests/pytests/data/2392975548_lvl3_0/nirsAddendum002.ti b/tests/pytests/data/2392975548_lvl3_0/nirsAddendum002.ti
new file mode 100755
index 0000000..0426f06
--- /dev/null
+++ b/tests/pytests/data/2392975548_lvl3_0/nirsAddendum002.ti
@@ -0,0 +1,34 @@
+\begintext
+The focal length was calculated from f# = 1 and aperture = 27.2 mm 
+See: http://sbn.psi.edu/pds/asteroid/HAY_A_NIRS_3_NIRSCAL_V1_0/document/nirscalpaper.pdf
+The units for focal length are meters and the units for pixel pitch are mm. 
+
+\begindata
+ INS-130200_FOCAL_LENGTH      = 0.0272
+
+ INS-130200_PIXEL_PITCH       = 0.047472922
+ INS-130200_BORESIGHT_SAMPLE  = 0.0
+ INS-130200_BORESIGHT_LINE    = 0.0
+
+\begintext
+  The NIRS orientientiation in ISIS camera model implemenation is
+  +Y = +SAMPLE, +X = -LINE, Z = +Z
+ 
+  ITRANSS and ITRANSL were calculated using the camcoeffs application.
+
+\begindata
+
+ INS-130200_TRANSX  = (0.0, 0.0, -0.047472922)
+ INS-130200_TRANSY  = (0.0, 0.047472922, 0.0)
+ INS-130200_ITRANSS = (0.0, 0.0, 21.064639754005)
+ INS-130200_ITRANSL = (0.0, -21.064639754005, 0.0)
+
+\begintext
+NIRS is very close to Itokawa so light time correction 
+and target/observer perspective are set as follows.
+
+\begindata 
+
+INS-130200_SWAP_OBSERVER_TARGET = 'TRUE'
+INS-130200_LIGHTTIME_CORRECTION = 'NONE'
+INS-130200_LT_SURFACE_CORRECT = 'FALSE'
diff --git a/tests/pytests/data/2392975548_lvl3_0/pck00009.tpc b/tests/pytests/data/2392975548_lvl3_0/pck00009.tpc
new file mode 100755
index 0000000..bfadaab
--- /dev/null
+++ b/tests/pytests/data/2392975548_lvl3_0/pck00009.tpc
@@ -0,0 +1,3639 @@
+KPL/PCK
+ 
+
+P_constants (PcK) SPICE kernel file
+===========================================================================
+
+        By: Nat Bachman (NAIF)    2010 March 3
+ 
+ 
+Purpose
+--------------------------------------------------------
+
+     This file makes available for use in SPICE-based application
+     software orientation and size/shape data for natural bodies. The
+     principal source of the data is a published report by the IAU/IAG
+     Working Group on Cartographic Coordinates and Rotational Elements [1].
+
+     Orientation and size/shape data not provided by this file may be
+     available in mission-specific PCK files. Such PCKs may be the preferred
+     data source for mission-related applications. Mission-specific PCKs can
+     be found in PDS archives or on the NAIF web site at URL:
+
+        http://naif.jpl.nasa.gov
+
+
+File Organization
+--------------------------------------------------------
+ 
+     The contents of this file are as follows.
+ 
+     Introductory Information:
+
+         --   Purpose
+
+         --   File Organization
+ 
+         --   Version description
+ 
+         --   Disclaimer
+ 
+         --   Sources
+ 
+         --   Explanatory notes
+ 
+         --   Body numbers and names
+ 
+
+     PcK Data:
+ 
+
+        Orientation Data
+        ----------------
+
+         --   Orientation constants for the Sun and planets.        
+              Additional items included in this section:
+
+                 - Earth north geomagnetic centered dipole values
+                   for epochs 1945-2000
+
+                 - Mars prime meridian offset "lambda_a"
+
+         --   Orientation constants for satellites
+ 
+         --   Orientation constants for asteroids Eros, Gaspra, Ida,
+              Itokawa, and Vesta
+ 
+         --   Orientation constants for comets 19P/Borrelly
+              and 9P/Tempel 1
+
+
+        Radii of Bodies
+        ---------------
+
+         --   Radii of Sun and planets
+         
+         --   Radii of satellites, where available
+         
+         --   Radii of asteroids Ceres, Eros, Gaspra, Ida, Itokawa,
+              Mathilde, Toutatis, and Vesta.
+            
+         --   Radii of comets 19P/Borrelly, Halley, 9P/Tempel 1,
+              and 81P/Wild 2
+
+
+
+Version Description
+--------------------------------------------------------
+ 
+     This file was created on March 3, 2010. This version
+     incorporates data from reference [1].
+ 
+     This file contains size, shape, and orientation data for all
+     objects described by the previous version of the file, except
+     for Kleopatra: a shape model for this body is not provided in [1]
+     because, according to this source, it had been "modeled from
+     low resolution radar data, and cannot be mapped from those
+     data."
+
+     New objects covered by this file but not the previous
+     version are:
+        
+        19P/Borrelly
+        Halley
+        9P/Tempel 1
+        81P/Wild 2
+        Ceres
+        Itokawa
+        Mathilde
+        Toutatis
+                         
+ 
+Disclaimer
+--------------------------------------------------------
+ 
+Applicability of Data
+
+     This P_constants file may not contain the parameter values that
+     you prefer. NAIF suggests that you inspect this file visually
+     before proceeding with any critical or extended data processing.
+
+File Modifications by Users
+
+     Note that this file may be readily modified by you to change
+     values or add/delete parameters. NAIF requests that you update the
+     "by line," date, and version description section if you modify
+     this file.
+     
+Known Limitations and Caveats
+
+     Accuracy
+     --------
+
+     In general, the orientation models given here are claimed by the
+     IAU/IAG Working Group Report [1] to be accurate to 0.1 degree
+     ([1], p.158). However, NAIF notes that orientation models for
+     natural satellites and asteroids have in some cases changed
+     substantially with the availability of new observational data, so
+     users are urged to investigate the suitability for their
+     applications of the models presented here.
+
+     Earth orientation
+     -----------------
+
+     NAIF strongly cautions against using the earth rotation model
+     (from [1]) for work demanding high accuracy. This model has been
+     determined by NAIF to have an error in the prime meridian location
+     of magnitude at least 150 arcseconds, with a local minimum
+     occurring during the year 1999. Regarding availability of better
+     earth orientation data for use with the SPICE system:
+
+        Earth orientation data are available from NAIF in the form of
+        binary earth PCK files. NAIF employs an automated process to
+        create these files; each time JPL's Tracking Systems and
+        Applications Section produces a new earth orientation parameter
+        (EOP) file, a new PCK is produced. These PCKs cover a roughly
+        10 year time span starting at Jan. 1, 2000. In these PCK files,
+        the following effects are accounted for in modeling the earth's
+        rotation:
+
+           - Precession:                   1976 IAU model
+
+           - Nutation:                     1980 IAU model, plus interpolated
+                                           EOP nutation corrections
+
+           - Polar motion:                 interpolated from EOP file
+
+           - True sidereal time:
+
+                  UT1 - UT1R (if needed):  given by analytic formula
+                + TAI - UT1 (or UT1R):     interpolated from EOP file
+                + UT1 - GMST:              given by analytic formula
+                + equation of equinoxes:   given by analytic formula
+
+             where
+
+                TAI    =   International Atomic Time
+                UT1    =   Greenwich hour angle of computed mean sun - 12h
+                UT1R   =   Regularized UT1
+                GMST   =   Greenwich mean sidereal time                   
+
+        These kernels are available from the NAIF web site
+
+           http://naif.jpl.nasa.gov
+
+        (follow the links to Data, generic_kernels, and PCK data) or
+
+           ftp://naif.jpl.nasa.gov/pub/naif/generic_kernels/pck
+
+        or via anonymous ftp from the server
+ 
+           naif.jpl.nasa.gov
+
+        The kernels are in the path
+
+           pub/naif/generic_kernels/pck
+
+        At this time, these kernels have file names of the form
+
+           earth_000101_yymmdd_yymmdd.bpc
+
+        The second and third dates are, respectively, the file's 
+        coverage end time and the epoch of the last datum.
+ 
+        These binary PCK files are very accurate (error < 0.1
+        microradian) for epochs preceding the epoch of the last datum.
+        For later epochs, the error rises to several microradians.
+
+        Binary PCK files giving accurate earth orientation from 1972 to
+        2007 and *low accuracy* predicted earth orientation from
+        2007 to 2037 are also available in the same location. See the
+        aareadme.txt file at the "pck" URL above for details.
+
+        Characteristics and names of the binary kernels described here
+        are subject to change. See the "pck" URL above for information
+        on current binary earth PCKs.
+
+
+     Lunar orientation
+     -----------------
+
+     The lunar orientation formula provided by this file is a
+     trigonometric polynomial approximation yielding the orientation of
+     the lunar "Mean Earth/Polar Axis" (ME) reference frame. A more
+     accurate approximation can be obtained by using both the NAIF
+     lunar frame kernel and the binary lunar orientation PCK file,
+     which are available on the NAIF web site (see URLS above)
+     and in the NAIF server's ftp area. The lunar frame kernel
+     is located in the path
+
+        pub/naif/generic_kernels/fk/satellites
+
+     and has a name of the form
+
+        moon_yymmdd.tf
+
+     The binary lunar PCK is in the path
+
+        pub/naif/generic_kernels/pck
+
+     and has a name of the form
+
+        moon_pa_dennn_yyyy-yyyy.bpc
+
+     See the "aareadme.txt" files in the paths shown above for details
+     on file contents and versions. We also suggest you refer to the
+     SPICE tutorial named "lunar_earth_pck-fk," which is available from
+     the NAIF web site.
+
+
+     Earth geomagnetic dipole
+     ------------------------
+
+     The SPICE Toolkit doesn't currently contain software to model the
+     earth's north geomagnetic centered dipole as a function of time.
+     As a convenience for users, the north dipole location from the
+     J2000 epoch was selected as a representative datum, and the
+     planetocentric longitude and latitude of this location have been
+     associated with the keywords
+       
+        BODY399_N_GEOMAG_CTR_DIPOLE_LON
+        BODY399_N_GEOMAG_CTR_DIPOLE_LAT
+     
+     Values for the earth's north geomagnetic centered dipole are
+     presented in comments as a discrete time series for the time range
+     1945-2000. For details concerning the geomagnetic field model from
+     which these values were derived, including a discussion of the
+     model's accuracy, see [9].
+ 
+
+     Mars prime meridian offset
+     --------------------------
+
+     The Mars prime meridian offset given by [5] is not used by
+     SPICE geometry software for computations involving the shape
+     of Mars (for example, in sub-observer point or surface intercept
+     computations). The value is provided for informational
+     purposes only.
+
+
+     Software limitations
+     --------------------
+
+     SPICE Toolkits prior to version N0057 cannot make use of
+     trigonometric polynomial terms in the formulas for orientation of
+     the planets. The only planets for which such terms are used are
+     Jupiter and Neptune. Use of trigonometric polynomial terms for
+     natural satellites is and has been supported for all SPICE Toolkit
+     versions.
+ 
+     The second nutation precession angle (M2) for Mars is represented
+     by a quadratic polynomial in the 2006 IAU report. The SPICELIB
+     subroutine BODEUL can not handle this term (which is extremely
+     small), so we truncate the polynomial to a linear one. The 
+     resulting orientation error has a maximum magnitude of less
+     than 0.0032 degrees over the time span 1996-2015 and less than
+     0.0082 degrees over the time span 1986-2025.
+
+
+Sources
+--------------------------------------------------------
+ 
+     The sources for the constants listed in this file are:
+
+
+        [1]   Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F., 
+              Conrad, A., Consolmagno, G.J., Hestroffer, D.,
+              Hilton, J.L., Krasinsky, G.A., Neumann, G.,
+              Oberst, J., Stooke, P., Tedesco, E.F., Tholen, D.J., 
+              and Thomas, P.C. "Report of the IAU/IAG Working Group 
+              on cartographic coordinates and rotational elements: 2006."
+
+        [2]   Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F., 
+              Cruikshank, D.P., Hilton, J.L., Keller, H.U., Oberst, J.,
+              Simon, J.L., Stooke, P., Tholen, D.J., and Thomas, P.C.
+              "Report of the IAU/IAG Working Group on Cartographic
+              Coordinates and Rotational Elements of the Planets and
+              Satellites: 2003."
+ 
+        [3]   Nautical Almanac Office, United States Naval Observatory
+              and H.M. Nautical Almanac Office, Rutherford Appleton
+              Laboratory (2010). "The Astronomical Almanac for
+              the Year 2010," U.S. Government Printing Office,
+              Washington, D.C.: and The Stationary Office, London.
+
+        [4]   Nautical Almanac Office, United States Naval Observatory,
+              H.M. Nautical Almanac Office, Royal Greenwich
+              Observatory, Jet Propulsion Laboratory, Bureau des
+              Longitudes, and The Time Service and Astronomy
+              Departments, United States Naval Observatory (1992).
+              "Explanatory Supplement to the Astronomical Almanac," P.
+              Kenneth Seidelmann, ed. University Science Books, 20
+              Edgehill Road, Mill Valley, CA 9494.
+
+        [5]   Duxbury, Thomas C. (2001). "IAU/IAG 2000 Mars Cartographic
+              Conventions,"  presentation to the Mars Express Data
+              Archive Working Group, Dec. 14, 2001.
+
+        [6]   Russell, C.T. and Luhmann, J.G. (1990). "Earth: Magnetic 
+              Field and Magnetosphere." <http://www-ssc.igpp.ucla.
+              edu/personnel/russell/papers/earth_mag>. Originally
+              published in "Encyclopedia of Planetary Sciences," J.H.
+              Shirley and R.W. Fainbridge, eds. Chapman and Hall,
+              New York, pp 208-211.
+
+        [7]   Russell, C.T. (1971). "Geophysical Coordinate 
+              Transformations," Cosmic Electrodynamics 2  184-186.
+              NAIF document 181.0.
+     
+        [8]   ESA/ESTEC Space Environment Information System (SPENVIS)
+              (2003). Web page:  "Dipole approximations of the
+              geomagnetic field."  <http://www.spenvis.oma.be/spenvis/
+              help/background/magfield/cd.html>.
+ 
+        [9]   International Association of Geomagnetism and Aeronomy
+              and International Union of Geodesy and Geophysics (2004).
+              Web page:  "The 9th Generation International Geomagnetic
+              Reference Field." <http://www.ngdc.noaa.gov/
+              IAGA/vmod/igrf.html>.
+                             
+        [10]  Davies, M.E., Abalakin, V.K., Bursa, M., Hunt, G.E.,
+              and Lieske, J.H. (1989). "Report of the IAU/IAG/COSPAR
+              Working Group on Cartographic Coordinates and Rotational
+              Elements of the Planets and Satellites: 1988," Celestial
+              Mechanics and Dynamical Astronomy, v.46, no.2, pp.
+              187-204.
+
+         
+     Most values are from [1]. All exceptions are 
+     commented where they occur in this file. The exceptions are:
+ 
+                 
+         --   Radii for the Sun are from [3].
+             
+         --   The second nutation precession angle (M2) for Mars is
+              represented by a quadratic polynomial in the 2000
+              IAU report. The SPICELIB subroutine BODEUL can not
+              handle this term (which is extremely small), so we
+              truncate the polynomial to a linear one.
+           
+          --  Earth north geomagnetic centered dipole values are from
+              [8]. The article [6] was used to check most of 
+              these values, and the values were also re-computed from 
+              the 9th generation IGRF [9] by Nat Bachman.
+         
+          -- The Mars prime meridian offset angle is from [5].
+
+
+     "Old values" listed are from the SPICE P_constants file
+     pck00008.tpc dated September 21, 2004. Most of these values came
+     from the 2003 IAU report [2].
+ 
+ 
+ 
+ 
+Explanatory Notes
+--------------------------------------------------------
+
+     This file, which is logically part of the SPICE P-kernel, contains
+     constants used to model the orientation, size and shape of the
+     Sun, planets, natural satellites, and selected comets and
+     asteroids. The orientation models express the direction of the
+     pole and location of the prime meridian of a body as a function of
+     time. The size/shape models ("shape models" for short) represent
+     all bodies as ellipsoids, using two equatorial radii and a polar
+     radius. Spheroids and spheres are obtained when two or all three
+     radii are equal.
+
+     The SPICE Toolkit routines that use this file are documented in
+     the SPICE "Required Reading" file pck.req. They are also 
+     documented in the "PCK" SPICE tutorial, which is available on
+     the NAIF web site.
+
+File Format
+        
+     A terse description of the PCK file format is given here. See the
+     SPICE "Required Reading" files pck.req and kernel.req for a
+     detailed explanation of the SPICE text kernel file format. The
+     files pck.req and kernel.req are included in the documentation
+     provided with the SPICE Toolkit.
+
+     The file starts out with the ``ID word'' string
+
+        KPL/PCK
+
+     This string identifies the file as a text kernel containing PCK 
+     data.
+
+     This file consists of a series of comment blocks and data blocks.
+     Comment blocks, which contain free-form descriptive or explanatory
+     text, are preceded by a \begintext token. Data blocks follow a
+     \begindata token. In order to be recognized, each of these tokens
+     must be placed on a line by itself.
+
+     The portion of the file preceding the first data block is treated
+     as a comment block; it doesn't require an initial \begintext
+     token.
+
+     This file identifies data using a series of
+
+        KEYWORD = VALUE
+
+     assignments. The left hand side of each assignment is a
+     "kernel variable" name; the right hand side is an associated value
+     or list of values. The SPICE subroutine API allows SPICE routines
+     and user applications to retrieve the set of values associated
+     with each kernel variable name.
+
+     Kernel variable names are case-sensitive and are limited to
+     32 characters in length. 
+
+     Numeric values may be integer or floating point. String values
+     are normally limited to 80 characters in length; however, SPICE
+     provides a mechanism for identifying longer, "continued" strings.
+     See the SPICE routine STPOOL for details.
+
+     String values are single quoted.
+
+     When the right hand side of an assignment is a list of values,
+     the list items may be separated by commas or simply by blanks.
+     The list must be bracketed by parentheses. Example:
+
+        BODY399_RADII = ( 6378.14 6378.14 6356.75 )
+ 
+     Any blanks preceding or following keyword names, values and equal
+     signs are ignored.
+  
+     Assignments may be spread over multiple lines, for example:
+
+        BODY399_RADII = ( 6378.14 
+                          6378.14 
+                          6356.75 )
+
+     This file may contain blank lines anywhere. Non-printing
+     characters including TAB should not be present in the file: the
+     presence of such characters may cause formatting errors when the
+     file is viewed.
+
+Time systems and reference frames
+
+     The 2006 IAU/IAG Working Group Report [1] states the time scale
+     used as the independent variable for the rotation formulas is
+     Barycentric Dynamical Time (TDB) and that the epoch of variable
+     quantities is J2000 TDB (2000 Jan 1 12:00 TDB). Throughout SPICE
+     documentation and in this file, we use the names "J2000 TDB" and
+     "J2000" for this epoch. The name "J2000.0" is equivalent.
+
+     SPICE documentation refers to the time system used in this file 
+     as either "ET" or "TDB." SPICE software makes no distinction 
+     between TDB and the time system associated with the independent
+     variable of the JPL planetary ephemerides T_eph.
+ 
+     The inertial reference frame used for the rotational elements in
+     this file is identified by [1] as the ICRF (International
+     Celestial Reference Frame). 
+
+     The SPICE PCK software that reads this file uses the label "J2000"
+     to refer to the ICRF; this is actually a mislabeling which has
+     been retained in the interest of backward compatibility. Using
+     data from this file, by means of calls to the SPICE frame
+     transformation routines, will actually compute orientation
+     relative to the ICRF.
+
+     The difference between the J2000 frame and the ICRF is
+     on the order of tens of milliarcseconds and is well below the
+     accuracy level of the formulas in this file.
+
+Orientation models
+ 
+     All of the orientation models use three Euler angles to describe
+     the orientation of the coordinate axes of the "Body Equator and
+     Prime Meridian" system with respect to an inertial system. By
+     default, the inertial system is the ICRF (labeled as "J2000"), but
+     other frames can be specified in the file. See the PCK Required
+     Reading for details.
+ 
+     The first two angles, in order, are the ICRF right ascension and
+     declination (henceforth RA and DEC) of the north pole of a body as
+     a function of time. The third angle is the prime meridian location
+     (represented by "W"), which is expressed as a rotation about the
+     north pole, and is also a function of time.
+ 
+     For each body, the expressions for the north pole's right
+     ascension and declination, as well as prime meridian location, are
+     sums (as far as the models that appear in this file are concerned)
+     of quadratic polynomials and trigonometric polynomials, where the
+     independent variable is time.
+ 
+     In this file, the time arguments in expressions always refer to
+     Barycentric Dynamical Time (TDB), measured in centuries or days
+     past a reference epoch. By default, the reference epoch is the
+     J2000 epoch, which is Julian ephemeris date 2451545.0, but other
+     epochs can be specified in the file. See the PCK Required Reading
+     for details.
+
+     Orientation models for satellites and some planets (including
+     Jupiter) involve both polynomial terms and trigonometric terms.
+     The arguments of the trigonometric terms are linear polynomials.
+     In this file, we call the arguments of these trigonometric terms
+     "nutation precession angles."
+
+     Example: 2006 IAU Model for orientation of Jupiter.  Note that 
+     these values are used as an example only; see the data area below 
+     for current values.
+
+        Right ascension
+        ---------------
+ 
+        alpha   =  268.056595 - 0.006499 T        +  0.000117 sin(Ja) 
+             0                + 0.000938 sin(Jb)  +  0.001432 sin(Jc)
+                              + 0.000030 sin(Jd)  +  0.002150 sin(Je)
+
+        Declination
+        -----------
+ 
+        delta   =   64.495303 + 0.002413 T        +  0.000050 cos(Ja)
+             0                + 0.000404 cos(Jb)  +  0.000617 cos(Jc)
+                              - 0.000013 cos(Jd)  +  0.000926 cos(Je)
+
+        Prime meridian
+        --------------
+
+        W       =  284.95  + 870.5366420 d
+ 
+
+     Here
+
+        T represents centuries past J2000 ( TDB ),
+ 
+        d represents days past J2000 ( TDB ).
+
+        Ja-Je are nutation precession angles.
+
+     In this file, the polynomials' coefficients above are assigned 
+     to kernel variable names (left-hand-side symbols) as follows
+
+        BODY599_POLE_RA        = (   268.056595     -0.006499       0. )
+        BODY599_POLE_DEC       = (    64.495303      0.002413       0. )
+        BODY599_PM             = (   284.95        870.5366420      0. )
+
+     and the trigonometric polynomials' coefficients are assigned 
+     as follows
+
+        BODY599_NUT_PREC_RA  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000117
+                                                                0.000938
+                                                                0.001432
+                                                                0.000030
+                                                                0.002150 )
+
+        BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000050
+                                                                0.000404
+                                                                0.000617
+                                                               -0.000013
+                                                                0.000926 )
+
+        BODY599_NUT_PREC_PM  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.0
+                                                                0.0
+                                                                0.0
+                                                                0.0
+                                                                0.0  ) 
+
+     Note the number "599"; this is the NAIF ID code for Jupiter.
+
+     In this file, the polynomial expressions for the nutation
+     precession angles are listed along with the planet's RA, DEC, and
+     prime meridian terms. Below are the 2006 IAU nutation precession
+     angles for the Jupiter system.
+
+        J1  =   73.32      +  91472.9 T
+        J2  =   24.62      +  45137.2 T
+        J3  =  283.90      +   4850.7 T
+        J4  =  355.80      +   1191.3 T
+        J5  =  119.90      +    262.1 T
+        J6  =  229.80      +     64.3 T
+        J7  =  352.25      +   2382.6 T
+        J8  =  113.35      +   6070.0 T
+
+        J9  =  146.64      + 182945.8 T
+        J10 =   49.24      +  90274.4 T 
+
+        Ja  =   99.360714  +   4850.4046 T
+        Jb  =  175.895369  +   1191.9605 T
+        Jc  =  300.323162  +    262.5475 T
+        Jd  =  114.012305  +   6070.2476 T
+        Je  =   49.511251  +     64.3000 T
+
+     Here
+
+        T represents centuries past J2000 ( TDB )
+
+        J1-J10 and Ja-Je are the nutation precession angles. The angles
+        J9 and J10 are equal to 2*J1 and 2*J2, respectively.
+ 
+        Angles J9 and J10 are not present in [1]; they have been added
+        to fit the terms 2*J1 and 2*J2, which appear in the orientation
+        models of several satellites, into a form that can be accepted
+        by the PCK system.
+
+     The assignment of the nutation precession angles for the
+     Jupiter system is as follows:
+ 
+        BODY5_NUT_PREC_ANGLES  = (    73.32      91472.9
+                                      24.62      45137.2
+                                     283.90       4850.7
+                                     355.80       1191.3
+                                     119.90        262.1
+                                     229.80         64.3
+                                     352.25       2382.6
+                                     113.35       6070.0   
+                                     146.64     182945.8
+                                      49.24      90274.4  
+                                      99.360714   4850.4046
+                                     175.895369   1191.9605
+                                     300.323162    262.5475
+                                     114.012305   6070.2476
+                                      49.511251     64.3000  )
+
+     You'll see an additional symbol grouped with the ones listed
+     above; it is
+ 
+        BODY599_LONG_AXIS
+ 
+     This term is zero for all bodies except Mars. It represents the
+     angular offset between the meridian containing the longest axis of
+     the triaxial ellipsoid used to model a body's surface and the
+     prime meridian of the body.
+
+     The pattern of the formulas for satellite orientation is similar
+     to that for Jupiter. Example: 2006 IAU values for Io. Again, these
+     values are used as an example only; see the data area below for
+     current values.
+ 
+        Right ascension
+        ---------------
+
+        alpha  = 268.05  -  0.009 T  + 0.094 sin(J3)  +  0.024 sin(J4)
+             0  
+
+        Declination
+        -----------
+
+        delta  =  64.50  +  0.003 T  + 0.040 cos(J3)  +  0.011 cos(J4)
+             0           
+                          
+        Prime meridian
+        --------------
+
+        W      = 200.39  +  203.4889538 d  -  0.085 sin(J3)  -  0.022 sin(J4)
+
+ 
+        d represents days past J2000.
+ 
+        J3 and J4 are nutation precession angles.
+ 
+     The polynomial terms are assigned to symbols by the statements
+ 
+        BODY501_POLE_RA       = (  268.05          -0.009      0. )
+        BODY501_POLE_DEC      = (   64.50           0.003      0. )
+        BODY501_PM            = (  200.39         203.4889538  0. )
+ 
+     The coefficients of the trigonometric terms are assigned to symbols by
+     the statements
+
+        BODY501_NUT_PREC_RA   = (    0.   0.     0.094    0.024   )
+        BODY501_NUT_PREC_DEC  = (    0.   0.     0.040    0.011   )
+        BODY501_NUT_PREC_PM   = (    0.   0.    -0.085   -0.022   )
+
+     501 is the NAIF ID code for Io.
+ 
+     SPICE software expects the models for satellite orientation to
+     follow the form of the model shown here: the polynomial portions of the
+     RA, DEC, and W expressions are expected to be quadratic, the 
+     trigonometric terms for RA and W (satellite prime meridian) are expected 
+     to be linear combinations of sines of nutation precession angles, the 
+     trigonometric terms for DEC are expected to be linear combinations of 
+     cosines of nutation precession angles, and the polynomials for the 
+     nutation precession angles themselves are expected to be linear.
+ 
+     Eventually, the software will handle more complex expressions, we
+     expect.
+ 
+ 
+Shape models
+ 
+     There is only one kind of shape model supported by the SPICE Toolkit
+     software at present: the triaxial ellipsoid. The 2006 IAU report does
+     not use any other models, except in the case of Mars, where 
+     separate values are given for the north and south polar radii.
+ 
+     For each body, three radii are listed:  The first number is
+     the largest equatorial radius (the length of the semi-axis
+     containing the prime meridian), the second number is the smaller
+     equatorial radius, and the third is the polar radius.
+ 
+     Example: Radii of the Earth.
+ 
+        BODY399_RADII     = (     6378.14    6378.14      6356.75   )
+ 
+ 
+Body Numbers and Names
+--------------------------------------------------------
+ 
+ 
+        1  Mercury barycenter
+        2  Venus barycenter
+        3  Earth barycenter
+        4  Mars barycenter
+        5  Jupiter barycenter
+        6  Saturn barycenter
+        7  Uranus barycenter
+        8  Neptune barycenter
+        9  Pluto barycenter
+        10 Sun
+
+ 
+        199 Mercury
+ 
+ 
+        299 Venus
+ 
+ 
+        399 Earth
+ 
+        301 Moon
+ 
+ 
+        499 Mars
+ 
+        401 Phobos      402 Deimos
+ 
+ 
+        599 Jupiter
+ 
+        501 Io          502 Europa      503 Ganymede    504 Callisto
+        505 Amalthea    506 Himalia     507 Elara       508 Pasiphae
+        509 Sinope      510 Lysithea    511 Carme       512 Ananke
+        513 Leda        514 Thebe       515 Adrastea    516 Metis
+ 
+ 
+        699 Saturn
+ 
+        601 Mimas       602 Enceladus   603 Tethys      604 Dione
+        605 Rhea        606 Titan       607 Hyperion    608 Iapetus
+        609 Phoebe      610 Janus       611 Epimetheus  612 Helene
+        613 Telesto     614 Calypso     615 Atlas       616 Prometheus
+        617 Pandora     618 Pan
+ 
+ 
+        799 Uranus
+ 
+        701 Ariel       702 Umbriel     703 Titania     704 Oberon
+        705 Miranda     706 Cordelia    707 Ophelia     708 Bianca
+        709 Cressida    710 Desdemona   711 Juliet      712 Portia
+        713 Rosalind    714 Belinda     715 Puck
+ 
+ 
+        899 Neptune
+ 
+        801 Triton      802 Nereid      803 Naiad       804 Thalassa
+        805 Despina     806 Galatea     807 Larissa     808 Proteus
+ 
+ 
+        999 Pluto
+ 
+        901 Charon
+ 
+ 
+        1000005 Comet 19P/Borrelly
+        1000036 Comet Halley
+        1000093 Comet 9P/Tempel 1
+        1000107 Comet 81P/Wild 2
+
+        2000001 Asteroid Ceres
+        2000004 Asteroid Vesta
+        2000216 Asteroid Kleopatra
+        2000253 Asteroid Mathilde
+        2000433 Asteroid Eros
+        2004179 Asteroid Toutatis
+        2025143 Asteroid Itokawa
+        2431010 Asteroid Ida
+        9511010 Asteroid Gaspra
+        
+ 
+Orientation Constants for the Sun and Planets
+--------------------------------------------------------
+ 
+ 
+Sun
+ 
+     Old values:
+
+        Values are from the 2003 IAU report.
+
+  
+        body10_pole_ra         = (  286.13       0.          0. )
+        body10_pole_dec        = (   63.87       0.          0. )
+        body10_pm              = (   84.10      14.18440     0. )
+        body10_long_axis       = (    0.                        )
+
+     Current values:
+ 
+        \begindata
+ 
+        BODY10_POLE_RA         = (  286.13       0.          0. )
+        BODY10_POLE_DEC        = (   63.87       0.          0. )
+        BODY10_PM              = (   84.176     14.18440     0. )
+        BODY10_LONG_AXIS       = (    0.                        )
+
+        \begintext
+ 
+Mercury
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+
+
+     Current values:
+  
+        \begindata
+
+        BODY199_POLE_RA          = (  281.01     -0.033      0. )
+        BODY199_POLE_DEC         = (   61.45     -0.005      0. )
+        BODY199_PM               = (  329.548     6.1385025  0. )
+ 
+        BODY199_LONG_AXIS        = (    0.                        )
+ 
+        \begintext
+ 
+  
+Venus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY299_POLE_RA          = (  272.76       0.          0. )
+        BODY299_POLE_DEC         = (   67.16       0.          0. )
+        BODY299_PM               = (  160.20      -1.4813688   0. )
+ 
+        BODY299_LONG_AXIS        = (    0.                        )
+ 
+        \begintext
+
+
+Earth
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 report.
+ 
+ 
+     Current values:
+ 
+        \begindata 
+ 
+        BODY399_POLE_RA        = (    0.      -0.641         0. )
+        BODY399_POLE_DEC       = (   90.      -0.557         0. )
+        BODY399_PM             = (  190.147  360.9856235     0. )
+        BODY399_LONG_AXIS      = (    0.                        )
+
+        \begintext
+
+
+        Nutation precession angles for the Earth-Moon system:
+
+           The linear coefficients have been scaled up from degrees/day
+           to degrees/century, because the SPICELIB PCK reader expects
+           these units.  The original constants were:
+        
+                                    125.045D0   -0.0529921D0
+                                    250.089D0   -0.1059842D0
+                                    260.008D0   13.0120009D0
+                                    176.625D0   13.3407154D0
+                                    357.529D0    0.9856003D0
+                                    311.589D0   26.4057084D0
+                                    134.963D0   13.0649930D0
+                                    276.617D0    0.3287146D0
+                                     34.226D0    1.7484877D0
+                                     15.134D0   -0.1589763D0
+                                    119.743D0    0.0036096D0
+                                    239.961D0    0.1643573D0
+                                     25.053D0   12.9590088D0 
+
+
+        \begindata
+
+       
+        BODY3_NUT_PREC_ANGLES  = (  125.045         -1935.5364525000
+                                    250.089         -3871.0729050000
+                                    260.008        475263.3328725000  
+                                    176.625        487269.6299850000
+                                    357.529         35999.0509575000
+                                    311.589        964468.4993100000
+                                    134.963        477198.8693250000
+                                    276.617         12006.3007650000
+                                     34.226         63863.5132425000 
+                                     15.134         -5806.6093575000
+                                    119.743           131.8406400000
+                                    239.961          6003.1503825000 
+                                     25.053        473327.7964200000 )
+
+
+        \begintext
+ 
+
+     Earth north geomagnetic centered dipole:
+
+        Old values:
+
+           Values are from [7].  Note the year of publication was 1971.
+
+           body399_mag_north_pole_lon  =  ( -69.761 )
+           body399_mag_north_pole_lat  =  (  78.565 )
+
+
+        Current values:
+
+           The north dipole location is time-varying.  The values shown
+           below, taken from [8], represent a discrete sampling of the
+           north dipole location from 1945 to 2000. The terms DGRF and
+           IGRF refer to, respectively, "Definitive Geomagnetic
+           Reference Field" and "International Geomagnetic Reference
+           Field."  See references [6], [8], and [9] for details.
+
+           Coordinates are planetocentric. 
+
+             Data source    Lat      Lon
+             -----------   -----    ------
+              DGRF 1945    78.47    291.47
+              DGRF 1950    78.47    291.15
+              DGRF 1955    78.46    290.84
+              DGRF 1960    78.51    290.53
+              DGRF 1965    78.53    290.15
+              DGRF 1970    78.59    289.82
+              DGRF 1975    78.69    289.53
+              DGRF 1980    78.81    289.24 
+              DGRF 1985    78.97    289.10
+              DGRF 1990    79.13    288.89
+              IGRF 1995    79.30    288.59
+              IGRF 2000    79.54    288.43      
+
+
+        Values are given for the epoch 2000 and are from the final row
+        of the above table, which is from [8]. As shown by the table
+        these values constitute a low-accuracy approximation for epochs
+        not close to 2000.
+
+        \begindata
+       
+        BODY399_N_GEOMAG_CTR_DIPOLE_LON  =  ( 288.43 )
+        BODY399_N_GEOMAG_CTR_DIPOLE_LAT  =  (  79.54 )
+
+        \begintext
+
+ 
+Mars
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+   
+     Current values:
+ 
+        \begindata
+ 
+        BODY499_POLE_RA          = (  317.68143   -0.1061      0.  )
+        BODY499_POLE_DEC         = (   52.88650   -0.0609      0.  )
+        BODY499_PM               = (  176.630    350.89198226  0.  )
+
+        \begintext
+ 
+        Source [5] specifies the following value for the lambda_a term
+        (BODY499_LONG_AXIS ) for Mars. This term is the POSITIVE EAST
+        LONGITUDE, measured from the prime meridian, of the meridian
+        containing the longest axis of the reference ellipsoid.
+        (CAUTION: previous values were POSITIVE WEST.)
+
+           body499_long_axis        = (  252.  )
+ 
+        We list this lambda_a value for completeness. The IAU report
+        [1] gives equal values for both equatorial radii, so the
+        lambda_a offset does not apply to the IAU model.
+ 
+        The 2003 IAU report defines M2, the second nutation precession angle,
+        by:
+ 
+                                                2
+           192.93  +  1128.4096700 d  +  8.864 T
+ 
+        We truncate the M2 series to a linear expression, because the PCK
+        software cannot handle the quadratic term.
+ 
+        Again, the linear terms are scaled by 36525.0:
+ 
+            -0.4357640000000000       -->     -15916.28010000000
+          1128.409670000000           -->   41215163.19675000
+            -1.8151000000000000E-02   -->       -662.9652750000000
+ 
+        We also introduce a fourth nutation precession angle, which
+        is the pi/2-complement of the third angle.  This angle is used
+        in computing the prime meridian location for Deimos.  See the
+        discussion of this angle below in the section containing orientation
+        constants for Deimos.
+ 
+        \begindata
+
+        BODY4_NUT_PREC_ANGLES  = (  169.51     -15916.2801
+                                    192.93   41215163.19675
+                                     53.47       -662.965275
+                                     36.53        662.965275  )
+ 
+        \begintext
+ 
+ 
+Jupiter
+ 
+     Old values:
+ 
+        Values are from the 2003 IAU report.
+
+
+           body599_pole_ra        = (   268.05      -0.009       0. )
+           body599_pole_dec       = (    64.49       0.003       0. )
+           body599_pm             = (   284.95     870.5366420   0. )
+           body599_long_axis      = (     0.                        )
+
+           body5_nut_prec_angles  = (    73.32   91472.9
+                                         24.62   45137.2
+                                        283.90    4850.7
+                                        355.80    1191.3
+                                        119.90     262.1
+                                        229.80      64.3
+                                        352.35    2382.6
+                                        113.35    6070.0   
+                                        146.64  182945.8
+                                         49.24   90274.4  )
+ 
+
+                   
+     Current values:
+ 
+        The number of nutation precession angles is 15. The ninth and
+        tenth are twice the first and second, respectively. The
+        eleventh through fifteenth correspond to angles JA-JE in
+        the 2006 IAU report; angles JA-JE were not used prior to that
+        report.
+
+        \begindata
+ 
+ 
+        BODY599_POLE_RA        = (   268.056595     -0.006499       0. )
+        BODY599_POLE_DEC       = (    64.495303      0.002413       0. )
+        BODY599_PM             = (   284.95        870.5366420      0. )
+        BODY599_LONG_AXIS      = (     0.                        )
+ 
+        BODY599_NUT_PREC_RA  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000117
+                                                                0.000938
+                                                                0.001432
+                                                                0.000030
+                                                                0.002150 )
+
+        BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000050
+                                                                0.000404
+                                                                0.000617
+                                                               -0.000013
+                                                                0.000926 )
+
+        BODY599_NUT_PREC_PM  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.0
+                                                                0.0
+                                                                0.0
+                                                                0.0
+                                                                0.0  ) 
+
+
+        BODY5_NUT_PREC_ANGLES  = (    73.32      91472.9
+                                      24.62      45137.2
+                                     283.90       4850.7
+                                     355.80       1191.3
+                                     119.90        262.1
+                                     229.80         64.3
+                                     352.25       2382.6
+                                     113.35       6070.0   
+                                     146.64     182945.8
+                                      49.24      90274.4  
+                                      99.360714   4850.4046
+                                     175.895369   1191.9605
+                                     300.323162    262.5475
+                                     114.012305   6070.2476
+                                      49.511251     64.3000  )
+        \begintext
+ 
+ 
+Saturn
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+
+     Current values:
+ 
+        \begindata
+
+        BODY699_POLE_RA        = (    40.589    -0.036      0.  )
+        BODY699_POLE_DEC       = (    83.537    -0.004      0.  )
+        BODY699_PM             = (    38.90    810.7939024  0.  )
+        BODY699_LONG_AXIS      = (     0.                       )
+ 
+        \begintext
+ 
+        The first seven angles given here are the angles S1 
+        through S7 from the 2000 report; the eighth and
+        ninth angles are 2*S1 and 2*S2, respectively.
+ 
+ 
+        \begindata
+
+        BODY6_NUT_PREC_ANGLES  = (  353.32   75706.7
+                                     28.72   75706.7  
+                                    177.40  -36505.5 
+                                    300.00   -7225.9 
+                                    316.45     506.2
+                                    345.20   -1016.3  
+                                     29.80     -52.1
+                                    706.64  151413.4
+                                     57.44  151413.4  )
+        \begintext
+ 
+ 
+Uranus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY799_POLE_RA        = (  257.311     0.         0.  )
+        BODY799_POLE_DEC       = (  -15.175     0.         0.  )
+        BODY799_PM             = (  203.81   -501.1600928  0.  )
+        BODY799_LONG_AXIS      = (    0.                       )
+ 
+        \begintext
+        
+        The first 16 angles given here are the angles U1 
+        through U16 from the 2000 report; the 17th and
+        18th angles are 2*U11 and 2*U12, respectively.
+        
+        \begindata
+         
+        BODY7_NUT_PREC_ANGLES  = (  115.75   54991.87
+                                    141.69   41887.66
+                                    135.03   29927.35
+                                     61.77   25733.59  
+                                    249.32   24471.46
+                                     43.86   22278.41 
+                                     77.66   20289.42  
+                                    157.36   16652.76  
+                                    101.81   12872.63   
+                                    138.64    8061.81
+                                    102.23   -2024.22 
+                                    316.41    2863.96  
+                                    304.01     -51.94  
+                                    308.71     -93.17 
+                                    340.82     -75.32 
+                                    259.14    -504.81 
+                                    204.46   -4048.44
+                                    632.82    5727.92     )
+                                    
+        \begintext
+ 
+ 
+ 
+Neptune
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+ 
+     Current values:
+
+        \begindata        
+ 
+           BODY899_POLE_RA        = (  299.36     0.         0. )
+           BODY899_POLE_DEC       = (   43.46     0.         0. )
+           BODY899_PM             = (  253.18   536.3128492  0. )
+           BODY899_LONG_AXIS      = (    0.                     )
+
+
+           BODY899_NUT_PREC_RA    = (  0.70 0. 0. 0. 0. 0. 0. 0. ) 
+           BODY899_NUT_PREC_DEC   = ( -0.51 0. 0. 0. 0. 0. 0. 0. )
+           BODY899_NUT_PREC_PM    = ( -0.48 0. 0. 0. 0. 0. 0. 0. )
+
+        \begintext
+ 
+           The 2000 report defines the nutation precession angles
+ 
+              N, N1, N2, ... , N7
+ 
+           and also uses the multiples of N1 and N7
+ 
+              2*N1
+ 
+           and
+ 
+              2*N7, 3*N7, ..., 9*N7
+ 
+           In this file, we treat the angles and their multiples as
+           separate angles.  In the kernel variable
+ 
+              BODY8_NUT_PREC_ANGLES
+ 
+           the order of the angles is
+ 
+              N, N1, N2, ... , N7, 2*N1, 2*N7, 3*N7, ..., 9*N7
+ 
+           Each angle is defined by a linear polynomial, so two
+           consecutive array elements are allocated for each
+           angle.  The first term of each pair is the constant term,
+           the second is the linear term.
+ 
+        \begindata 
+
+              BODY8_NUT_PREC_ANGLES = (   357.85         52.316
+                                          323.92      62606.6
+                                          220.51      55064.2 
+                                          354.27      46564.5
+                                           75.31      26109.4 
+                                           35.36      14325.4
+                                          142.61       2824.6  
+                                          177.85         52.316 
+                                          647.840    125213.200
+                                          355.700       104.632
+                                          533.550       156.948
+                                          711.400       209.264
+                                          889.250       261.580
+                                         1067.100       313.896
+                                         1244.950       366.212
+                                         1422.800       418.528
+                                         1600.650       470.844   )
+                                         
+        \begintext
+ 
+ 
+ 
+Pluto
+ 
+     Old values:
+ 
+        Values are from the 2003 IAU report. 
+ 
+        BODY999_POLE_RA        = (  313.02    0.         0.   )
+        BODY999_POLE_DEC       = (    9.09    0.         0.   )
+        BODY999_PM             = (  236.77  -56.3623195  0.   )
+        BODY999_LONG_AXIS      = (    0.                      )
+
+
+     Current values:
+ 
+        \begindata
+ 
+        BODY999_POLE_RA        = (  312.993   0.          0. )
+        BODY999_POLE_DEC       = (    6.163   0.          0. )
+        BODY999_PM             = (  237.305  -56.3625225  0. )
+        BODY999_LONG_AXIS      = (    0.                     )
+
+        \begintext
+ 
+ 
+ 
+ 
+Orientation constants for the satellites
+--------------------------------------------------------
+ 
+ 
+Satellites of Earth
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+
+ 
+     New values:
+ 
+        \begindata
+ 
+ 
+
+
+
+        BODY301_POLE_RA      = (  269.9949        0.0031        0.      )
+        BODY301_POLE_DEC     = (   66.5392        0.0130        0.      )
+        BODY301_PM           = (   38.3213       13.17635815   -1.4D-12 )
+        BODY301_LONG_AXIS    = (    0.                                  )
+   
+        BODY301_NUT_PREC_RA  = (   -3.8787   -0.1204   0.0700   -0.0172
+                                    0.0       0.0072   0.0       0.0
+                                    0.0      -0.0052   0.0       0.0
+                                    0.0043                              )
+        
+        BODY301_NUT_PREC_DEC = (   1.5419     0.0239  -0.0278    0.0068
+                                   0.0       -0.0029   0.0009    0.0
+                                   0.0        0.0008   0.0       0.0     
+                                  -0.0009                               )
+        
+        BODY301_NUT_PREC_PM  = (   3.5610     0.1208  -0.0642    0.0158
+                                   0.0252    -0.0066  -0.0047   -0.0046
+                                   0.0028     0.0052   0.0040    0.0019
+                                  -0.0044                               )
+        \begintext
+ 
+
+ 
+Satellites of Mars
+ 
+ 
+     Phobos
+ 
+          Old values:
+ 
+             Values are unchanged in the 2006 IAU report.
+ 
+          Current values:
+ 
+            The quadratic prime meridian term is scaled by 1/36525**2:
+ 
+               8.864000000000000   --->   6.6443009930565219E-09
+ 
+        \begindata
+ 
+          BODY401_POLE_RA  = ( 317.68    -0.108     0.                     )
+          BODY401_POLE_DEC = (  52.90    -0.061     0.                     )
+          BODY401_PM       = (  35.06  1128.8445850 6.6443009930565219E-09 )
+                                       
+          BODY401_LONG_AXIS     = (    0.   )
+ 
+          BODY401_NUT_PREC_RA   = (   1.79    0.    0.   0. )
+          BODY401_NUT_PREC_DEC  = (  -1.08    0.    0.   0. )
+          BODY401_NUT_PREC_PM   = (  -1.42   -0.78  0.   0. )
+
+
+        \begintext
+ 
+ 
+     Deimos
+ 
+        Old values:
+ 
+           Values are unchanged in the 2006 IAU report.
+ 
+ 
+        New values:
+ 
+           The Deimos prime meridian expression is:
+ 
+ 
+                                                     2
+              W = 79.41  +  285.1618970 d  -  0.520 T  -  2.58 sin M
+                                                                    3
+ 
+                                                       +  0.19 cos M .
+                                                                    3
+ 
+ 
+           At the present time, the PCK kernel software (the routine
+           BODEUL in particular) cannot handle the cosine term directly,
+           but we can represent it as
+ 
+              0.19 sin M
+                        4
+ 
+           where
+ 
+              M   =  90.D0 - M
+               4              3
+ 
+           Therefore, the nutation precession angle assignments for Phobos
+           and Deimos contain four coefficients rather than three.
+ 
+           The quadratic prime meridian term is scaled by 1/36525**2:
+ 
+              -0.5200000000000000  --->   -3.8978300049519307E-10
+ 
+        \begindata
+ 
+           BODY402_POLE_RA       = (  316.65     -0.108       0.           )
+           BODY402_POLE_DEC      = (   53.52     -0.061       0.           )
+           BODY402_PM            = (   79.41    285.1618970  -3.897830D-10 )
+           BODY402_LONG_AXIS     = (    0.                                 )
+ 
+           BODY402_NUT_PREC_RA   = (    0.   0.   2.98    0.   )
+           BODY402_NUT_PREC_DEC  = (    0.   0.  -1.78    0.   )
+           BODY402_NUT_PREC_PM   = (    0.   0.  -2.58    0.19 )
+
+        \begintext
+ 
+ 
+ 
+ 
+Satellites of Jupiter
+ 
+ 
+     Io
+ 
+          Old values:
+ 
+             Values are unchanged in the 2006 IAU report.
+ 
+          Current values:
+         
+        \begindata
+ 
+        BODY501_POLE_RA       = (  268.05          -0.009      0. )
+        BODY501_POLE_DEC      = (   64.50           0.003      0. )
+        BODY501_PM            = (  200.39         203.4889538  0. )
+        BODY501_LONG_AXIS     = (    0.                           )
+ 
+        BODY501_NUT_PREC_RA   = (    0.   0.     0.094    0.024   )
+        BODY501_NUT_PREC_DEC  = (    0.   0.     0.040    0.011   )
+        BODY501_NUT_PREC_PM   = (    0.   0.    -0.085   -0.022   )
+
+        \begintext
+ 
+ 
+ 
+     Europa
+ 
+ 
+        Old values:
+
+           Values are from the 2003 IAU report.
+
+
+        body502_pole_ra       = (  268.08          -0.009      0.   )
+        body502_pole_dec      = (   64.51           0.003      0.   )
+        body502_pm            = (   35.67         101.3747235  0.   )
+        body502_long_axis     = (    0.                             )
+ 
+        body502_nut_prec_ra   = ( 0. 0. 0.   1.086   0.060   0.015   0.009 )
+        body502_nut_prec_dec  = ( 0. 0. 0.   0.468   0.026   0.007   0.002 )
+        body502_nut_prec_pm   = ( 0. 0. 0.  -0.980  -0.054  -0.014  -0.008 )
+        
+
+        Current values:
+ 
+        \begindata 
+ 
+        BODY502_POLE_RA       = (  268.08          -0.009      0.   )
+        BODY502_POLE_DEC      = (   64.51           0.003      0.   )
+        BODY502_PM            = (   36.022        101.3747235  0.   )
+        BODY502_LONG_AXIS     = (    0.                             )
+ 
+        BODY502_NUT_PREC_RA   = ( 0. 0. 0.   1.086   0.060   0.015   0.009 )
+        BODY502_NUT_PREC_DEC  = ( 0. 0. 0.   0.468   0.026   0.007   0.002 )
+        BODY502_NUT_PREC_PM   = ( 0. 0. 0.  -0.980  -0.054  -0.014  -0.008 )
+ 
+        \begintext
+ 
+ 
+     Ganymede
+ 
+        Old values:
+ 
+             Values are unchanged in the 2006 IAU report.
+ 
+
+        Current values:
+        
+        \begindata
+    
+        BODY503_POLE_RA       = (  268.20         -0.009       0.  )
+        BODY503_POLE_DEC      = (   64.57          0.003       0.  )
+        BODY503_PM            = (   44.064        50.3176081   0.  )
+        BODY503_LONG_AXIS     = (    0.                            )
+
+        BODY503_NUT_PREC_RA   = ( 0. 0. 0.  -0.037   0.431   0.091   )
+        BODY503_NUT_PREC_DEC  = ( 0. 0. 0.  -0.016   0.186   0.039   )
+        BODY503_NUT_PREC_PM   = ( 0. 0. 0.   0.033  -0.389  -0.082   )
+ 
+        \begintext
+ 
+ 
+     Callisto
+ 
+        Old values:
+
+             Values are unchanged in the 2006 IAU report.
+        
+        
+        Current values:
+        
+        
+        \begindata
+  
+        BODY504_POLE_RA       = (   268.72    -0.009       0.  )
+        BODY504_POLE_DEC      = (    64.83     0.003       0.  )
+        BODY504_PM            = (   259.51    21.5710715   0.  )
+        BODY504_LONG_AXIS     = (     0.                       )
+ 
+        BODY504_NUT_PREC_RA   = ( 0. 0. 0. 0.  -0.068   0.590  0.   0.010 )
+        BODY504_NUT_PREC_DEC  = ( 0. 0. 0. 0.  -0.029   0.254  0.  -0.004 )
+        BODY504_NUT_PREC_PM   = ( 0. 0. 0. 0.   0.061  -0.533  0.  -0.009 )
+ 
+        \begintext
+ 
+ 
+     Amalthea
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report.        
+        
+        Current values:
+         
+        \begindata
+ 
+        BODY505_POLE_RA       = (   268.05    -0.009      0.  )
+        BODY505_POLE_DEC      = (    64.49     0.003      0.  )
+        BODY505_PM            = (   231.67   722.6314560  0.  )
+        BODY505_LONG_AXIS     = (     0.                      )
+ 
+        BODY505_NUT_PREC_RA  = ( -0.84  0. 0. 0. 0. 0. 0. 0.   0.01  0. )
+        BODY505_NUT_PREC_DEC = ( -0.36  0. 0. 0. 0. 0. 0. 0.   0.    0. )
+        BODY505_NUT_PREC_PM  = (  0.76  0. 0. 0. 0. 0. 0. 0.  -0.01  0. )
+ 
+        \begintext
+ 
+ 
+     Thebe
+ 
+ 
+        Old values:
+                
+           Values are unchanged in the 2006 IAU report.                
+          
+        Current values:
+        
+        \begindata
+ 
+        BODY514_POLE_RA       = (  268.05     -0.009       0.  )
+        BODY514_POLE_DEC      = (   64.49      0.003       0.  )
+        BODY514_PM            = (    8.56    533.7004100   0.  )
+        BODY514_LONG_AXIS     = (    0.                        )
+ 
+        BODY514_NUT_PREC_RA  = ( 0.  -2.11  0. 0. 0. 0. 0. 0. 0.  0.04 )
+        BODY514_NUT_PREC_DEC = ( 0.  -0.91  0. 0. 0. 0. 0. 0. 0.  0.01 )
+        BODY514_NUT_PREC_PM  = ( 0.   1.91  0. 0. 0. 0. 0. 0. 0. -0.04 )
+ 
+        \begintext
+ 
+ 
+     Adrastea
+ 
+        Old values:
+                
+           Values are unchanged in the 2006 IAU report.                
+        
+        Current values:
+        
+        \begindata
+ 
+ 
+ 
+        BODY515_POLE_RA       = (  268.05     -0.009       0.  )
+        BODY515_POLE_DEC      = (   64.49      0.003       0.  )
+        BODY515_PM            = (   33.29   1206.9986602   0.  )
+        BODY515_LONG_AXIS     = (    0.                        )
+
+        \begintext
+ 
+ 
+     Metis
+  
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report.  
+              
+        Current values:
+           
+        \begindata
+
+        BODY516_POLE_RA       = (  268.05     -0.009       0.  )
+        BODY516_POLE_DEC      = (   64.49      0.003       0.  )
+        BODY516_PM            = (  346.09   1221.2547301   0.  )
+        BODY516_LONG_AXIS     = (    0.                        )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Saturn
+      
+     
+     Mimas
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report.  
+               
+        Current values:
+ 
+        \begindata
+  
+           BODY601_POLE_RA       = (   40.66     -0.036      0.  )
+           BODY601_POLE_DEC      = (   83.52     -0.004      0.  )
+           BODY601_PM            = (  337.46    381.9945550  0.  )
+           BODY601_LONG_AXIS     = (     0.                      )
+ 
+           BODY601_NUT_PREC_RA   = ( 0. 0.   13.56  0.    0.    0. 0. 0. 0. )
+           BODY601_NUT_PREC_DEC  = ( 0. 0.   -1.53  0.    0.    0. 0. 0. 0. )
+           BODY601_NUT_PREC_PM   = ( 0. 0.  -13.48  0.  -44.85  0. 0. 0. 0. )
+
+        \begintext
+ 
+ 
+     Enceladus
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report.  
+               
+        Current values:
+ 
+        \begindata
+ 
+           BODY602_POLE_RA       = (   40.66    -0.036       0. )
+           BODY602_POLE_DEC      = (   83.52    -0.004       0. )
+           BODY602_PM            = (    2.82   262.7318996   0. )
+           BODY602_LONG_AXIS     = (    0.                      )
+
+        \begintext
+ 
+ 
+ 
+     Tethys
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+ 
+        Current values:
+ 
+        \begindata
+ 
+           BODY603_POLE_RA       = (   40.66    -0.036       0. )
+           BODY603_POLE_DEC      = (   83.52    -0.004       0. )
+           BODY603_PM            = (   10.45   190.6979085   0. )
+           BODY603_LONG_AXIS     = (    0.                      )
+ 
+           BODY603_NUT_PREC_RA   = ( 0. 0. 0.   9.66   0.    0.  0.  0.  0. )
+           BODY603_NUT_PREC_DEC  = ( 0. 0. 0.  -1.09   0.    0.  0.  0.  0. )
+           BODY603_NUT_PREC_PM   = ( 0. 0. 0.  -9.60   2.23  0.  0.  0.  0. )
+
+        \begintext
+ 
+ 
+     Dione
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+ 
+        Current values:
+ 
+        \begindata
+   
+           BODY604_POLE_RA       = (  40.66      -0.036      0.  )
+           BODY604_POLE_DEC      = (  83.52      -0.004      0.  )
+           BODY604_PM            = (  357.00    131.5349316  0.  )
+           BODY604_LONG_AXIS     = (    0.                       )
+
+        \begintext
+ 
+ 
+ 
+     Rhea
+     
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+ 
+        Current values:
+ 
+        \begindata
+   
+           BODY605_POLE_RA       = (   40.38   -0.036       0. )
+           BODY605_POLE_DEC      = (   83.55   -0.004       0. )
+           BODY605_PM            = (  235.16   79.6900478   0. )
+           BODY605_LONG_AXIS     = (    0.                     )
+ 
+           BODY605_NUT_PREC_RA   = ( 0. 0. 0. 0. 0.   3.10   0. 0. 0. )
+           BODY605_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0.  -0.35   0. 0. 0. )
+           BODY605_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  -3.08   0. 0. 0. )
+ 
+        \begintext
+ 
+ 
+ 
+     Titan
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY606_POLE_RA       = (    36.41   -0.036      0. )
+           BODY606_POLE_DEC      = (    83.94   -0.004      0. )
+           BODY606_PM            = (   189.64   22.5769768  0. )
+           BODY606_LONG_AXIS     = (     0.                    )
+ 
+           BODY606_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 0.  2.66  0. 0 )
+           BODY606_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 0. -0.30  0. 0 )
+           BODY606_NUT_PREC_PM   = ( 0. 0. 0. 0. 0. 0. -2.64  0. 0 )
+
+        \begintext
+ 
+ 
+ 
+     Hyperion
+ 
+         The IAU report does not give an orientation model for Hyperion.
+         Hyperion's rotation is in chaotic and is not predictable for
+         long periods.
+
+ 
+     Iapetus
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY608_POLE_RA       = (   318.16  -3.949      0.  )
+           BODY608_POLE_DEC      = (    75.03  -1.143      0.  )
+           BODY608_PM            = (   350.20   4.5379572  0.  )
+           BODY608_LONG_AXIS     = (     0.                    )
+
+        \begintext
+ 
+ 
+ 
+     Phoebe
+ 
+
+        Old values:
+        
+           Values are from the 2003 IAU report. 
+  
+           body609_pole_ra       = ( 355.00       0.         0.  )
+           body609_pole_dec      = (  68.70       0.         0.  )
+           body609_pm            = ( 304.70     930.8338720  0.  )
+           body609_long_axis     = (    0.                       )
+
+        Current values:
+ 
+        \begindata 
+  
+           BODY609_POLE_RA       = ( 356.90       0.         0.  )
+           BODY609_POLE_DEC      = (  77.80       0.         0.  )
+           BODY609_PM            = ( 178.58     931.639      0.  )
+           BODY609_LONG_AXIS     = (    0.                       )
+
+        \begintext
+ 
+ 
+     Janus
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY610_POLE_RA       = (  40.58    -0.036       0. )
+           BODY610_POLE_DEC      = (  83.52    -0.004       0. )
+           BODY610_PM            = (  58.83   518.2359876   0. )
+           BODY610_LONG_AXIS     = (   0.                      )
+ 
+           BODY610_NUT_PREC_RA   = ( 0. -1.623  0. 0. 0. 0. 0. 0.  0.023 )
+           BODY610_NUT_PREC_DEC  = ( 0. -0.183  0. 0. 0. 0. 0. 0.  0.001 )
+           BODY610_NUT_PREC_PM   = ( 0.  1.613  0. 0. 0. 0. 0. 0. -0.023 )
+ 
+        \begintext
+ 
+ 
+ 
+     Epimetheus
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+         
+        Current values:
+ 
+        \begindata 
+  
+           BODY611_POLE_RA       = (  40.58    -0.036        0. )
+           BODY611_POLE_DEC      = (  83.52    -0.004        0. )
+           BODY611_PM            = ( 293.87   518.4907239    0. )
+           BODY611_LONG_AXIS     = (   0.                       )
+ 
+           BODY611_NUT_PREC_RA   = ( -3.153   0. 0. 0. 0. 0. 0.   0.086  0. )
+           BODY611_NUT_PREC_DEC  = ( -0.356   0. 0. 0. 0. 0. 0.   0.005  0. )
+           BODY611_NUT_PREC_PM   = (  3.133   0. 0. 0. 0. 0. 0.  -0.086  0. )
+
+        \begintext
+ 
+ 
+ 
+     Helene
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+ 
+           BODY612_POLE_RA       = (  40.85     -0.036        0. )
+           BODY612_POLE_DEC      = (  83.34     -0.004        0. )
+           BODY612_PM            = ( 245.12    131.6174056    0. )
+           BODY612_LONG_AXIS     = (   0.                        )
+
+        \begintext
+ 
+ 
+ 
+     Telesto
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+ 
+           BODY613_POLE_RA       = ( 50.51    -0.036      0.  )
+           BODY613_POLE_DEC      = ( 84.06    -0.004      0.  )
+           BODY613_PM            = ( 56.88   190.6979332  0.  )
+           BODY613_LONG_AXIS     = (  0.                      )
+
+        \begintext
+
+ 
+ 
+     Calypso
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY614_POLE_RA       = (   36.41    -0.036        0.  )
+           BODY614_POLE_DEC      = (   85.04    -0.004        0.  )
+           BODY614_PM            = (  153.51   190.6742373    0.  )
+           BODY614_LONG_AXIS     = (    0.                        )
+ 
+        \begintext
+ 
+ 
+ 
+     Atlas
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY615_POLE_RA       = (   40.58     -0.036      0. )
+           BODY615_POLE_DEC      = (   83.53     -0.004      0. )  
+           BODY615_PM            = (  137.88    598.3060000  0. )
+           BODY615_LONG_AXIS     = (    0.                      )
+
+        \begintext
+ 
+ 
+ 
+     Prometheus
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY616_POLE_RA       = (  40.58      -0.036    )
+           BODY616_POLE_DEC      = (  83.53      -0.004    )
+           BODY616_PM            = ( 296.14     587.289000 )
+           BODY616_LONG_AXIS     = (   0.                  )
+ 
+        \begintext
+ 
+ 
+ 
+     Pandora
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY617_POLE_RA       = (   40.58     -0.036      0.  )
+           BODY617_POLE_DEC      = (   83.53     -0.004      0.  )
+           BODY617_PM            = (  162.92    572.7891000  0.  )
+           BODY617_LONG_AXIS     = (     0.                      )
+ 
+        \begintext
+ 
+ 
+ 
+     Pan
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY618_POLE_RA       = (   40.6     -0.036       0. )
+           BODY618_POLE_DEC      = (   83.5     -0.004       0. )
+           BODY618_PM            = (   48.8    626.0440000   0. )
+           BODY618_LONG_AXIS     = (    0.                      )
+
+        \begintext
+ 
+ 
+ 
+ 
+ 
+Satellites of Uranus
+ 
+  
+ 
+     Ariel
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+ 
+        Current values:
+
+        \begindata 
+
+           BODY701_POLE_RA       = ( 257.43     0.          0. )
+           BODY701_POLE_DEC      = ( -15.10     0.          0. )
+           BODY701_PM            = ( 156.22  -142.8356681   0. )
+           BODY701_LONG_AXIS     = (   0.                      )
+ 
+           BODY701_NUT_PREC_RA   = (  0. 0. 0. 0. 0.
+                                      0. 0. 0. 0. 0.  0.    0.    0.29 )
+ 
+           BODY701_NUT_PREC_DEC  = (  0. 0. 0. 0. 0.
+                                      0. 0. 0. 0. 0.  0.    0.    0.28 )
+ 
+           BODY701_NUT_PREC_PM   = (  0. 0. 0. 0. 0.
+                                      0. 0. 0. 0. 0.  0.   0.05   0.08 )
+        \begintext
+ 
+ 
+ 
+     Umbriel
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+ 
+           BODY702_POLE_RA       = (  257.43     0.          0. )
+           BODY702_POLE_DEC      = (  -15.10     0.          0. )
+           BODY702_PM            = (  108.05   -86.8688923   0. )
+           BODY702_LONG_AXIS     = (    0.                      )
+ 
+           BODY702_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0.   0.    0.   0.21 )
+ 
+           BODY702_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0.   0.    0.   0.20 )
+ 
+           BODY702_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  
+                                     0. 0. 0. 0. 0.   0.  -0.09  0.   0.06 )
+
+        \begintext
+ 
+ 
+ 
+     Titania
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY703_POLE_RA       = (  257.43    0.          0. )
+           BODY703_POLE_DEC      = (  -15.10    0.          0. )
+           BODY703_PM            = (   77.74  -41.3514316   0. )
+           BODY703_LONG_AXIS     = (    0.                     )
+ 
+           BODY703_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0. 0. 0. 0.   0.29 )
+ 
+           BODY703_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0. 0. 0. 0.   0.28 )
+ 
+           BODY703_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  
+                                     0. 0. 0. 0. 0.   0. 0. 0. 0.   0.08 )
+        \begintext
+ 
+ 
+ 
+     Oberon
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY704_POLE_RA       = (  257.43    0.          0. )
+           BODY704_POLE_DEC      = (  -15.10    0.          0. )
+           BODY704_PM            = (    6.77  -26.7394932   0. )
+           BODY704_LONG_AXIS     = (    0.                     )
+ 
+ 
+           BODY704_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0.16 )
+ 
+           BODY704_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0.16 )
+ 
+           BODY704_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  
+                                     0. 0. 0. 0. 0.  
+                                     0. 0. 0. 0. 0.   0.04 )
+        \begintext
+ 
+ 
+ 
+     Miranda
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+
+           BODY705_POLE_RA      = (  257.43     0.         0. )
+           BODY705_POLE_DEC     = (  -15.08     0.         0. )
+           BODY705_PM           = (   30.70  -254.6906892  0. )
+           BODY705_LONG_AXIS    = (    0.                     )
+ 
+           BODY705_NUT_PREC_RA  = ( 0.     0.     0.    0.    0.  
+                                    0.     0.     0.    0.    0. 
+                                    4.41   0.     0.    0.    0. 
+                                    0.    -0.04   0.             )
+ 
+           BODY705_NUT_PREC_DEC = ( 0.     0.     0.    0.    0.  
+                                    0.     0.     0.    0.    0. 
+                                    4.25   0.     0.    0.    0. 
+                                    0.    -0.02   0.             )
+ 
+           BODY705_NUT_PREC_PM  = ( 0.     0.     0.    0.    0.  
+                                    0.     0.     0.    0.    0. 
+                                    1.15  -1.27   0.    0.    0.  
+                                    0.    -0.09   0.15           )
+        \begintext
+ 
+ 
+ 
+     Cordelia
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY706_POLE_RA      = (   257.31      0.         0.  )
+           BODY706_POLE_DEC     = (   -15.18      0.         0.  )
+           BODY706_PM           = (   127.69  -1074.5205730  0.  )
+           BODY706_LONG_AXIS    = (     0.                       )
+ 
+           BODY706_NUT_PREC_RA  = (   -0.15    0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )
+
+           BODY706_NUT_PREC_DEC = (    0.14    0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )  
+
+           BODY706_NUT_PREC_PM  = (   -0.04    0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             ) 
+ 
+        \begintext
+ 
+ 
+
+     Ophelia
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+   
+           BODY707_POLE_RA      = (  257.31     0.         0. )
+           BODY707_POLE_DEC     = (  -15.18     0.         0. )
+           BODY707_PM           = (  130.35  -956.4068150  0. )
+           BODY707_LONG_AXIS    = (    0.                     )
+ 
+           BODY707_NUT_PREC_RA  = (    0.     -0.09   0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )
+
+           BODY707_NUT_PREC_DEC = (    0.      0.09   0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )
+
+           BODY707_NUT_PREC_PM  = (    0.     -0.03   0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )
+ 
+        \begintext
+ 
+ 
+ 
+     Bianca
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY708_POLE_RA      = (  257.31     0.         0.  )
+           BODY708_POLE_DEC     = (  -15.18     0.         0.  )
+           BODY708_PM           = (  105.46  -828.3914760  0.  )
+           BODY708_LONG_AXIS    = (    0.                      )
+ 
+           BODY708_NUT_PREC_RA  = (    0.      0.    -0.16    0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.               )
+
+           BODY708_NUT_PREC_DEC = (    0.      0.     0.16    0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.               )
+
+           BODY708_NUT_PREC_PM  = (    0.      0.    -0.04    0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.               )
+
+        \begintext
+ 
+ 
+ 
+     Cressida
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+ 
+           BODY709_POLE_RA      = (  257.31      0.          0.  )
+           BODY709_POLE_DEC     = (  -15.18      0.          0.  )
+           BODY709_PM           = (   59.16   -776.5816320   0.  )
+           BODY709_LONG_AXIS    = (    0.                        )
+ 
+
+           BODY709_NUT_PREC_RA  = (    0.      0.     0.     -0.04   0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.                )
+
+
+           BODY709_NUT_PREC_DEC = (    0.      0.     0.      0.04   0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.                )
+
+
+           BODY709_NUT_PREC_PM  = (    0.      0.     0.     -0.01   0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.                )
+
+
+        \begintext
+ 
+ 
+ 
+     Desdemona
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+  
+           BODY710_POLE_RA      = ( 257.31      0.           0.  )
+           BODY710_POLE_DEC     = ( -15.18      0.           0.  )
+           BODY710_PM           = (  95.08   -760.0531690    0.  )
+           BODY710_LONG_AXIS    = (   0.                         )
+ 
+           BODY710_NUT_PREC_RA  = (   0.      0.     0.      0.    -0.17 
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+
+           BODY710_NUT_PREC_DEC = (   0.      0.     0.      0.     0.16 
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+
+           BODY710_NUT_PREC_PM  = (   0.      0.     0.      0.    -0.04  
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                 )
+
+        \begintext
+ 
+ 
+ 
+     Juliet
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY711_POLE_RA      = (  257.31     0.           0.   )
+           BODY711_POLE_DEC     = (  -15.18     0.           0.   )
+           BODY711_PM           = (  302.56  -730.1253660    0.   )
+           BODY711_LONG_AXIS    = (    0.                         )
+ 
+           BODY711_NUT_PREC_RA  = (   0.      0.     0.      0.     0.  
+                                     -0.06    0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                 )
+ 
+           BODY711_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.06    0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                 )
+  
+           BODY711_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                     -0.02    0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                 )
+ 
+        \begintext
+ 
+ 
+ 
+     Portia
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+    
+           BODY712_POLE_RA      = (  257.31      0.           0.   )
+           BODY712_POLE_DEC     = (  -15.18      0.           0.   )
+           BODY712_PM           = (   25.03   -701.4865870    0.   )
+           BODY712_LONG_AXIS    = (    0.                          )
+ 
+           BODY712_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
+                                      0.     -0.09   0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                )
+
+           BODY712_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.      0.09   0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.               )
+
+           BODY712_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                      0.     -0.02   0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.               )
+
+        \begintext
+ 
+ 
+ 
+     Rosalind
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+   
+           BODY713_POLE_RA      = ( 257.31      0.          0.  )
+           BODY713_POLE_DEC     = ( -15.18      0.          0.  )
+           BODY713_PM           = ( 314.90   -644.6311260   0.  )
+           BODY713_LONG_AXIS    = (   0.                        )
+ 
+           BODY713_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
+                                      0.      0.    -0.29    0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.               )
+
+           BODY713_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.28    0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.              )
+
+           BODY713_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                      0.      0.    -0.08    0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.              )
+ 
+        \begintext
+ 
+ 
+ 
+     Belinda
+ 
+       Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+ 
+           BODY714_POLE_RA      = (   257.31      0.         0. )
+           BODY714_POLE_DEC     = (   -15.18      0.         0. )
+           BODY714_PM           = (   297.46   -577.3628170  0. )
+           BODY714_LONG_AXIS    = (     0.                      )
+ 
+           BODY714_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.     -0.03   0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                )
+
+           BODY714_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.      0.03   0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                )
+
+           BODY714_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.     -0.01   0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                )
+        \begintext
+ 
+ 
+ 
+     Puck
+ 
+       Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY715_POLE_RA      = (  257.31      0.         0.  )
+           BODY715_POLE_DEC     = (  -15.18      0.         0.  )
+           BODY715_PM           = (   91.24   -472.5450690  0.  )
+           BODY715_LONG_AXIS    = (    0.                       )
+ 
+           BODY715_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.      0.    -0.33 
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+
+           BODY715_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.      0.     0.31
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+
+           BODY715_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.      0.    -0.09
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+  
+        \begintext
+ 
+ 
+ 
+ 
+Satellites of Neptune
+ 
+ 
+     Triton
+ 
+       Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+ 
+        Current values:
+ 
+        \begindata
+
+           BODY801_POLE_RA       = ( 299.36     0.         0.  )
+           BODY801_POLE_DEC      = (  41.17     0.         0.  )
+           BODY801_PM            = ( 296.53   -61.2572637  0.  )
+           BODY801_LONG_AXIS     = (   0.                      )
+ 
+ 
+           BODY801_NUT_PREC_RA   = (  0.      0.      0.      0.  
+                                      0.      0.      0.    -32.35    
+                                      0.     -6.28   -2.08   -0.74       
+                                     -0.28   -0.11   -0.07   -0.02    
+                                     -0.01                         )
+ 
+ 
+           BODY801_NUT_PREC_DEC  = (  0.      0.      0.      0.  
+                                      0.      0.      0.     22.55    
+                                      0.      2.10    0.55    0.16   
+                                      0.05    0.02    0.01    0.
+                                      0.                           )
+ 
+ 
+           BODY801_NUT_PREC_PM   = (  0.      0.      0.      0.  
+                                      0.      0.      0.     22.25   
+                                      0.      6.73    2.05    0.74   
+                                      0.28    0.11    0.05    0.02
+                                      0.01                         )
+  
+        \begintext
+ 
+ 
+ 
+ 
+     Nereid
+ 
+        Old values:
+ 
+           Values are from the 1988 IAU report [10].  Note that this 
+           rotation model pre-dated the 1989 Voyager 2 Neptune
+           encounter.
+
+ 
+           body802_pole_ra       = (    273.48    0.        0.  )
+           body802_pole_dec      = (     67.22    0.        0.  )
+           body802_pm            = (    237.22    0.9996465 0.  )
+           body802_long_axis     = (      0.                    )
+ 
+ 
+           The report seems to have a typo:  in the nut_prec_ra expression,
+           where the report gives  -0.51 sin 3N3, we use -0.51 3N2.
+ 
+           body802_nut_prec_ra   = (  0.    -17.81
+                                      0.      0.     0.      0.
+                                      0.      0.     0.
+                                      2.56   -0.51   0.11   -0.03  )
+ 
+           body802_nut_prec_dec  = (  0.     -6.67
+                                      0.      0.     0.      0.
+                                      0.      0.     0.
+                                      0.47   -0.07   0.01          )
+ 
+           body802_nut_prec_pm   = (  0.     16.48
+                                      0.      0.     0.      0.
+                                      0.      0.     0.
+                                     -2.57    0.51 -0.11    0.02  )
+ 
+ 
+ 
+        Current values:
+ 
+           The 2006 report [1] states that values for Nereid are not
+           given because Nereid is not in synchronous rotation with Neptune
+           (p. 167).
+ 
+ 
+ 
+     Naiad
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+ 
+        \begindata
+  
+           BODY803_POLE_RA       = (  299.36      0.          0.  )
+           BODY803_POLE_DEC      = (   43.36      0.          0.  )
+           BODY803_PM            = (  254.06  +1222.8441209   0.  )
+           BODY803_LONG_AXIS     = (    0.                        )
+ 
+ 
+           BODY803_NUT_PREC_RA   = (    0.70     -6.49     0.      0.
+                                        0.        0.       0.      0.
+                                        0.25      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+ 
+           BODY803_NUT_PREC_DEC  = (   -0.51     -4.75     0.      0.
+                                        0.        0.       0.      0.
+                                        0.09      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+ 
+           BODY803_NUT_PREC_PM   = (   -0.48      4.40     0.      0.
+                                        0.        0.       0.      0.
+                                       -0.27      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+    
+        \begintext
+ 
+ 
+ 
+ 
+     Thalassa
+ 
+
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY804_POLE_RA       = (  299.36      0.          0. )
+           BODY804_POLE_DEC      = (   43.45      0.          0. )
+           BODY804_PM            = (  102.06   1155.7555612   0. )  
+           BODY804_LONG_AXIS     = (    0.                       )
+ 
+ 
+           BODY804_NUT_PREC_RA   = (    0.70      0.      -0.28    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+   
+  
+           BODY804_NUT_PREC_DEC  = (   -0.51      0.      -0.21    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0. 
+                                        0.                             )
+ 
+           BODY804_NUT_PREC_PM   = (   -0.48      0.       0.19    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0. 
+                                        0.                             )
+                                                                 
+        \begintext
+ 
+ 
+ 
+     Despina
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+ 
+        \begindata
+  
+           BODY805_POLE_RA       = (  299.36      0.          0. )
+           BODY805_POLE_DEC      = (   43.45      0.          0. )
+           BODY805_PM            = (  306.51  +1075.7341562   0. )
+           BODY805_LONG_AXIS     = (    0.                       )
+ 
+ 
+           BODY805_NUT_PREC_RA   = (    0.70      0.       0.     -0.09
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                              )
+ 
+           BODY805_NUT_PREC_DEC  = (   -0.51      0.       0.     -0.07
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                              )
+ 
+           BODY805_NUT_PREC_PM   = (   -0.49      0.       0.      0.06
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                              )
+        \begintext
+ 
+ 
+ 
+     Galatea
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+ 
+        \begindata
+  
+           BODY806_POLE_RA       = (   299.36      0.          0. )
+           BODY806_POLE_DEC      = (    43.43      0.          0. )
+           BODY806_PM            = (   258.09    839.6597686   0. )
+           BODY806_LONG_AXIS     = (     0.                       )
+ 
+ 
+           BODY806_NUT_PREC_RA   = (    0.70      0.       0.      0.
+                                       -0.07      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+ 
+           BODY806_NUT_PREC_DEC  = (   -0.51      0.       0.      0.
+                                       -0.05      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+ 
+           BODY806_NUT_PREC_PM   = (   -0.48      0.       0.      0.
+                                        0.05      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             ) 
+        \begintext
+
+ 
+     Larissa
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+  
+        \begindata
+
+           BODY807_POLE_RA       = (   299.36     0.           0. )
+           BODY807_POLE_DEC      = (    43.41     0.           0. )
+           BODY807_PM            = (   179.41  +649.0534470    0. )
+           BODY807_LONG_AXIS     = (     0.                       )
+ 
+ 
+           BODY807_NUT_PREC_RA   = (    0.70      0.       0.      0.
+                                        0.       -0.27     0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+ 
+           BODY807_NUT_PREC_DEC  = (   -0.51      0.       0.      0.
+                                        0.       -0.20     0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+ 
+           BODY807_NUT_PREC_PM   = (   -0.48      0.       0.      0.
+                                        0.        0.19     0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+        \begintext
+ 
+ 
+ 
+     Proteus
+ 
+
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY808_POLE_RA       = (  299.27      0.          0.  )
+           BODY808_POLE_DEC      = (   42.91      0.          0.  )
+           BODY808_PM            = (   93.38   +320.7654228   0.  )
+           BODY808_LONG_AXIS     = (    0.                        )
+ 
+ 
+           BODY808_NUT_PREC_RA   = (    0.70      0.       0.      0.
+                                        0.        0.      -0.05    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+ 
+           BODY808_NUT_PREC_DEC  = (   -0.51      0.       0.      0.
+                                        0.        0.      -0.04    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+ 
+           BODY808_NUT_PREC_PM   = (   -0.48      0.       0.      0.
+                                        0.        0.       0.04    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+   
+        \begintext
+  
+ 
+ 
+ 
+ 
+Satellites of Pluto
+ 
+     Charon
+ 
+        Old values:
+        
+           Values are from the 2003 IAU report. 
+ 
+           body901_pole_ra       = (   313.02     0.         0. )
+           body901_pole_dec      = (     9.09     0.         0. )
+           body901_pm            = (    56.77   -56.3623195  0. )
+           body901_long_axis     = (     0.                     )
+               
+        Current values:
+ 
+        \begindata
+ 
+           BODY901_POLE_RA       = (   312.993    0.         0. )
+           BODY901_POLE_DEC      = (     6.163    0.         0. )
+           BODY901_PM            = (    57.305  -56.3625225  0. )
+           BODY901_LONG_AXIS     = (     0.                     )
+
+        \begintext
+ 
+ 
+ 
+Orientation constants for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+19P/Borrelly
+
+
+        Current values:
+ 
+        \begindata
+
+           BODY1000005_POLE_RA       = (   218.5      0.         0.  )
+           BODY1000005_POLE_DEC      = (   -12.5      0.         0.  )
+           BODY1000005_PM            = (   000.     390.0        0.  )
+           BODY1000005_LONG_AXIS     = (     0.                      )
+ 
+        \begintext
+
+
+
+9P/Tempel 1
+
+
+        Current values:
+ 
+        \begindata
+
+           BODY1000093_POLE_RA       = (   294.       0.         0.  )
+           BODY1000093_POLE_DEC      = (    73.       0.         0.  )
+           BODY1000093_PM            = (   252.63   212.064      0.  )
+           BODY1000093_LONG_AXIS     = (     0.                      )
+ 
+        \begintext
+
+
+Vesta
+
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY2000004_POLE_RA       = (   301.      0.         0.  )
+           BODY2000004_POLE_DEC      = (    41.      0.         0.  )
+           BODY2000004_PM            = (   292.   1617.332776   0.  )
+           BODY2000004_LONG_AXIS     = (     0.                     )
+ 
+        \begintext
+
+Eros
+
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY2000433_POLE_RA       = (   11.35       0.           0. )
+           BODY2000433_POLE_DEC      = (   17.22       0.           0. )
+           BODY2000433_PM            = (  326.07    1639.38864745   0. )
+           BODY2000433_LONG_AXIS     = (    0.                         )
+ 
+        \begintext
+
+
+Itokawa
+
+
+        Current values:
+ 
+        \begindata
+
+           BODY2025143_POLE_RA       = (   90.53       0.           0. )
+           BODY2025143_POLE_DEC      = (  -66.30       0.           0. )
+           BODY2025143_PM            = (  000.0      712.143        0. )
+           BODY2025143_LONG_AXIS     = (    0.                         )
+ 
+        \begintext
+
+
+
+Ida
+
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY2431010_POLE_RA       = (  168.76      0.         0. )
+           BODY2431010_POLE_DEC      = (   -2.88      0.         0. )
+           BODY2431010_PM            = (  265.95  +1864.6280070  0. )
+           BODY2431010_LONG_AXIS     = (    0.                      )
+ 
+        \begintext
+
+Gaspra
+
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+               
+        Current values:
+ 
+        \begindata 
+ 
+           BODY9511010_POLE_RA       = (   9.47     0.         0. )
+           BODY9511010_POLE_DEC      = (  26.70     0.         0. )
+           BODY9511010_PM            = (  83.67  1226.9114850  0. )
+           BODY9511010_LONG_AXIS     = (   0.                     )
+
+        \begintext
+
+
+
+
+
+
+
+
+
+ 
+Radii of Sun and Planets
+--------------------------------------------------------
+ 
+ 
+Sun
+ 
+     Value for the Sun is from the [3], page K7.
+ 
+        \begindata
+ 
+        BODY10_RADII      = (   696000.     696000.      696000.     )
+ 
+        \begintext
+ 
+ 
+Mercury
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY199_RADII     = ( 2439.7   2439.7   2439.7 )
+ 
+        \begintext
+ 
+ 
+Venus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY299_RADII     = ( 6051.8   6051.8   6051.8 )
+ 
+        \begintext
+ 
+ 
+Earth
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+
+        \begindata
+ 
+        BODY399_RADII     = ( 6378.14   6378.14   6356.75 )
+ 
+        \begintext
+ 
+ 
+Mars
+ 
+ 
+     Old values:
+
+        body499_radii       = (     3397.      3397.         3375.     )
+ 
+     Current values:
+
+
+        The IAU report gives separate values for the north and south
+        polar radii:
+
+           north:  3373.19
+           south:  3379.21 
+
+        We use the average of these values as the polar radius for
+        the triaxial model.
+ 
+        \begindata
+ 
+        BODY499_RADII       = ( 3396.19   3396.19   3376.20 )
+ 
+        \begintext
+ 
+ 
+ 
+Jupiter
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY599_RADII     = ( 71492   71492   66854 )
+ 
+        \begintext
+ 
+ 
+ 
+Saturn
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY699_RADII     = ( 60268   60268   54364 )
+ 
+        \begintext
+ 
+ 
+ 
+Uranus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY799_RADII     = ( 25559   25559   24973 )
+ 
+        \begintext
+ 
+ 
+ 
+Neptune
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+  
+     Current values:
+ 
+        (Values are for the 1 bar pressure level.)
+ 
+        \begindata
+ 
+        BODY899_RADII     = ( 24764   24764  24341 )
+ 
+        \begintext
+ 
+ 
+ 
+Pluto
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY999_RADII     = ( 1195   1195   1195 )
+ 
+        \begintext
+ 
+
+
+
+Radii of Satellites
+--------------------------------------------------------
+ 
+ 
+Moon
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY301_RADII     = ( 1737.4   1737.4   1737.4 )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Mars
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY401_RADII     = ( 13.4    11.2    9.2 )
+        BODY402_RADII     = (  7.5     6.1    5.2 )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Jupiter
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+         
+        \begindata
+ 
+        BODY501_RADII     = ( 1829.4   1819.3   1815.7  )
+        BODY502_RADII     = ( 1564.13  1561.23  1560.93 )
+        BODY503_RADII     = ( 2632.4   2632.29  2632.35 )
+        BODY504_RADII     = ( 2409.4   2409.2   2409.3  )
+        BODY505_RADII     = (  125       73       64    )
+ 
+        \begintext
+ 
+        Only mean radii are available in the 2003 IAU report for bodies
+        506-513.
+ 
+        \begindata
+ 
+        BODY506_RADII    = (    85       85       85   )
+        BODY507_RADII    = (    40       40       40   )
+        BODY508_RADII    = (    18       18       18   )
+        BODY509_RADII    = (    14       14       14   )
+        BODY510_RADII    = (    12       12       12   )
+        BODY511_RADII    = (    15       15       15   )
+        BODY512_RADII    = (    10       10       10   )
+        BODY513_RADII    = (     5        5        5   )
+        BODY514_RADII    = (    58       49       42   )
+        BODY515_RADII    = (    10        8        7   )
+ 
+        \begintext
+ 
+        The value for the second radius for body 516 is not given in 
+        2003 IAU report.   The values given are:
+ 
+           BODY516_RADII    = (  30   ---   20   )
+ 
+        For use within the SPICE system, we use only the mean radius.
+        \begindata
+ 
+        BODY516_RADII    = (  21.5   21.5  21.5  )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Saturn
+ 
+ 
+     Old values:
+ 
+        Values are from the 2003 IAU report.
+    
+        body601_radii     = (  209.1   196.2   191.4 )
+        body602_radii     = (  256.3   247.3   244.6 )
+        body603_radii     = (  535.6   528.2   525.8 )
+        body604_radii     = (  560     560     560   )
+        body605_radii     = (  764     764     764   )
+        body606_radii     = ( 2575    2575    2575   )
+        body607_radii     = (  164     130     107   )
+        body608_radii     = (  718     718     718   )
+        body609_radii     = (  115     110     105   )
+        body610_radii     = (   97.0    95.0    77.0 )
+        body611_radii     = (   69.0    55.0    55.0 )
+ 
+ 
+        Only the first equatorial radius for Helene (body 612) was given in the
+        2003 IAU report:
+ 
+            body612_radii     = (       17.5        ---          ---     )
+ 
+        The mean radius was 16km; we used this radius for all three axes, as
+        we do for the satellites for which only the mean radius is available.
+ 
+ 
+        body612_radii     = (   16      16       16  )
+        body613_radii     = (   15      12.5     7.5 )
+        body614_radii     = (   15.0     8.0     8.0 )
+        body615_radii     = (   18.5    17.2    13.5 )
+        body616_radii     = (   74.0    50.0    34.0 )
+        body617_radii     = (   55.0    44.0    31.0 )
+  
+      
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY601_RADII     = (  207.4     196.8     190.6  )
+        BODY602_RADII     = (  256.6     251.4     248.3  )
+        BODY603_RADII     = (  540.4     531.1     527.5  )
+        BODY604_RADII     = (  563.8     561.0     560.3  )
+        BODY605_RADII     = (  767.2     762.5     763.1  )
+        BODY606_RADII     = ( 2575      2575      2575    )
+        BODY607_RADII     = (  164       130       107    )
+        BODY608_RADII     = (  747.4     747.4     712.4  )
+        BODY609_RADII     = (  108.6     107.7     101.5  )
+        BODY610_RADII     = (   97.0      95.0      77.0  )
+        BODY611_RADII     = (   69.0      55.0      55.0  )
+ 
+        \begintext
+ 
+        Only the first equatorial radius for Helene (body 612) is given in the
+        2006 IAU report:
+ 
+            BODY612_RADII     = (       17.5        ---          ---     )
+ 
+        The mean radius is 16km; we use this radius for all three axes, as
+        we do for the satellites for which only the mean radius is available.
+ 
+ 
+        \begindata
+ 
+        BODY612_RADII     = (  17.5      17.5      17.5  )
+        BODY613_RADII     = (  15        12.5       7.5  )
+        BODY614_RADII     = (  15.0       8.0       8.0  )
+        BODY615_RADII     = (  18.5      17.2      13.5  )
+        BODY616_RADII     = (  74.0      50.0      34.0  )
+        BODY617_RADII     = (  55.0      44.0      31.0  )
+ 
+        \begintext
+ 
+ 
+         For Pan, only a mean radius is given in the 2006 report.
+ 
+        \begindata
+ 
+        BODY618_RADII     = (   10       10     10   )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Uranus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY701_RADII     = (  581.1   577.9   577.7 )
+        BODY702_RADII     = (  584.7   584.7   584.7 )
+        BODY703_RADII     = (  788.9   788.9   788.9 )
+        BODY704_RADII     = (  761.4   761.4   761.4 )
+        BODY705_RADII     = (  240.4   234.2   232.9 )
+ 
+        \begintext
+ 
+        The 2000 report gives only mean radii for satellites 706--715.
+ 
+        \begindata
+ 
+        BODY706_RADII     = (   13      13      13 )
+        BODY707_RADII     = (   15      15      15 )
+        BODY708_RADII     = (   21      21      21 )
+        BODY709_RADII     = (   31      31      31 )
+        BODY710_RADII     = (   27      27      27 )
+        BODY711_RADII     = (   42      42      42 )
+        BODY712_RADII     = (   54      54      54 )
+        BODY713_RADII     = (   27      27      27 )
+        BODY714_RADII     = (   33      33      33 )
+        BODY715_RADII     = (   77      77      77 )
+ 
+        \begintext
+ 
+ 
+ 
+ 
+Satellites of Neptune
+ 
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+ 
+     Current values:
+ 
+        The 2000 report gives mean radii only for bodies 801-806.
+ 
+        \begindata
+ 
+        BODY801_RADII     = ( 1352.6  1352.6  1352.6 )
+        BODY802_RADII     = (  170     170     170   )
+        BODY803_RADII     = (   29      29     29    )
+        BODY804_RADII     = (   40      40     40    )
+        BODY805_RADII     = (   74      74     74    )
+        BODY806_RADII     = (   79      79     79    )
+ 
+        \begintext
+ 
+ 
+        The second equatorial radius for Larissa is not given in the 2000
+        report.  The available values are:
+ 
+            BODY807_RADII     = (   104     ---     89   )
+ 
+        For use within the SPICE system, we use only the mean radius.
+        \begindata
+ 
+        BODY807_RADII     = (   96      96     96   )
+        BODY808_RADII     = (  218     208    201   )
+ 
+        \begintext
+ 
+ 
+ 
+ 
+Satellites of Pluto
+ 
+     
+     Old values:
+ 
+        Values are from the 2003 IAU report. 
+
+        BODY901_RADII     = (  593     593    593   )
+             
+     Current values:
+ 
+        \begindata
+ 
+        BODY901_RADII     = (  605     605    605   )
+ 
+        \begintext
+ 
+
+
+Radii for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+19P/Borrelly
+
+
+     Current values:
+ 
+
+        The value in the data assignment below is the 
+        "effective radius."
+
+        The first principal axis length is 
+
+           3.5 km
+
+        The lengths of the other semi-axes are not provided
+        by [1].
+
+        \begindata
+ 
+        BODY1000005_RADII     = (  4.22   4.22   4.22  )
+ 
+        \begintext
+
+
+
+Halley
+
+
+     Current values:
+
+        \begindata
+ 
+        BODY1000036_RADII     = (  8.0   4.0   4.0  )
+ 
+        \begintext
+
+
+
+9P/Tempel 1
+
+
+     Current values:
+
+
+        The value in the data assignment below is the 
+        "effective radius."
+            
+        According to [1]:
+
+           The maximum and minimum radii are not properly 
+           the values of the principal semi-axes, they
+           are half the maximum and minimum values of the
+           diameter. Due to the large deviations from a
+           simple ellipsoid, they may not correspond with
+           measurements along the principal axes, or be
+           orthogonal to each other.
+
+        \begindata
+ 
+        BODY1000093_RADII     = (  3.0   3.0   3.0  )
+ 
+        \begintext
+
+
+81P/Wild 2
+
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY1000107_RADII     = (  2.7   1.9   1.5 )
+ 
+        \begintext
+
+
+Ceres
+
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2000001_RADII     = ( 487.3  487.3  454.7 )
+ 
+        \begintext
+
+
+Vesta
+
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2000004_RADII     = ( 289.  280.  229.  )
+ 
+        \begintext
+
+
+Toutatis
+
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2004179_RADII     = (  2.13  1.015  0.85  )
+ 
+        \begintext
+
+ 
+Kleopatra
+
+
+     Old values:
+
+        Values are from the 2003 report.
+
+ 
+        body2000216_radii     = (   108.5      47    40.5  )
+ 
+
+     Current values:
+ 
+ 
+        No values are provided in the 2006 report.
+
+
+Mathilde
+
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2000253_RADII     = (  33.   24.   23.  )
+ 
+        \begintext
+       
+Eros
+ 
+
+     Current values:
+ 
+ 
+        \begindata
+ 
+        BODY2000433_RADII     = (  17.0   5.5   5.5  )
+ 
+        \begintext
+
+
+Itokawa
+
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2025143_RADII     = (  0.535   0.294   0.209  )
+ 
+        \begintext
+
+
+
+Gaspra
+
+     
+     Current values:
+ 
+ 
+        \begindata
+ 
+        BODY9511010_RADII     = (    9.1    5.2    4.4 )
+ 
+        \begintext
+
+        
+        
+        
+Ida
+
+     
+     Current values:
+ 
+ 
+        \begindata
+ 
+        BODY2431010_RADII     = (   26.8   12.0    7.6 )
+ 
+        \begintext
+
+        
+
+===========================================================================
+End of file pck00009.tpc
+===========================================================================
+
+
+
diff --git a/tests/pytests/data/isds/hayabusanirs_isd.json b/tests/pytests/data/isds/hayabusanirs_isd.json
new file mode 100644
index 0000000..2d80c5f
--- /dev/null
+++ b/tests/pytests/data/isds/hayabusanirs_isd.json
@@ -0,0 +1,260 @@
+{
+  "isis_camera_version": 1,
+  "image_lines": 1,
+  "image_samples": 1,
+  "name_platform": "HAYABUSA",
+  "name_sensor": "HAYABUSA_NIRS",
+  "reference_height": {
+    "maxheight": 1000,
+    "minheight": -1000,
+    "unit": "m"
+  },
+  "name_model": "USGS_ASTRO_FRAME_SENSOR_MODEL",
+  "center_ephemeris_time": 180486501.50056908,
+  "radii": {
+    "semimajor": 0.274,
+    "semiminor": 0.138,
+    "unit": "km"
+  },
+  "body_rotation": {
+    "time_dependent_frames": [
+      2025143,
+      1
+    ],
+    "ck_table_start_time": 180486501.50056908,
+    "ck_table_end_time": 180486501.50056908,
+    "ck_table_original_size": 1,
+    "ephemeris_times": [
+      180486501.50056908
+    ],
+    "quaternions": [
+      [
+        -0.16055829299369445,
+        -0.7903828492935261,
+        0.57934404912348,
+        0.11779838215701044
+      ]
+    ],
+    "angular_velocities": [
+      [
+        -2.512589340257489e-08,
+        5.614694041984393e-05,
+        -0.00013244767067246738
+      ]
+    ],
+    "reference_frame": 1
+  },
+  "instrument_pointing": {
+    "time_dependent_frames": [
+      -130000,
+      1
+    ],
+    "ck_table_start_time": 180486501.50056908,
+    "ck_table_end_time": 180486501.50056908,
+    "ck_table_original_size": 1,
+    "ephemeris_times": [
+      180486501.50056908
+    ],
+    "quaternions": [
+      [
+        -0.5455420110134627,
+        -0.314681795394347,
+        0.6704074453706204,
+        -0.3923176507097482
+      ]
+    ],
+    "angular_velocities": [
+      [
+        -1.0633204332538909e-06,
+        3.518145848279672e-06,
+        -2.36852765977406e-06
+      ]
+    ],
+    "reference_frame": 1,
+    "constant_frames": [
+      -130200,
+      -130201,
+      -130000
+    ],
+    "constant_rotation": [
+      4.167163544668958e-08,
+      0.9999999997806756,
+      2.0943909565874054e-05,
+      0.9999980205966593,
+      8.20744220945079e-17,
+      -0.0019896740344834754,
+      -0.001989674034047091,
+      2.0943951022400417e-05,
+      -0.9999980203773353
+    ]
+  },
+  "naif_keywords": {
+    "BODY2025143_RADII": [
+      0.274,
+      0.156,
+      0.138
+    ],
+    "BODY_FRAME_CODE": 2025143,
+    "BODY_CODE": 2025143,
+    "INS-130200_SWAP_OBSERVER_TARGET": "TRUE",
+    "FRAME_-130200_CLASS": 4.0,
+    "INS-130200_LT_SURFACE_CORRECT": "FALSE",
+    "INS-130200_LIGHTTIME_CORRECTION": "NONE",
+    "INS-130200_FOV_BOUNDARY_CORNERS": [
+      0.000872664,
+      0.000872664,
+      1.0,
+      -0.000872664,
+      0.000872664,
+      1.0,
+      -0.000872664,
+      -0.000872664,
+      1.0,
+      0.000872664
+    ],
+    "INS-130200_BORESIGHT_SAMPLE": 0.0,
+    "INS-130200_ITRANSL": [
+      0.0,
+      -21.064639754005,
+      0.0
+    ],
+    "INS-130200_ITRANSS": [
+      0.0,
+      0.0,
+      21.064639754005
+    ],
+    "TKFRAME_-130200_RELATIVE": "HAYABUSA_NIRS_IDEAL",
+    "TKFRAME_-130200_UNITS": "DEGREES",
+    "FRAME_-130200_CLASS_ID": -130200.0,
+    "INS-130200_TRANSX": [
+      0.0,
+      0.0,
+      -0.047472922
+    ],
+    "INS-130200_TRANSY": [
+      0.0,
+      0.047472922,
+      0.0
+    ],
+    "INS-130200_PIXEL_PITCH": 0.047472922,
+    "INS-130200_BORESIGHT": [
+      0.0,
+      0.0,
+      1.0
+    ],
+    "TKFRAME_-130200_ANGLES": [
+      -0.114,
+      -0.0012,
+      0.0
+    ],
+    "FRAME_-130200_CENTER": -130.0,
+    "INS-130200_FOV_SHAPE": "POLYGON",
+    "INS-130200_FOCAL_LENGTH": 0.0272,
+    "TKFRAME_-130200_AXES": [
+      1.0,
+      2.0,
+      3.0
+    ],
+    "TKFRAME_-130200_SPEC": "ANGLES",
+    "FRAME_-130200_NAME": "HAYABUSA_NIRS",
+    "INS-130200_FOV_FRAME": "HAYABUSA_NIRS",
+    "INS-130200_BORESIGHT_LINE": 0.0,
+    "OBJECT_2025143_FRAME": "ITOKAWA_FIXED",
+    "FRAME_2025143_CLASS": 2.0,
+    "BODY2025143_PM": [
+      129.73,
+      712.1437611,
+      0.0
+    ],
+    "BODY2025143_POLE_RA": [
+      90.02564,
+      0.0,
+      0.0
+    ],
+    "FRAME_2025143_CLASS_ID": 2025143.0,
+    "BODY2025143_POLE_DEC": [
+      -67.02704,
+      0.0,
+      0.0
+    ],
+    "FRAME_2025143_CENTER": 2025143.0,
+    "BODY2025143_LONG_AXIS": 0.0,
+    "FRAME_2025143_NAME": "ITOKAWA_FIXED"
+  },
+  "detector_sample_summing": 1,
+  "detector_line_summing": 1,
+  "focal_length_model": {
+    "focal_length": 0.0272
+  },
+  "detector_center": {
+    "line": 0.0,
+    "sample": 0.0
+  },
+  "focal2pixel_lines": [
+    0.0,
+    -21.064639754005,
+    0.0
+  ],
+  "focal2pixel_samples": [
+    0.0,
+    0.0,
+    21.064639754005
+  ],
+  "optical_distortion": {
+    "radial": {
+      "coefficients": [
+        0.0,
+        0.0,
+        0.0
+      ]
+    }
+  },
+  "starting_detector_line": 0,
+  "starting_detector_sample": 0,
+  "instrument_position": {
+    "spk_table_start_time": 180486501.50056908,
+    "spk_table_end_time": 180486501.50056908,
+    "spk_table_original_size": 1,
+    "ephemeris_times": [
+      180486501.50056908
+    ],
+    "positions": [
+      [
+        16.755715427571857,
+        -3.217421876546119,
+        -1.8170226741623652
+      ]
+    ],
+    "velocities": [
+      [
+        2.1028869650818293e-05,
+        -3.528483828922901e-07,
+        -4.334941153621985e-07
+      ]
+    ],
+    "reference_frame": 1
+  },
+  "sun_position": {
+    "spk_table_start_time": 180486501.50056908,
+    "spk_table_end_time": 180486501.50056908,
+    "spk_table_original_size": 1,
+    "ephemeris_times": [
+      180486501.50056908
+    ],
+    "positions": [
+      [
+        157546274.8360496,
+        -51773929.736718364,
+        -27634141.47982414
+      ]
+    ],
+    "velocities": [
+      [
+        3.4484780727773905,
+        27.389486836276948,
+        12.105185350948945
+      ]
+    ],
+    "reference_frame": 1
+  }
+}
\ No newline at end of file
diff --git a/tests/pytests/test_hayabusa_drivers.py b/tests/pytests/test_hayabusa_drivers.py
index 2da7df8..f36384c 100644
--- a/tests/pytests/test_hayabusa_drivers.py
+++ b/tests/pytests/test_hayabusa_drivers.py
@@ -8,10 +8,11 @@ import json
 
 from conftest import get_image, get_image_label, get_isd, get_image_kernels, convert_kernels, compare_dicts
 import ale
-from ale.drivers.hayabusa_drivers import HayabusaAmicaIsisLabelNaifSpiceDriver
+from ale.drivers.hayabusa_drivers import HayabusaAmicaIsisLabelNaifSpiceDriver, HayabusaNirsIsisLabelNaifSpiceDriver
 from ale import util
 
 
+# AMICA Tests
 @pytest.fixture(scope='module')
 def test_amica_kernels():
     kernels = get_image_kernels('st_2458542208_v')
@@ -29,7 +30,7 @@ def test_amica_load(test_amica_kernels):
     assert compare_dicts(isd_obj, compare_dict) == []
 
 
-class test_nac_isis_naif(unittest.TestCase):
+class test_amica_isis_naif(unittest.TestCase):
     def setUp(self):
         label = get_image_label("st_2458542208_v", "isis")
         self.driver = HayabusaAmicaIsisLabelNaifSpiceDriver(label)
@@ -42,3 +43,46 @@ class test_nac_isis_naif(unittest.TestCase):
 
     def test_sensor_name(self):
         assert self.driver.sensor_name == "HAYABUSA_AMICA"
+
+
+# NIRS Tests
+@pytest.fixture(scope='module')
+def test_nirs_kernels():
+    kernels = get_image_kernels('2392975548_lvl3_0')
+    updated_kernels, binary_kernels = convert_kernels(kernels)
+    yield updated_kernels
+    for kern in binary_kernels:
+        os.remove(kern)
+
+def test_nirs_load(test_nirs_kernels):
+    label_file = get_image_label('2392975548_lvl3_0', 'isis')
+    compare_dict = get_isd("hayabusanirs")
+
+    isd_str = ale.loads(label_file, props={'kernels': test_nirs_kernels}, verbose=True)
+    isd_obj = json.loads(isd_str)
+    assert compare_dicts(isd_obj, compare_dict) == []
+
+
+class test_nirs_isis_naif(unittest.TestCase):
+    def setUp(self):
+        label = get_image_label("2392975548_lvl3_0", "isis")
+        self.driver = HayabusaNirsIsisLabelNaifSpiceDriver(label)
+
+    def test_instrument_id(self):
+        assert self.driver.instrument_id == "HAYABUSA_NIRS"
+    
+    def test_sensor_model_version(self):
+        assert self.driver.sensor_model_version == 1
+
+    def test_sensor_name(self):
+        assert self.driver.sensor_name == "HAYABUSA_NIRS"
+
+    def test_exposure_duration(self):
+        with patch('ale.drivers.hayabusa_drivers.spice.scs2e', return_value=12345) as scs2e:
+            assert self.driver.exposure_duration == 0
+            scs2e.assert_called_with(-130, '1/2392973413.133')
+    
+    def test_ephemeris_stop_time(self):
+        with patch('ale.drivers.hayabusa_drivers.spice.scs2e', return_value=12345) as scs2e:
+            assert self.driver.ephemeris_stop_time == 12345
+            scs2e.assert_called_with(-130, '1/2392975548.000')
-- 
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