From a7d8a148f54d5141c63ed45a24a71c890ca11de7 Mon Sep 17 00:00:00 2001
From: Amy Stamile <74275278+amystamile-usgs@users.noreply.github.com>
Date: Thu, 14 Dec 2023 14:14:15 -0700
Subject: [PATCH] DawnVIR Driver (#566)

* Draft DawnVIR driver

* Adds interpolate and framechain updates

* fixes line scan rate

* Fixed FrameChain

* updated gitignore

* Fixed Body Rotation

* fixed rebase deletion

* added tests

* failing tests - no alespiceroot

* fix tests

* Initial fixes for dawn virs

* Fixed tests

* addressed PR feedback

* Fixed dawn vir isd

---------

Co-authored-by: acpaquette <acp263@nau.edu>
---
 .gitignore                                    |     2 +
 CHANGELOG.md                                  |     1 +
 ale/drivers/dawn_drivers.py                   |   318 +-
 ale/formatters/formatter.py                   |     3 +
 ...rite_DawnVirIsisLabelNaifSpiceDriver.ipynb |   120 +
 .../DAWN_203_SCLKSCET.00091.tsc               |   673 +
 .../VIR_IR_1A_1_362681634_1_isis3.lbl         |   271 +
 .../VIR_IR_1A_1_362681634_1_isis3_0.xsp       |  1013 ++
 .../dawn_fc_v3_0_sliced_-203120.xc            |    31 +
 .../dawn_sc_110627_110703_0_sliced_-203000.xc | 14536 ++++++++++++++++
 .../data/VIR_IR_1A_1_362681634_1/dawn_v15.tf  |  2285 +++
 .../VIR_IR_1A_1_362681634_1/dawn_vesta_v00.tf |    93 +
 .../dawn_vesta_v06.tpc                        |   306 +
 .../VIR_IR_1A_1_362681634_1/dawn_vir_v05.ti   |   574 +
 .../dawn_vir_zero_0_sliced_-203201.xc         |    31 +
 .../dawnvirAddendum001.ti                     |    22 +
 .../data/VIR_IR_1A_1_362681634_1/naif0012.tls |   152 +
 .../data/VIR_IR_1A_1_362681634_1/pck00009.tpc |  3639 ++++
 tests/pytests/data/isds/dawnvir_isd.json      |  1972 +++
 tests/pytests/test_dawn_drivers.py            |   152 +-
 20 files changed, 26182 insertions(+), 12 deletions(-)
 create mode 100644 notebooks/write_DawnVirIsisLabelNaifSpiceDriver.ipynb
 create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/DAWN_203_SCLKSCET.00091.tsc
 create mode 100644 tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3.lbl
 create mode 100644 tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3_0.xsp
 create mode 100644 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_fc_v3_0_sliced_-203120.xc
 create mode 100644 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_sc_110627_110703_0_sliced_-203000.xc
 create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_v15.tf
 create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v00.tf
 create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v06.tpc
 create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_v05.ti
 create mode 100644 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_zero_0_sliced_-203201.xc
 create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/dawnvirAddendum001.ti
 create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/naif0012.tls
 create mode 100755 tests/pytests/data/VIR_IR_1A_1_362681634_1/pck00009.tpc
 create mode 100644 tests/pytests/data/isds/dawnvir_isd.json

diff --git a/.gitignore b/.gitignore
index a4e6eef..07b225e 100644
--- a/.gitignore
+++ b/.gitignore
@@ -13,6 +13,7 @@ __pycache__/
 # Distribution / packaging
 .Python
 build/
+docs/
 develop-eggs/
 dist/
 downloads/
@@ -222,3 +223,4 @@ dmypy.json
 *.CUB
 *.img
 *.IMG
+print.prt
diff --git a/CHANGELOG.md b/CHANGELOG.md
index 8e012f7..791e85e 100644
--- a/CHANGELOG.md
+++ b/CHANGELOG.md
@@ -40,6 +40,7 @@ release.
 ### Added
 - Mariner10 IsisLabelNaifSpice driver, tests, and test data [#547](https://github.com/DOI-USGS/ale/pull/547)
 - DawnFC IsisLabelNaifSpice driver, tests, and test data [#567](https://github.com/DOI-USGS/ale/pull/567)
+- DawnVIR IsisLabelNaifSpice driver, tests, and test data [#566](https://github.com/DOI-USGS/ale/pull/566)
 - Updated the spiceypy version used in environment.yml [#552]
 
 ### Fixed
diff --git a/ale/drivers/dawn_drivers.py b/ale/drivers/dawn_drivers.py
index ee9b043..0766700 100644
--- a/ale/drivers/dawn_drivers.py
+++ b/ale/drivers/dawn_drivers.py
@@ -1,22 +1,31 @@
-import pvl
+import re
 import spiceypy as spice
 import os
+import math
+import numpy as np
 
-from glob import glob
+from scipy.interpolate import CubicSpline
 
 import ale
 from ale.base import Driver
 from ale.base.label_isis import IsisLabel
 from ale.base.data_naif import NaifSpice
+from ale.base.data_isis import IsisSpice
 from ale.base.label_pds3 import Pds3Label
 from ale.base.type_distortion import NoDistortion
-from ale.base.type_sensor import Framer
+from ale.base.type_sensor import Framer, LineScanner
+from ale.base.data_isis import read_table_data
+from ale.base.data_isis import parse_table
+from ale.transformation import TimeDependentRotation
+from ale.transformation import ConstantRotation
 
 ID_LOOKUP = {
     "FC1" : "DAWN_FC1",
     "FC2" : "DAWN_FC2"
 }
 
+degs_per_rad = 57.2957795
+
 class DawnFcPds3NaifSpiceDriver(Framer, Pds3Label, NaifSpice, Driver):
     """
     Dawn driver for generating an ISD from a Dawn PDS3 image.
@@ -393,3 +402,306 @@ class DawnFcIsisLabelNaifSpiceDriver(Framer, IsisLabel, NaifSpice, NoDistortion,
           center ephemeris time
         """
         return self.ephemeris_start_time + (self.exposure_duration_ms / 2.0)
+    
+
+class DawnVirIsisLabelNaifSpiceDriver(LineScanner, IsisLabel, NaifSpice, NoDistortion, Driver):
+    @property
+    def instrument_id(self):
+        """
+        Returns the ID of the instrument
+
+        Returns
+        -------
+        : str
+          Name of the instrument
+        """
+        lookup_table = {'VIR': 'Visual and Infrared Spectrometer'}
+        return lookup_table[super().instrument_id]
+    
+    @property
+    def sensor_name(self):
+        """
+        Returns the name of the instrument
+
+        Returns
+        -------
+        : str
+          Name of the sensor
+        """
+        return self.label["IsisCube"]["Instrument"]["InstrumentId"]
+    
+    @property
+    def line_exposure_duration(self):
+      """
+      The exposure duration of the image, in seconds
+
+      Returns
+      -------
+      : float
+        Exposure duration in seconds
+      """
+      return self.label["IsisCube"]["Instrument"]["FrameParameter"][0]
+    
+    @property
+    def focal_length(self):
+      return float(spice.gdpool('INS{}_FOCAL_LENGTH'.format(self.ikid), 0, 1)[0])
+    
+    @property
+    def detector_center_sample(self):
+        """
+        Returns the center detector sample. Expects ikid to be defined. This should
+        be an integer containing the Naif Id code of the instrument.
+
+        Returns
+        -------
+        : float
+          Detector sample of the principal point
+        """
+        return super().detector_center_sample - 0.5
+
+    @property
+    def ikid(self):
+        """
+        Returns the Naif ID code for the instrument
+        Expects the instrument_id to be defined. This must be a string containing
+        the short name of the instrument.
+
+        Returns
+        -------
+        : int
+          Naif ID used to for identifying the instrument in Spice kernels
+        """
+        lookup_table = {
+          'VIS': -203211,
+          "IR": -203213
+        }
+        return lookup_table[self.label["IsisCube"]["Instrument"]["ChannelId"]]
+    
+    @property
+    def sensor_frame_id(self):
+        """
+        Returns the FRAME_DAWN_VIR_{VIS/IR}_ZERO Naif ID code if there are no associated articulation kernels. 
+        Otherwise the original Naif ID code is returned.
+        Returns
+        -------
+        : int
+          Naif ID code for the sensor frame
+        """
+        if self.has_articulation_kernel:
+          lookup_table = {
+            'VIS': -203211,
+            "IR": -203213
+         }
+        else:
+          lookup_table = {
+            'VIS': -203221,
+            "IR": -203223
+          }
+        return lookup_table[self.label["IsisCube"]["Instrument"]["ChannelId"]]
+    
+    @property
+    def housekeeping_table(self):
+        """
+        This table named, "VIRHouseKeeping", contains four fields: ScetTimeClock, ShutterStatus,
+        MirrorSin, and MirrorCos.  These fields contain the scan line time in SCLK, status of 
+        shutter - open, closed (dark), sine and cosine of the scan mirror, respectively.
+
+        Returns
+        -------
+        : dict
+          Dictionary with ScetTimeClock, ShutterStatus, MirrorSin, and MirrorCos
+        """
+        isis_bytes = read_table_data(self.label['Table'], self._file)
+        return parse_table(self.label['Table'], isis_bytes)
+    
+    @property
+    def line_scan_rate(self):
+        """
+        Returns
+        -------
+        : list
+          Start lines
+        : list
+          Line times
+        : list
+          Exposure durations
+        """
+        line_times = []
+        start_lines = []
+        exposure_durations = []
+
+        line_no = 0.5
+
+        for line_midtime in self.hk_ephemeris_time:
+          if not self.is_calibrated:
+            line_times.append(line_midtime - (self.line_exposure_duration / 2.0) - self.center_ephemeris_time)
+            start_lines.append(line_no)
+            exposure_durations.append(self.label["IsisCube"]["Instrument"]["FrameParameter"][2])
+            line_no += 1
+
+        line_times.append(line_times[-1] + self.label["IsisCube"]["Instrument"]["FrameParameter"][2])
+        start_lines.append(line_no)
+        exposure_durations.append(self.label["IsisCube"]["Instrument"]["FrameParameter"][2])
+
+        return start_lines, line_times, exposure_durations
+
+    @property
+    def sensor_model_version(self):
+        """
+        Returns
+        -------
+        : int
+          ISIS sensor model version
+        """
+        return 1
+    
+    @property
+    def optical_angles(self):
+        hk_dict = self.housekeeping_table
+        
+        opt_angles = []
+        x = np.array([])
+        y = np.array([])
+        for index, mirror_sin in enumerate(hk_dict["MirrorSin"]):
+            shutter_status = hk_dict["ShutterStatus"][index].lower().replace(" ", "")
+            is_dark = (shutter_status == "closed")   
+
+            mirror_cos = hk_dict["MirrorCos"][index]
+
+            scan_elec_deg = math.atan(mirror_sin/mirror_cos) * degs_per_rad
+            opt_ang = ((scan_elec_deg - 3.7996979) * 0.25/0.257812) / 1000
+
+            if not is_dark:
+                x = np.append(x, index + 1)
+                y = np.append(y, opt_ang)
+
+            if not self.is_calibrated:
+                opt_angles.append(opt_ang)
+
+        cs = CubicSpline(x, y, extrapolate="periodic")
+
+        for i, opt_ang in enumerate(opt_angles):
+          shutter_status = hk_dict["ShutterStatus"][i].lower().replace(" ", "")
+          is_dark = (shutter_status == "closed")
+
+          if (is_dark):
+            if (i == 0):
+              opt_angles[i] = opt_angles[i+1]
+            elif (i == len(opt_angles) - 1):
+              opt_angles[i] = opt_angles[i-1]
+            else:
+              opt_angles[i] = cs(i+1)
+
+        return opt_angles
+    
+    @property
+    def hk_ephemeris_time(self):
+
+        line_times = []
+        scet_times = self.housekeeping_table["ScetTimeClock"]
+        for scet in scet_times:
+          line_midtime = spice.scs2e(self.spacecraft_id, scet)
+          line_times.append(line_midtime)
+
+        return line_times
+    
+    @property
+    def ephemeris_start_time(self):
+        """
+        Returns the starting ephemeris time of the image using the first et time from
+        the housekeeping table minus the line exposure duration / 2. 
+
+        Returns
+        -------
+        : double
+          Starting ephemeris time of the image
+        """
+        return self.hk_ephemeris_time[0] - (self.line_exposure_duration / 2)
+
+
+    @property
+    def ephemeris_stop_time(self):
+        """
+        Returns the ephemeris stop time of the image using the last et time from
+        the housekeeping table plus the line exposure duration / 2. 
+
+        Returns
+        -------
+        : double
+          Ephemeris stop time of the image
+        """
+        return self.hk_ephemeris_time[-1] + (self.line_exposure_duration / 2)
+
+    @property
+    def center_ephemeris_time(self):
+      return self.hk_ephemeris_time[int(len(self.hk_ephemeris_time)/2)]
+    
+    @property
+    def is_calibrated(self):
+        """
+        Checks if image is calibrated.
+
+        Returns
+        -------
+        : bool
+        """
+        return self.label['IsisCube']['Archive']['ProcessingLevelId'] > 2
+
+    @property 
+    def has_articulation_kernel(self):
+        """
+        Checks if articulation kernel exists in pool of kernels.
+
+        Returns
+        -------
+        : bool
+        """
+        try:
+          regex = re.compile('.*dawn_vir_[0-9]{9}_[0-9]{1}.BC')
+          return any([re.match(regex, i) for i in self.kernels])
+        except ValueError:
+          return False
+
+    @property
+    def frame_chain(self):
+      frame_chain = super().frame_chain
+      frame_chain.add_edge(rotation=self.inst_pointing_rotation)
+      return frame_chain
+    
+    @property
+    def inst_pointing_rotation(self):
+        """
+        Returns a time dependent instrument pointing rotation for -203221 and -203223 sensor frame ids.
+
+        Returns
+        -------
+        : TimeDependentRotation
+          Instrument pointing rotation
+        """
+        time_dep_quats = np.zeros((len(self.hk_ephemeris_time), 4))
+        avs = []
+
+        for i, time in enumerate(self.hk_ephemeris_time):
+          try:
+            state_matrix = spice.sxform("J2000", spice.frmnam(self.sensor_frame_id), time)
+          except:
+            rotation_matrix = spice.pxform("J2000", spice.frmnam(self.sensor_frame_id), time)
+            state_matrix = spice.rav2xf(rotation_matrix, [0, 0, 0])
+
+          opt_angle = self.optical_angles[i]
+          
+          xform = spice.eul2xf([0, -opt_angle, 0, 0, 0, 0], 1, 2, 3)
+          xform2 = spice.mxmg(xform, state_matrix)
+
+          rot_mat, av = spice.xf2rav(xform2)
+          avs.append(av)
+
+          quat_from_rotation = spice.m2q(rot_mat)
+          time_dep_quats[i,:3] = quat_from_rotation[1:]
+          time_dep_quats[i, 3] = quat_from_rotation[0]
+
+        time_dep_rot = TimeDependentRotation(time_dep_quats, self.hk_ephemeris_time, 1, self.sensor_frame_id, av=avs)
+
+        return time_dep_rot
+
+    
\ No newline at end of file
diff --git a/ale/formatters/formatter.py b/ale/formatters/formatter.py
index afeb2f9..751afc6 100644
--- a/ale/formatters/formatter.py
+++ b/ale/formatters/formatter.py
@@ -2,6 +2,8 @@ import json
 import numpy as np
 from scipy.interpolate import interp1d, BPoly
 
+import spiceypy as spice
+
 from networkx.algorithms.shortest_paths.generic import shortest_path
 
 from ale.transformation import FrameChain
@@ -140,6 +142,7 @@ def to_isd(driver):
     instrument_pointing['constant_frames'] = shortest_path(frame_chain, sensor_frame, destination_frame)
     constant_rotation = frame_chain.compute_rotation(destination_frame, sensor_frame)
     instrument_pointing['constant_rotation'] = constant_rotation.rotation_matrix().flatten()
+    
     meta_data['instrument_pointing'] = instrument_pointing
 
     # interior orientation
diff --git a/notebooks/write_DawnVirIsisLabelNaifSpiceDriver.ipynb b/notebooks/write_DawnVirIsisLabelNaifSpiceDriver.ipynb
new file mode 100644
index 0000000..9f0e500
--- /dev/null
+++ b/notebooks/write_DawnVirIsisLabelNaifSpiceDriver.ipynb
@@ -0,0 +1,120 @@
+{
+ "cells": [
+  {
+   "cell_type": "code",
+   "execution_count": null,
+   "metadata": {},
+   "outputs": [],
+   "source": [
+    "fileName = 'VIR_IR_1A_1_362681634_1_isis3.cub'\n",
+    "\n",
+    "import os\n",
+    "os.environ[\"ISISDATA\"] = \"isisdata/isis_data\"\"\n",
+    "os.environ[\"ISISTESTDATA\"] = \"/isisdata/isis_testData\"\n",
+    "os.environ[\"ISISROOT\"] = \"/ISIS3/build\"\n",
+    "\n",
+    "import ale \n",
+    "from ale.drivers.dawn_drivers import DawnVirIsisNaifSpiceDriver\n",
+    "from ale.formatters.formatter import to_isd\n",
+    "import spiceypy as spice\n",
+    "from ale.drivers import AleJsonEncoder"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": null,
+   "metadata": {},
+   "outputs": [],
+   "source": [
+    "from ale.util import generate_kernels_from_cube\n",
+    "kernels = generate_kernels_from_cube(fileName, expand=True, format_as='list')\n"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": null,
+   "metadata": {},
+   "outputs": [],
+   "source": [
+    "kernels"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": null,
+   "metadata": {
+    "scrolled": false
+   },
+   "outputs": [],
+   "source": [
+    "with DawnVirIsisNaifSpiceDriver(fileName, props = {\"kernels\": kernels}) as driver:\n",
+    "    isisString = to_isd(driver)"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": null,
+   "metadata": {},
+   "outputs": [],
+   "source": [
+    "isisString"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": null,
+   "metadata": {},
+   "outputs": [],
+   "source": [
+    "import json\n",
+    "\n",
+    "isis_dict = isisString\n",
+    "\n",
+    "json_file = os.path.splitext(fileName)[0] + '.json'\n",
+    "\n",
+    "with open(json_file, 'w') as fp:\n",
+    "    json.dump(isis_dict, fp, cls = AleJsonEncoder)\n",
+    "    \n",
+    "with open(json_file, 'r') as fp:\n",
+    "    isis_dict = json.load(fp)\n",
+    "    \n",
+    "isis_dict.keys()"
+   ]
+  },
+  {
+   "cell_type": "code",
+   "execution_count": null,
+   "metadata": {},
+   "outputs": [],
+   "source": []
+  },
+  {
+   "cell_type": "code",
+   "execution_count": null,
+   "metadata": {},
+   "outputs": [],
+   "source": []
+  }
+ ],
+ "metadata": {
+  "kernelspec": {
+   "display_name": "Python 3 (ipykernel)",
+   "language": "python",
+   "name": "python3"
+  },
+  "language_info": {
+   "codemirror_mode": {
+    "name": "ipython",
+    "version": 3
+   },
+   "file_extension": ".py",
+   "mimetype": "text/x-python",
+   "name": "python",
+   "nbconvert_exporter": "python",
+   "pygments_lexer": "ipython3",
+   "version": "3.10.2"
+  }
+ },
+ "nbformat": 4,
+ "nbformat_minor": 2
+}
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/DAWN_203_SCLKSCET.00091.tsc b/tests/pytests/data/VIR_IR_1A_1_362681634_1/DAWN_203_SCLKSCET.00091.tsc
new file mode 100755
index 0000000..b0afa1e
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/DAWN_203_SCLKSCET.00091.tsc
@@ -0,0 +1,673 @@
+KPL/SCLK
+
+
+DAWN SCLK File
+===========================================================================
+
+     This file is a SPICE spacecraft clock (SCLK) kernel containing
+     information required for DAWN spacecraft on-board clock to UTC
+     conversion.
+
+
+Production/History of this SCLK file
+--------------------------------------------------------
+
+     This file was generated by the NAIF utility program MAKCLK, version
+     3.5.2, from the most recent DAWN spacecraft SCLKvSCET file (see
+     corresponding sections of these comments for a copy of the source
+     SCLKvSCET file and MAKCLK setup file).
+
+
+Usage
+--------------------------------------------------------
+
+     This file must be loaded into the user's program by a call to the
+     FURNSH subroutine
+
+          CALL FURNSH( 'this_file_name' )
+
+     in order to use the SPICELIB SCLK family of subroutines to convert
+     DAWN 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:
+
+          SSSSSSSSSS:FFF
+
+     where:
+
+          SSSSSSSSSS -- count of on-board seconds
+
+          FFF        -- count of fractions of a second with one fraction
+                        being 1/256 of a second; normally this field value
+                        is within 0..255 range.
+
+
+References
+--------------------------------------------------------
+
+         1.   SCLK Required Reading Document
+
+         2.   MAKCLK User's Guide Document
+
+         3.   SFOC SCLKvSCET SIS Document
+
+
+Inquiries
+--------------------------------------------------------
+
+     If you have any questions regarding this file contact NAIF  at JPL
+
+           Charles H. Acton, Jr
+           (818) 354-3869
+           Chuck.Acton@jpl.nasa.gov
+
+           Boris V. Semenov
+           (818) 354-8136
+           Boris.Semenov@jpl.nasa.gov
+
+
+Source SCLKvSCET File
+--------------------------------------------------------
+
+     CCSD3ZS00001$$sclk$$NJPL3KS0L015$$scet$$
+     MISSION_NAME=DAWN;
+     SPACECRAFT_NAME=DAWN;
+     DATA_SET_ID=SCLK_SCET;
+     FILE_NAME=DAWN_203_SCLKSCET.00091;
+     PRODUCT_CREATION_TIME=2018-270T19:25:38.266;
+     PRODUCT_VERSION_ID=00091;
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+       570468916.000    2018-029T03:34:06.818 69.184  1.000000031
+       571815371.000    2018-044T17:35:01.860 69.184  0.999998116
+       571816371.000    2018-044T17:51:41.858 69.184  1.000000035
+       577218094.000    2018-107T06:20:25.047 69.184  1.000000875
+       577219094.000    2018-107T06:37:05.048 69.184  1.000000136
+       579212589.000    2018-130T08:22:00.319 69.184  0.999999670
+       579213589.000    2018-130T08:38:40.319 69.184  1.000000107
+       579582887.000    2018-134T15:13:38.359 69.184  1.000007697
+       579583887.000    2018-134T15:30:18.366 69.184  1.000000037
+       581075680.000    2018-151T21:53:31.421 69.184  1.000016584
+       581076680.000    2018-151T22:10:11.438 69.184  1.000000069
+       581548472.000    2018-157T09:13:23.471 69.184  1.000013882
+       581549472.000    2018-157T09:30:03.484 69.184  1.000000039
+       587129196.000    2018-221T23:25:27.702 69.184  1.000002286
+       587130196.000    2018-221T23:42:07.704 69.184  1.000000037
+     CCSD3RE00000$$data$$CCSD3RE00000$$sclk$$
+     
+
+
+MAKCLK Setup file
+--------------------------------------------------------
+
+     SCLKSCET_FILE          = DAWN_203_SCLKSCET.00091.clean
+     OLD_SCLK_KERNEL        = /sdma/naif/ops/projects/DAWN/scet/bin/dawn_template.tsc
+     FILE_NAME              = DAWN_203_SCLKSCET.00091.tsc
+     NAIF_SPACECRAFT_ID     = -203
+     LEAPSECONDS_FILE       = /sdma/naif/ops/projects/DAWN/lsk/dawn.tls
+     PARTITION_TOLERANCE    = 10
+     LOG_FILE               = DAWN_203_SCLKSCET.00091.log
+     
+
+
+Kernel DATA
+--------------------------------------------------------
+
+\begindata
+
+
+SCLK_KERNEL_ID           = ( @2018-09-28/01:15:03.00 )
+
+SCLK_DATA_TYPE_203        = ( 1 )
+SCLK01_TIME_SYSTEM_203    = ( 2 )
+SCLK01_N_FIELDS_203       = ( 2 )
+SCLK01_MODULI_203         = ( 4294967296 256 )
+SCLK01_OFFSETS_203        = ( 0 0 )
+SCLK01_OUTPUT_DELIM_203   = ( 1 )
+
+SCLK_PARTITION_START_203  = ( 0.0000000000000E+00 )
+
+SCLK_PARTITION_END_203    = ( 1.0995116277750E+12 )
+
+SCLK01_COEFFICIENTS_203   = (
+ 
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+    6.2601984000000E+10     2.4453900610200E+08     1.0000071403510E+00
+    6.2645760000000E+10     2.4471000732300E+08     1.0000110000074E+00
+    6.2646016000000E+10     2.4471100733400E+08     1.0000071522418E+00
+    6.2848461056000E+10     2.4550181399000E+08     1.0000329999924E+00
+    6.2848717056000E+10     2.4550281402300E+08     9.9899907834244E-01
+    6.2851494656000E+10     2.4551365316300E+08     9.9901600000262E-01
+    6.2851750656000E+10     2.4551465217900E+08     1.0000000010087E+00
+    6.3866880000000E+10     2.4948000118300E+08     9.9915799999237E-01
+    6.3867136000000E+10     2.4948100034100E+08     1.0000000889535E+00
+    6.4307456000000E+10     2.5120100049400E+08     9.9990999999642E-01
+    6.4307712000000E+10     2.5120200040400E+08     1.0000000459588E+00
+    6.4953856000000E+10     2.5372600052000E+08     1.0001089999974E+00
+    6.4954112000000E+10     2.5372700062900E+08     1.0000000890295E+00
+    6.5560832000000E+10     2.5609700084000E+08     1.0000499999821E+00
+    6.5561088000000E+10     2.5609800089000E+08     1.0000001131272E+00
+    6.5789644800000E+10     2.5699080099100E+08     9.9986400002241E-01
+    6.5789900800000E+10     2.5699180085500E+08     9.9904588236528E-01
+    6.5790118400000E+10     2.5699265004400E+08     9.9875999987125E-01
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+    1.5030533017600E+11     5.8713019688800E+08     1.0000000370000E+00 )
+
+\begintext
+
+
+
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3.lbl b/tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3.lbl
new file mode 100644
index 0000000..b1abddd
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3.lbl
@@ -0,0 +1,271 @@
+Object = IsisCube
+  Object = Core
+    StartByte   = 65537
+    Format      = Tile
+    TileSamples = 256
+    TileLines   = 60
+
+    Group = Dimensions
+      Samples = 256
+      Lines   = 60
+      Bands   = 432
+    End_Group
+
+    Group = Pixels
+      Type       = SignedWord
+      ByteOrder  = Lsb
+      Base       = 0.0
+      Multiplier = 1.0
+    End_Group
+  End_Object
+
+  Group = Instrument
+    SpacecraftName               = DAWN
+    MissionPhaseName             = "VESTA SCIENCE APPROACH (VSA)"
+    InstrumentId                 = VIR
+    SpacecraftClockStartCount    = 1/362681634.2933
+    SpacecraftClockStopCount     = 1/362682578.0394
+    StartTime                    = 2011-06-30T05:53:54.29
+    StopTime                     = 2011-06-30T06:09:38.04
+    TargetName                   = VESTA
+    OriginalTargetName           = "4 VESTA"
+    OrbitNumber                  = N/A
+    DataQualityId                = 1
+    ChannelId                    = IR
+    InstrumentModeId             = S_H_SPE_H_SPA_F
+    ScanModeId                   = 4
+    FrameParameter               = (0.5, 1, 16, 58)
+    VirIrStartXPosition          = 1
+    VirIrStartYPosition          = 7
+    MaximumInstrumentTemperature = (81.5, 139.6, 140.6, 74.4)
+  End_Group
+
+  Group = Archive
+    SoftwareVersionId         = "EGSE V1.14,AMDLSpace"
+    DataSetName               = "DAWN VIR RAW (EDR) VESTA INFRARED SPECTRA
+                                 V1.0"
+    DataSetId                 = DAWN-A-VIR-2-EDR-IR-VESTA-SPECTRA-V1.0
+    ProductId                 = VIR_IR_1A_1_362681634_1
+    ProductType               = EDR
+    ProducerFullName          = "A. CORADINI"
+    ProducerInstitutionName   = "ISTITUTO NAZIONALE DI ASTROFISICA"
+    ProductCreationTime       = 2011-07-01T11:21:40.95
+    ProductVersionId          = 01
+    InstrumentName            = "VISIBLE AND INFRARED SPECTROMETER"
+    InstrumentType            = "IMAGING SPECTROMETER"
+    ImageMidTime              = NULL
+    ProcessingLevelId         = 2
+    EncodingType              = N/A
+    PhotometricCorrectionType = NONE
+  End_Group
+
+  Group = BandBin
+    Unit         = MICROMETER
+    Center       = (1.021, 1.030, 1.040, 1.049, 1.059, 1.068, 1.078, 1.087,
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diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3_0.xsp b/tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3_0.xsp
new file mode 100644
index 0000000..80d0cdb
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/VIR_IR_1A_1_362681634_1_isis3_0.xsp
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+'159E18336E19FD^8'
+'159E1C33B1B7A3^8'
+'C^1'
+END_ARRAY 2 865
+BEGIN_ARRAY 3 39
+'DE-0421LE-0421                          '
+'159E106596D27^8'
+'159E194B5DFD66^8'
+'A'
+'0'
+'1'
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+'B313A0D099DEB8^-5'
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+'-5EC97B9EA6E2F4^-5'
+'1455A78ABB1748^-6'
+'158B5B4^8'
+'1518^6'
+'23^2'
+'1^1'
+END_ARRAY 3 39
+TOTAL_ARRAYS 3
+ ~NAIF/SPC BEGIN COMMENTS~
+; /Users/astamile/testData/ale/dawnVIR/VIR_IR_1A_1_362681634_1_isis3_0.bsp LOG FILE
+
+; Created 2023-12-10/09:42:34.00.
+;
+; BEGIN SPKMERGE COMMANDS
+
+LEAPSECONDS_KERNEL = /Users/astamile/isisdata/isis_data/base/kernels/lsk/naif0012.tls
+
+SPK_KERNEL = /Users/astamile/testData/ale/dawnVIR/VIR_IR_1A_1_362681634_1_isis3_0.bsp
+SOURCE_SPK_KERNEL = /Users/astamile/isisdata/isis_data/dawn/kernels/tspk/sb_vesta_110211.bsp
+    INCLUDE_COMMENTS = NO
+    BODIES           = 2000004
+    BEGIN_TIME       = 2011 JUN 30 04:32:35.405
+    END_TIME         = 2011 JUN 30 05:10:33.183
+SOURCE_SPK_KERNEL = /Users/astamile/isisdata/isis_data/dawn/kernels/spk/dawn_rec_110416-110802_110913_v1.bsp
+    INCLUDE_COMMENTS = NO
+    BODIES           = -203
+    BEGIN_TIME       = 2011 JUN 30 04:32:35.405
+    END_TIME         = 2011 JUN 30 05:10:33.183
+SOURCE_SPK_KERNEL = /Users/astamile/isisdata/isis_data/dawn/kernels/tspk/de421.bsp
+    INCLUDE_COMMENTS = NO
+    BODIES           = 10
+    BEGIN_TIME       = 2011 JUN 30 04:32:35.405
+    END_TIME         = 2011 JUN 30 05:10:33.183
+
+; END SPKMERGE COMMANDS
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_fc_v3_0_sliced_-203120.xc b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_fc_v3_0_sliced_-203120.xc
new file mode 100644
index 0000000..919a7a7
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_fc_v3_0_sliced_-203120.xc
@@ -0,0 +1,31 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK  '
+'2'
+'6'
+'DAWN FC ALIGNMENT                                           '
+BEGIN_ARRAY 1 10
+'DAWN FC2 ALIGNMENT, 10/22/15            '
+'159E1065C3^A'
+'159E194B8A^A'
+'-31970'
+'-318F8'
+'2'
+'1'
+10
+'FFFFE61784D86^0'
+'-1CE1654009A4C1^-2'
+'681F4D63A264F8^-2'
+'27DE1942838A74^-2'
+'0^0'
+'0^0'
+'0^0'
+'FFFFFFFF1C422^-2'
+'159E1065C3^A'
+'159E194B8A^A'
+END_ARRAY 1 10
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /Users/astamile/testData/ale/dawnVIR/VIR_IR_1A_1_362681634_1_isis3.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_sc_110627_110703_0_sliced_-203000.xc b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_sc_110627_110703_0_sliced_-203000.xc
new file mode 100644
index 0000000..6243766
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_sc_110627_110703_0_sliced_-203000.xc
@@ -0,0 +1,14536 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK  '
+'2'
+'6'
+'DAWN TLM-Based SC Bus CK File by NAIF/JPL                   '
+BEGIN_ARRAY 1 14501
+'DAWN SC BUS TLM-BASED QUATS/AVS         '
+'159E1065C3^A'
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+'159E18DDD7^A'
+'159E1941D7^A'
+'159E1065C3^A'
+'1^1'
+'712^3'
+END_ARRAY 1 14501
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /Users/astamile/testData/ale/dawnVIR/VIR_IR_1A_1_362681634_1_isis3.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_v15.tf b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_v15.tf
new file mode 100755
index 0000000..73f2a79
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_v15.tf
@@ -0,0 +1,2285 @@
+KPL/FK
+
+Dawn Frames Kernel
+========================================================================
+
+   This frame kernel contains complete set of frame definitions for the
+   Dawn Spacecraft (DAWN) including definitions for the Dawn spacecraft
+   and Dawn science instrument and engineering structure frames. This
+   kernel also contains NAIF ID/name mapping for the Dawn instruments.
+
+
+Version and Date
+========================================================================
+
+
+   Version 1.5 -- October 19, 2018 -- Boris Semenov, NAIF
+
+      Added more DSK surface name-IDs.
+
+   Version 1.4 -- March 29, 2018 -- Boris Semenov, NAIF
+
+      Added DSK surface name-ID mapping section.
+
+   Version 1.3 -- April 6, 2016 -- Boris Semenov, NAIF
+
+      Redefined the DAWN_FC2 frame as a CK-based frame to facilitate
+      providing different FC2 alignments relative to the s/c frame for
+      Vesta and Ceres missions.
+
+   Version 1.2 -- October 29, 2012 -- Boris Semenov, NAIF
+
+      Added Euler dynamic frames for Vesta coordinate systems
+      ``IAU-2000'' and ``DAWN-Claudia''.
+
+   Version 1.1 -- July 5, 2011 -- Boris Semenov, NAIF
+
+      Corrected description of the FC1 and FC2 frames. All frame 
+      definitions are identical to Version 1.0.
+
+   Version 1.0 -- March 21, 2011 -- Boris Semenov, NAIF
+
+      Incorporated updated definitions of the DAWN_VIR_VIS, DAWN_VIR_IR, 
+      DAWN_VIR_VIS_ZERO, and DAWN_VIR_IR_ZERO frames provided by 
+      by Dr. Federico Tosi, INAF in "dawn_v10_draft3.tf"
+
+      Changed IDs of DAWN_VIR_VIS_ZERO and DAWN_VIR_IR_ZERO frames from
+      -203212 and -203214 to -203221 and -203223 to eliminate confusion
+      that may result from the IDs -203212 and -203214 mapping to
+      different names in the frames and physical objects domains. Since
+      these frames are fixed-offset, class 4 frames that are referred to
+      only by name in SPICE API calls and other kernels (e.g. IKs) this
+      change should be transparent to the users of this FK.
+
+      Updated star tracker alignments (frames DAWN_ST1 and DAWN_ST2)
+      and FC alignments (frames DAWN_FC1 and DAWN_FC2) per MCR-111570.
+
+   Version 0.9 -- July 1, 2010 -- Boris Semenov, NAIF
+
+      Incorporated updated definitions of the DAWN_VIR_VIS, DAWN_VIR_IR, 
+      DAWN_VIR_VIS_ZERO, and DAWN_VIR_IR_ZERO frames provided by 
+      Eleonora Ammannito, INAF in "VIR_kernel_update_r2.doc".
+
+   Version 0.8 -- October 8, 2009 -- Dr. Federico Tosi, INAF - IFSI
+                                     Boris Semenov, NAIF
+
+      Redefined VIR frames to better encapsulate the instrument scan
+      mirror motion and optical path misalignments, specifically:
+
+         -  added DAWN_VIR frame (-203200), fixed to the spacecraft, to
+            capture the instrument base alignment relative to the spacecraft
+
+         -  added DAWN_VIR_SCAN frame (-203201), CK-based, to capture
+            the motion of the mirror
+
+         -  changed the reference frame for DAWN_VIR_VIS and
+            DAWN_VIR_IR to DAWN_VIR_SCAN
+
+         -  renamed DAWN_VIR_VIS_SCAN and DAWN_VIR_IR_SCAN to
+            DAWN_VIR_VIS_ZERO and DAWN_VIR_IR_ZERO while keeping the
+            same IDs (-203212 and -203214) and redefined them to be
+            fixed offset frames relative to DAWN_VIR
+
+         -  added DAWN_VIR/-203200 and DAWN_VIR_SCAN/-203201 name/ID
+            mappings
+
+   Version 0.7 -- July 3, 2009 -- Boris Semenov, NAIF
+
+      Incorporated Thomas Roatsch's name/ID mappings and individual
+      frames for FC filters. Included FC alignments used by DLR to
+      process MGA data in the comments.
+
+      Corrected and completed comments in the "Dawn Mission
+      NAIF ID Codes -- Summary Section" section.
+
+      Re-worded some of the version section entries for clarity.
+
+   Version 0.6t2 -- June 23, 2009 -- Steven Joy, DSC
+
+      Propagated test version of the DAWN_VIR_VIS_96/-203218 and
+      DAWN_VIR_VIS_32/-203219 name/ID mapping. Neither this nor the
+      previous updates have still been reviewed by the VIR team.
+
+   Version 0.6t -- April 09, 2009 -- Steven Joy, DSC
+
+      Propagated test version of the DAWN_VIR_VIS_16/-203217 name/ID
+      mapping. Neither this nor the previous updates have still been
+      reviewed by the VIR team.
+
+   Version 0.6t -- Jan 12, 2009 -- Steven Joy, DSC
+
+      Propagated test version of the DAWN_VIR_VIS_124/-203215 and
+      DAWN_VIR_VIS_64/-203216 name/ID mappings from version 0.5t into
+      the version 0.6 released by Boris. These updates have still not
+      been reviewed by the VIR team.
+
+   Version 0.6 -- January 5, 2009 -- Boris Semenov, NAIF
+
+      Preliminary Version. Pending review and approval by Dawn
+      instrument teams.
+
+      Incorporated FC alignments provided by Nick Mastrodemos.
+
+   Version 0.5t -- June 23, 2008 -- Steven Joy, DSC with Boris Semenov, NAIF
+
+      Preliminary Version. Pending review and approval by Dawn
+      instrument teams.
+
+      Added definitions for name/ID mappings DAWN_VIR_VIS_124/-203215
+      and DAWN_VIR_VIS_64/-203216. These IDs are needed to define
+      special FOV for the VIR scan mirror of 128 (64) positions, half
+      on either side of the mirror center position.
+
+      Updated HGA frame orientation based on [7].
+
+
+   Version 0.5 -- January 10, 2008 -- Boris Semenov, NAIF
+
+      Preliminary Version. Pending review and approval by Dawn
+      instrument teams.
+
+      Updated HGA frame orientation based on [7].
+
+   Version 0.4 -- May 8, 2007 -- Boris Semenov, NAIF
+
+      Preliminary Version. Pending review and approval by Dawn
+      instrument teams.
+
+      Added ID/name mappings for the solar array corners.
+
+   Version 0.3 -- August 7, 2006 -- Boris Semenov, NAIF
+
+      Preliminary Version. Pending review and approval by Dawn
+      instrument teams.
+
+      Added star tracker (ST1 and ST2) and flight thruster (FT1, FT2,
+      and FT3) frames and name/ID mappings. In this version all STn and
+      FTn frames provide on nominal alignment.
+
+   Version 0.2 -- July 27, 2006 -- Boris Semenov, NAIF
+
+      Preliminary Version. Pending review and approval by Dawn
+      instrument teams.
+
+      Renamed DAWN_LGA frame and structure name to be DAWN_LGA+Z. Added
+      DAWN_LGA+X and DAWN_LGA-Z frames and structure name/IDs.
+
+   Version 0.1 -- May 9, 2005 -- Boris Semenov, NAIF
+
+      Preliminary Version. Pending review and approval by Dawn
+      instrument teams.
+
+      Added FC and VIR radiator name-ID mapping keywords. Removed
+      definitions of VESTA_FIXED and CERES_FIXED frames; these frames
+      are now defined in separate FKs (per request from SOA).
+
+   Version 0.0 -- October 11, 2004 -- Boris Semenov, NAIF
+
+      Preliminary Version. Pending review and approval by Dawn
+      instrument teams.
+
+
+References
+========================================================================
+
+   1. ``Frames Required Reading''
+
+   2. ``Kernel Pool Required Reading''
+
+   3. ``C-Kernel Required Reading''
+
+   4. Dawn CDR Presentations.
+
+   5. Dawn Instrument ICD/MICD documents.
+
+   6. DAWN FSDD, CDRL TD-006, 9/27/04
+
+   7. HGA Boresight Direction, e-mail from Ed Swenka, 01/10/08
+
+   8. "Post-Processing Of Framing Camera Alignments"
+      (FCalignment_110118.docx), Ian Roundhill, January 18, 2011
+
+   9. "Star Tracker and IRU In-Flight Calibration Test Report.
+      DN-DAWN-ACS-026" (DN-DAWN-ACS-026_01.pdf), A. Cross, 01/15/08
+
+
+Contact Information
+========================================================================
+
+   Boris V. Semenov, NAIF/JPL, (818)-354-8136, boris.semenov@jpl.nasa.gov
+
+
+Implementation Notes
+========================================================================
+
+   This file is used by the SPICE system as follows: programs that make
+   use of this frame kernel must ``load'' the kernel, normally during
+   program initialization. The SPICE routine FURNSH loads a kernel file
+   into the pool as shown below.
+
+      CALL FURNSH ( 'frame_kernel_name; )    -- FORTRAN
+      furnsh_c ( "frame_kernel_name" );      -- C
+      cspice_furnsh, frame_kernel_name       -- IDL
+      cspice_furnsh( 'frame_kernel_name' )   -- MATLAB
+
+   This file was created and may be updated with a text editor or word
+   processor.
+
+
+Dawn Mission NAIF ID Codes -- Summary Section
+========================================================================
+
+   The following names and NAIF ID codes are assigned to the Dawn
+   spacecraft, its structures and science instruments (the keywords
+   implementing these definitions are located in the section "Dawn
+   Mission NAIF ID Codes -- Definition Section" at the end of this
+   file):
+
+   Dawn Targets:
+
+            VESTA                   2000004 (synonyms: '4 VESTA')
+            CERES                   2000001 (synonyms: '1 CERES')
+
+   Dawn Spacecraft and Spacecraft Structures names/IDs:
+
+            DAWN                   -203
+            DAWN_SPACECRAFT        -203000
+            DAWN_SA+Y              -203010
+            DAWN_SA+Y_GIMBAL       -203011
+            DAWN_SA+Y_C1           -203012
+            DAWN_SA+Y_C2           -203013
+            DAWN_SA+Y_C3           -203014
+            DAWN_SA+Y_C4           -203015
+            DAWN_SA-Y              -203020
+            DAWN_SA-Y_GIMBAL       -203021
+            DAWN_SA-Y_C1           -203022
+            DAWN_SA-Y_C2           -203023
+            DAWN_SA-Y_C3           -203024
+            DAWN_SA-Y_C4           -203025
+            DAWN_HGA               -203040
+            DAWN_LGA+Z             -203030
+            DAWN_LGA+X             -203050
+            DAWN_LGA-Z             -203060
+            DAWN_ST1               -203071
+            DAWN_ST2               -203072
+            DAWN_FT1               -203081
+            DAWN_FT2               -203082
+            DAWN_FT3               -203083
+
+   FC1 and FC2 names/IDs:
+
+            DAWN_FC1               -203110
+            DAWN_FC1_FILTER_1      -203111
+            DAWN_FC1_FILTER_2      -203112
+            DAWN_FC1_FILTER_3      -203113
+            DAWN_FC1_FILTER_4      -203114
+            DAWN_FC1_FILTER_5      -203115
+            DAWN_FC1_FILTER_6      -203116
+            DAWN_FC1_FILTER_7      -203117
+            DAWN_FC1_FILTER_8      -203118
+            DAWN_FC1_RAD           -203119
+
+            DAWN_FC2               -203120
+            DAWN_FC2_FILTER_1      -203121
+            DAWN_FC2_FILTER_2      -203122
+            DAWN_FC2_FILTER_3      -203123
+            DAWN_FC2_FILTER_4      -203124
+            DAWN_FC2_FILTER_5      -203125
+            DAWN_FC2_FILTER_6      -203126
+            DAWN_FC2_FILTER_7      -203127
+            DAWN_FC2_FILTER_8      -203128
+            DAWN_FC2_RAD           -203129
+
+   VIR names/IDs:
+
+            DAWN_VIR               -203200
+            DAWN_VIR_SCAN          -203201
+            DAWN_VIR_VIS           -203211
+            DAWN_VIR_IR            -203213
+            DAWN_VIR_VIS_SCAN      -203212
+            DAWN_VIR_IR_SCAN       -203214
+            DAWN_VIR_VIS_128       -203215
+            DAWN_VIR_VIS_64        -203216
+            DAWN_VIR_VIS_16        -203217
+            DAWN_VIR_VIS_96        -203218
+            DAWN_VIR_VIS_32        -203219
+            DAWN_VIR_RAD           -203209
+
+   GRAND names/IDs:
+
+            DAWN_GRAND             -203300
+
+
+   Vesta and Ceres DSK Surface names/IDs:
+
+      See "Dawn DSK Surface NAIF Names/ID Codes -- Definition Section"
+      section at the end the file.
+
+
+Dawn Frames
+========================================================================
+
+   The following Dawn frames are defined in this kernel file:
+
+           Name                  Relative to           Type       NAIF ID
+      ======================  ===================  ============   =======
+
+   Dawn Target frames:
+   ----------------------------------------------------
+      IAU_VESTA               J2000                PCK            10099   (1)
+      VESTA_FIXED             J2000                PCK            2000004 (2)
+      VESTA_IAU_2000          J2000                DYNAMIC        -203911
+      DAWN_CLAUDIA            J2000                DYNAMIC        -203912
+
+      CERES_FIXED             J2000                PCK            2000001
+
+   Dawn Spacecraft and Spacecraft Structures frames:
+   ----------------------------------------------------
+      DAWN_SPACECRAFT         J2000                CK             -203000
+      DAWN_SA+Y               DAWN_SPACECRAFT      CK             -203010
+      DAWN_SA-Y               DAWN_SPACECRAFT      CK             -203020
+      DAWN_HGA                DAWN_SPACECRAFT      FIXED          -203040
+      DAWN_LGA+Z              DAWN_SPACECRAFT      FIXED          -203030
+      DAWN_LGA+X              DAWN_SPACECRAFT      FIXED          -203050
+      DAWN_LGA-Z              DAWN_SPACECRAFT      FIXED          -203060
+      DAWN_ST1                DAWN_SPACECRAFT      FIXED          -203071
+      DAWN_ST2                DAWN_SPACECRAFT      FIXED          -203072
+      DAWN_FT1                DAWN_SPACECRAFT      FIXED (3)      -203081
+      DAWN_FT2                DAWN_SPACECRAFT      FIXED (3)      -203082
+      DAWN_FT3                DAWN_SPACECRAFT      FIXED (3)      -203083
+
+   FC1 and FC2 frames:
+   -------------------
+      DAWN_FC1                DAWN_SPACECRAFT      FIXED          -203110
+      DAWN_FC1_FILTER_1       DAWN_FC1             FIXED          -203111
+      DAWN_FC1_FILTER_2       DAWN_FC1             FIXED          -203112
+      DAWN_FC1_FILTER_3       DAWN_FC1             FIXED          -203113
+      DAWN_FC1_FILTER_4       DAWN_FC1             FIXED          -203114
+      DAWN_FC1_FILTER_5       DAWN_FC1             FIXED          -203115
+      DAWN_FC1_FILTER_6       DAWN_FC1             FIXED          -203116
+      DAWN_FC1_FILTER_7       DAWN_FC1             FIXED          -203117
+      DAWN_FC1_FILTER_8       DAWN_FC1             FIXED          -203118
+
+      DAWN_FC2                DAWN_SPACECRAFT      CK             -203120
+      DAWN_FC2_FILTER_1       DAWN_FC2             FIXED          -203121
+      DAWN_FC2_FILTER_2       DAWN_FC2             FIXED          -203122
+      DAWN_FC2_FILTER_3       DAWN_FC2             FIXED          -203123
+      DAWN_FC2_FILTER_4       DAWN_FC2             FIXED          -203124
+      DAWN_FC2_FILTER_5       DAWN_FC2             FIXED          -203125
+      DAWN_FC2_FILTER_6       DAWN_FC2             FIXED          -203126
+      DAWN_FC2_FILTER_7       DAWN_FC2             FIXED          -203127
+      DAWN_FC2_FILTER_8       DAWN_FC2             FIXED          -203128
+
+   VIR frames:
+   -----------
+      DAWN_VIR                DAWN_SPACECRAFT      FIXED          -203200
+      DAWN_VIR_SCAN           DAWN_VIR             CK             -203201
+      DAWN_VIR_VIS            DAWN_VIR_SCAN        FIXED          -203211
+      DAWN_VIR_IR             DAWN_VIR_SCAN        FIXED          -203213
+
+      DAWN_VIR_VIS_ZERO       DAWN_VIR             FIXED          -203221
+      DAWN_VIR_IR_ZERO        DAWN_VIR             FIXED          -203223
+
+   GRAND frames:
+   -------------
+      DAWN_GRAND              DAWN_SPACECRAFT      FIXED          -203300
+
+   (1) The IAU_VESTA frame is built into the Toolkit starting with the
+       Toolkit version N0054 (June 2010).
+
+   (2) The VESTA_FIXED frame is defined in a separate FK. It is essentially
+       a synonym of the IAU_VESTA frame.
+
+   (3) Although all flight thrusters are mounted on gimbals and can be
+       articulated within a small angular range (+/- 5 degrees during
+       flight), in this version of the FK their frames are defined as
+       fixed offset frames with respect to the spacecraft frame.
+
+
+Spacecraft and Spacecraft Structures Frame Tree
+========================================================================
+
+   The diagram below shows the frame hierarchy for the Dawn spacecraft
+   and its structure frame (not including science instrument frames.)
+
+     "VESTA_IAU_2000"
+     ----------------
+           ^     
+           |<-dynamic
+           |
+           |  "DAWN_CLAUDIA"
+           |  --------------
+           |     ^
+           |     |<-dynamic
+           |     |
+           |     |      
+           |     |             "J2000" INERTIAL
+           +-----------------------------------------------------+
+           |                |         |                          |
+           |<-pck           |<-pck    |                          |<-pck
+           |                |         |                          |
+           V                V         |                          V
+      "VESTA_FIXED"    "IAU_VESTA"    |                    "CERES_FIXED"
+      -------------   -------------   |                    -------------
+                                      |
+                                      |
+                                      |
+       "DAWN_ST1" "DAWN_ST2"          |         "DAWN_LGA+X" "DAWN_LGA-Z"
+       ---------  ----------          |         ------------ ------------
+           ^           ^              |              ^           ^
+           |           |              |              |           |
+           |<-fixed    |<-fixed       |<-ck          |<-fixed    |<-fixed
+           |           |              |              |           |
+           |           |              V              |           |
+           |           |       "DAWN_SPACECRAFT"     |           |
+           +-----------------------------------------------------+
+           |           |              .  | | |       |           |
+           |<-ck       |<-ck          .  | | |       |<-fixed    |<-fixed
+           |           |              .  | | |       |           |
+           V           V              .  | | |       V           V
+       "DAWN_SA+Y" "DAWN_SA-Y"        .  | | |  "DAWN_LGA+Z" "DAWN_HGA"
+       ----------- -----------        .  | | |  ------------ ----------
+                                      .  | | |
+                                      .  | | |<-fixed
+                                      .  | | |
+                                      .  | | V
+                                      .  | | "DAWN_FT1"
+                                      .  | | ----------
+                                      .  | |
+                                      .  | |<-fixed
+                                      .  | |
+                                      .  | V
+                                      .  | "DAWN_FT2"
+                                      .  | ----------
+                                      .  |
+                                      .  |<-fixed
+                                      .  |
+                                      .  V
+                                      .  "DAWN_FT3"
+                                      .  ----------
+                                      .
+                                      .
+                                      V
+                Individual instrument frame trees are provided
+                      in the other sections of this file
+
+
+Dawn Target Frames
+========================================================================
+
+   This section of the file contains the body-fixed frame definitions
+   for the Dawn mission targets -- asteroids 4 Vesta and 1 Ceres.
+
+   All target body-fixed frames are defined according to the standard
+   body-fixed frame formation rules:
+
+      -  +Z axis is toward the North pole;
+
+      -  +X axis is toward the prime meridian;
+
+      -  +Y axis completes the right handed frame;
+
+      -  the origin of this frame is at the center of the body.
+
+   Some of these frames are defined as PCK-based frames with the
+   orientation computed by evaluating corresponding rotation constants
+   provided in the PCK file(s). 
+
+   Other frames are defined as Euler frames with the constants
+   equivalent to the PCK constants included directly into the frame
+   definition.
+
+
+Vesta Frames
+--------------------------------------
+
+``IAU_VESTA'' Frame
+
+   The IAU_VESTA frame is a PCK-based Vesta body-fixed frame built into
+   the SPICE Toolkit starting with the Toolkit version N0064 (June
+   2010). Its orientation is computed using Vesta rotation constants
+   from the last loaded PCK file containing such constants.
+   
+
+``VESTA_FIXED'' Frame
+
+   The VESTA_FIXED frame is a PCK-based Vesta body-fixed frame defined
+   in a separate FK (per request from SOA team on May 9, 2005). This
+   frame is a synonym of the IAU_VESTA frame. Its orientation is
+   computed using Vesta rotation constants from the last loaded PCK
+   file containing such constants.
+
+
+``IAU-2000'' Frame
+
+   The VESTA_IAU_2000 frame represents the ``IAU-2000'' coordinate
+   system used by the project prior to its arrival to Vesta as well as
+   in numerous pre-DAWN ground observations of Vesta. It is defined as
+   an Euler frame mathematically identical to the PCK frame IAU_VESTA
+   when the IAU_VESTA frame is used with the rotation constants from
+   the DAWN PCK file ``pck00008.tpc''.
+
+   The ``pck00008.tpc'' PCK data defining the ``IAU-2000'' coordinate
+   system orientation are:
+
+      BODY2000004_POLE_RA       = (   301.      0.         0.  )
+      BODY2000004_POLE_DEC      = (    41.      0.         0.  )
+      BODY2000004_PM            = (   292.   1617.332776   0.  )
+
+   According to the section ``Example of an Euler Frame'' of [1] the
+   angles for the Euler frame relative to the J2000 frame with the
+   reference epoch of J2000 TDB are derived from the standard set of
+   text PCK body orientation terms as follows:
+
+      ANGLE_1 = -pi/2 - RA
+      ANGLE_2 = -pi/2 + Dec
+      ANGLE_3 =       - PM
+
+   The definition below incorporates the angles derived in this way
+   from the ``IAU-2000'' coordinate system orientation constants
+   above, in degrees with with the PM rate term converted to
+   degrees/sec.
+
+   \begindata
+
+      FRAME_VESTA_IAU_2000             =  -203911
+      FRAME_-203911_NAME               = 'VESTA_IAU_2000'
+      FRAME_-203911_CLASS              =  5
+      FRAME_-203911_CLASS_ID           =  -203911
+      FRAME_-203911_CENTER             =  2000004
+      FRAME_-203911_RELATIVE           = 'J2000'
+      FRAME_-203911_DEF_STYLE          = 'PARAMETERIZED'
+      FRAME_-203911_FAMILY             = 'EULER'
+      FRAME_-203911_EPOCH              =  @2000-JAN-01/12:00:00
+      FRAME_-203911_AXES               =  ( 3  1  3 )
+      FRAME_-203911_UNITS              = 'DEGREES'
+      FRAME_-203911_ANGLE_1_COEFFS     = (  -31.00                           )
+      FRAME_-203911_ANGLE_2_COEFFS     = (  -49.00                           )
+      FRAME_-203911_ANGLE_3_COEFFS     = ( -292.00, -0.18719129351851851E-01 )
+
+   \begintext
+
+
+``DAWN-Claudia'' Frame
+
+   The DAWN_CLAUDIA frame represents the ``DAWN-Claudia'' coordinate
+   system used by the project during operations at Vesta. It is defined
+   as an Euler frame mathematically identical to the PCK frame
+   IAU_VESTA when the IAU_VESTA frame is used with the rotation
+   constants from the DAWN PCK file ``dawn_vesta_v04.tpc''.
+
+   The ``dawn_vesta_v04.tpc'' PCK data defining the ``DAWN-Claudia''
+   coordinate system orientation are:
+
+      BODY2000004_POLE_RA    = ( 309.031    0.0              0.0 )
+      BODY2000004_POLE_DEC   = (  42.235    0.0              0.0 )
+      BODY2000004_PM         = (  75.39  1617.3329428        0.0 )
+
+   According to the section ``Example of an Euler Frame'' of [1] the
+   angles for the Euler frame relative to the J2000 frame with the
+   reference epoch of J2000 TDB are derived from the standard set of
+   text PCK body orientation terms as follows:
+
+      ANGLE_1 = -pi/2 - RA
+      ANGLE_2 = -pi/2 + Dec
+      ANGLE_3 =       - PM
+
+   The definition below incorporates the angles derived in this way
+   from the ``DAWN-Claudia'' coordinate system orientation constants
+   above, in degrees with with the PM rate term converted to
+   degrees/sec.
+
+   \begindata
+
+      FRAME_DAWN_CLAUDIA               =  -203912
+      FRAME_-203912_NAME               = 'DAWN_CLAUDIA'
+      FRAME_-203912_CLASS              =  5
+      FRAME_-203912_CLASS_ID           =  -203912
+      FRAME_-203912_CENTER             =  2000004
+      FRAME_-203912_RELATIVE           = 'J2000'
+      FRAME_-203912_DEF_STYLE          = 'PARAMETERIZED'
+      FRAME_-203912_FAMILY             = 'EULER'
+      FRAME_-203912_EPOCH              =  @2000-JAN-01/12:00:00
+      FRAME_-203912_AXES               =  ( 3  1  3 )
+      FRAME_-203912_UNITS              = 'DEGREES'
+      FRAME_-203912_ANGLE_1_COEFFS     = (  -39.031                          )
+      FRAME_-203912_ANGLE_2_COEFFS     = (  -47.765                          )
+      FRAME_-203912_ANGLE_3_COEFFS     = (  -75.39, -0.18719131282407406E-01 )
+
+   \begintext
+
+
+Dawn Spacecraft and Spacecraft Structures Frames
+========================================================================
+
+   This section of the file contains the definitions of the spacecraft
+   and spacecraft structures frames.
+
+
+Dawn Spacecraft Frame
+--------------------------------------
+
+   The Dawn spacecraft frame is defined as follows:
+
+      -  +Z axis is along the nominal boresight direction of the framing
+         cameras;
+
+      -  +X axis is along the nominal boresight direction of the HGA;
+
+      -  +Y axis completes the right-hand frame;
+
+      -  the origin of this frame is the launch vehicle interface point.
+
+   These diagrams illustrate the DAWN_SPACECRAFT frame:
+
+
+   +X s/c side (HGA side) view:
+   ----------------------------
+                                    ^
+                                    | toward asteroid
+                                    |
+
+                               Science Deck
+                             ._____________.
+   .__  _______________.     |   ._____.   |     .______________  ___.
+   |  \ \               \    | .'       `. |    /               \ \  |
+   |  / /                \   |/     |     \|   /                / /  |
+   |  \ \                 `. .      |      . .'                 \ \  |
+   |  / /                 | o|      o      |o |                 / /  |
+   |  \ \                 .' .    .' `.    . `.                 \ \  |
+   |  / /                /   |\ +Zsc^  `  /|   \                / /  |
+   .__\ \_______________/    | `.   |   .' |    \_______________\ \__.
+     -Y Solar Array          .___` -|- '___.       +Y Solar Array
+                                  / | \
+                                  `-o-----> +Ysc
+                                  +Xsc
+                                                     +Xsc is out of
+                                                        the page
+
+   +Z s/c side (science deck side) view:
+   -------------------------------------
+
+                             ._____________.
+                             |             |
+                             |             |
+                             |  +Zsc    +Ysc
+   o==/ /==================o |      o----->|o==================/ /==o
+     -Y Solar Array          |      |      |        +Y Solar Array
+                             |      |      |
+                             .______|______.
+                                 .--V +Xsc
+                          HGA  .'       `.
+                              /___________\
+                                  `.|.'                 +Zsc is out
+                                                       of the page
+
+
+   Since the orientation of the DAWN_SPACECRAFT frame is computed
+   on-board, sent down in telemetry, and stored in the s/c CK files, it
+   is defined as a CK-based frame.
+
+   \begindata
+
+      FRAME_DAWN_SPACECRAFT            = -203000
+      FRAME_-203000_NAME               = 'DAWN_SPACECRAFT'
+      FRAME_-203000_CLASS              =  3
+      FRAME_-203000_CLASS_ID           = -203000
+      FRAME_-203000_CENTER             = -203
+      CK_-203000_SCLK                  = -203
+      CK_-203000_SPK                   = -203
+
+   \begintext
+
+
+Dawn Solar Array Frames
+--------------------------------------
+
+   Since the Dawn solar arrays can be articulated (each having one
+   degree of freedom), the solar Array frames, DAWN_SA+Y and DAWN_SA-Y,
+   are defined as CK frames with their orientation given relative to
+   the DAWN_SPACECRAFT frame.
+
+   Both array frames are defined as follows (from [5]):
+
+      -  +Y axis is parallel to the longest side of the array,
+         positively oriented from the yoke to the end of the wing;
+
+      -  +Z axis is normal to the solar array plane, the solar cells
+         facing +Z;
+
+      -  +X axis is defined such that (X,Y,Z) is right handed;
+
+      -  the origin of the frame is located at the yoke geometric
+         center.
+
+   The axis of rotation is parallel to the Y axis of the spacecraft and
+   solar array frames.
+
+   This diagram illustrates the DAWN_SA+Y and DAWN_SA-Y frames:
+
+
+   +X s/c side (HGA side) view:
+   ----------------------------
+                                    ^
+                                    | toward asteroid
+                                    |
+
+                               Science Deck
+                             ._____________. +Xsa+y
+   .__  _______________.     |   ._____.   |^    .______________  ___.
+   |  \ \               \    | .'       `. ||   /               \ \  |
+   |  / /                \   |/     |     \||  /                / /  |
+   |  \ \                 `. .      |      .|.'                 \ \  |
+   |  / /      +Ysa-y <-----x|      o      |x-----> +Ysa+y      / /  |
+   |  \ \                 .'|.    .' `.    . `.                 \ \  |
+   |  / /                /  ||\ +Zsc^  `  /|   \                / /  |
+   .__\ \_______________/   || `.   |   .' |    \_______________\ \__.
+     -Y Solar Array         V.___` -|- '___.       +Y Solar Array
+                      +Xsa-y      / | \
+                                  `-o-----> +Ysc
+                                  +Xsc
+                                               +Xsc is out of the page
+
+                                                  +Zsa+y and +Zsa-y
+                                                  are into the page
+
+                                                 Active solar cell is
+                                              facing away from the viewer
+
+
+   These sets of keywords define the solar array frames as CK frames:
+
+   \begindata
+
+      FRAME_DAWN_SA+Y                  = -203010
+      FRAME_-203010_NAME               = 'DAWN_SA+Y'
+      FRAME_-203010_CLASS              =  3
+      FRAME_-203010_CLASS_ID           = -203010
+      FRAME_-203010_CENTER             = -203
+      CK_-203010_SCLK                  = -203
+      CK_-203010_SPK                   = -203
+
+      FRAME_DAWN_SA-Y                  = -203020
+      FRAME_-203020_NAME               = 'DAWN_SA-Y'
+      FRAME_-203020_CLASS              =  3
+      FRAME_-203020_CLASS_ID           = -203020
+      FRAME_-203020_CENTER             = -203
+      CK_-203020_SCLK                  = -203
+      CK_-203020_SPK                   = -203
+
+   \begintext
+
+
+Dawn Low Gain Antenna Frames
+--------------------------------------
+
+   DAWN has three Low Gain Antennas (LGAs) [see 6]: LGA+Z pointing along
+   the s/c +Z axis, LGA+X pointing along the s/c +X axis, and LGA-Z
+   pointing along the s/c -Z axis. All three LGAs are rigidly attached
+   to the s/c bus. Therefore, their frames -- DAWN_LGA+Z, DAWN_LGA+X,
+   and DAWN_LGA-Z -- are defined as a fixed offset frames with
+   orientation given relative to the DAWN_SPACECRAFT frame.
+
+   Each of the DAWN LGA frames - DAWN_LGA+Z, DAWN_LGA+X, and DAWN_LGA-Z
+   -- is defined as follows:
+
+      -  +Z axis is in the antenna boresight direction;
+
+      -  +Y axis is nominally parallel to the s/c +Y axis;
+
+      -  +X axis completes the right handed frame;
+
+      -  the origin of the frame is located at the geometric center of
+         the LGA outer patch.
+
+   Neither +X nor +Y axis of in each frame is lined up with the antenna
+   clock angle reference direction, which was not known at the time
+   when this version of the FK was created.
+
+   This diagram illustrates the DAWN LGA frames:
+
+   +Z s/c side view:
+   -----------------
+
+                             ._____________.
+                             |             |
+                             |             |
+                             |  +Zsc    +Ysc
+   o==/ /==================o |      o---->  o==================/ /==o
+   -Y Solar Array          +Zlga+z  |      ^+Xlga-z     +Y Solar Array
+                             | o----->     |
+                             ._|____|______|
+                               | .--V--.   x-----> +Ylga-z
+                               |  +Xsc  `. x-----> +Ylga+x
+                               V _________\|
+                          +Xlga+z `.|.'    |
+                                           |
+                                   HGA     V
+                                         +Zlga+x
+
+                                                   +Zsc and +Zlga+z are out
+                                                         of the page
+
+                                                   +Xlga+x and +Zlga-z are
+                                                        into the page
+
+   As seen on the diagram the DAWN_LGA+Z frame and the s/c frame are
+   nominally co-aligned, the DAWN_LGA+X frame is rotated from the s/c
+   frame by +90 degrees about Y, and the DAWN_LGA-Z frame is rotated
+   from the s/c frame by 180 degree about Y.
+
+   These sets of keywords define the LGA frames:
+
+   \begindata
+
+      FRAME_DAWN_LGA+Z                 =  -203030
+      FRAME_-203030_NAME               = 'DAWN_LGA+Z'
+      FRAME_-203030_CLASS              =  4
+      FRAME_-203030_CLASS_ID           =  -203030
+      FRAME_-203030_CENTER             =  -203
+      TKFRAME_-203030_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203030_SPEC             = 'ANGLES'
+      TKFRAME_-203030_UNITS            = 'DEGREES'
+      TKFRAME_-203030_ANGLES           = (   0.000,  0.000,   0.000 )
+      TKFRAME_-203030_AXES             = (   1,      2,       3     )
+
+      FRAME_DAWN_LGA+X                 =  -203050
+      FRAME_-203050_NAME               = 'DAWN_LGA+X'
+      FRAME_-203050_CLASS              =  4
+      FRAME_-203050_CLASS_ID           =  -203050
+      FRAME_-203050_CENTER             =  -203
+      TKFRAME_-203050_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203050_SPEC             = 'ANGLES'
+      TKFRAME_-203050_UNITS            = 'DEGREES'
+      TKFRAME_-203050_ANGLES           = (   0.000, -90.00,   0.000 )
+      TKFRAME_-203050_AXES             = (   1,       2,      3     )
+
+      FRAME_DAWN_LGA-Z                 =  -203060
+      FRAME_-203060_NAME               = 'DAWN_LGA-Z'
+      FRAME_-203060_CLASS              =  4
+      FRAME_-203060_CLASS_ID           =  -203060
+      FRAME_-203060_CENTER             =  -203
+      TKFRAME_-203060_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203060_SPEC             = 'ANGLES'
+      TKFRAME_-203060_UNITS            = 'DEGREES'
+      TKFRAME_-203060_ANGLES           = (   0.000, 180.00,  0.000 )
+      TKFRAME_-203060_AXES             = (   1,       2,     3     )
+
+   \begintext
+
+
+Dawn High Gain Antenna Frame
+--------------------------------------
+
+   The Dawn High Gain Antenna is rigidly attached to the +X side of the
+   s/c bus. Therefore, the Dawn HGA frame, DAWN_HGA, is defined as a
+   fixed offset frame with its orientation given relative to the
+   DAWN_SPACECRAFT frame.
+
+   The DAWN_HGA frame is defined as follows:
+
+      -  +Z axis is in the antenna boresight direction;
+
+      -  +Y axis is nominally parallel to the s/c +Y axis;
+
+      -  +X axis completes the right handed frame;
+
+      -  the origin of the frame is located at the geometric center of
+         the HGA dish outer rim circle.
+
+   This diagram illustrates the DAWN_HGA frame:
+
+   +Z s/c side (science deck side) view:
+   -------------------------------------
+
+                             ._____________.
+                             |             |
+                             |             |
+                             |  +Zsc    +Ysc
+   o==/ /==================o |      o----->|o==================/ /==o
+     -Y Solar Array          |      |      |        +Y Solar Array
+                             |      |      |
+                             .______|______.
+                                 .--V +Xsc
+                          HGA  .'       `.
+                              /_____x----->
+                                  `.|.'  +Yhga         +Zsc is out
+                                    |                  of the page
+                                    |
+                                    V +Zhga            +Xhga is into
+                                                         the page
+
+
+
+   As seen on the diagram a single rotation by +90 degrees about +Y is
+   needed to align the s/c frame with the HGA frame.
+
+   According to [7] the actual HGA boresight direction in the spacecraft
+   frame used in the on-board FSW code and ACS ground tools is:
+
+      AcTable.Boresight.HighGainAntenna.v =
+        {0.999999899738598, -0.000219079458599998, -0.000390547031294996}
+
+   The following two rotations are needed to align the spacecraft frame
+   with the HGA frame having +Z along this direction: first by
+   +90.02237670 degrees about Y, then by +0.01255233 degrees about X.
+
+   This set of keywords defines the HGA frame as a fixed offset frame:
+
+   \begindata
+
+      FRAME_DAWN_HGA                   =  -203040
+      FRAME_-203040_NAME               = 'DAWN_HGA'
+      FRAME_-203040_CLASS              =  4
+      FRAME_-203040_CLASS_ID           =  -203040
+      FRAME_-203040_CENTER             =  -203
+      TKFRAME_-203040_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203040_SPEC             = 'ANGLES'
+      TKFRAME_-203040_UNITS            = 'DEGREES'
+      TKFRAME_-203040_ANGLES           = ( -90.02237670, -0.01255233,   0.0 )
+      TKFRAME_-203040_AXES             = (   2,           1,            3   )
+
+   \begintext
+
+
+Dawn Star Tracker Frames
+--------------------------------------
+
+   The star trackers (ST1 and ST2) are rigidly attached to the +Z side
+   of the s/c bus. Therefore, the star tracker frames, DAWN_ST1 and
+   DAWN_ST2, are defined as fixed offset frames with their orientation
+   given relative to the DAWN_SPACECRAFT frame.
+
+   The star tracker frames are defined as follows:
+
+      -  +Z axis is in the star tracker boresight direction;
+
+      -  +X axis nominally points along the s/c +Z axis;
+
+      -  +Y axis completes the right handed frame;
+
+      -  the origin of the frame is located at the star tracker focal
+         point.
+
+   This diagram illustrates the star tracker frames:
+
+   +Z s/c side (science deck side) view:
+   -------------------------------------
+
+
+                       \   30 deg   |   30 deg   /
+                        \<--------->|<--------->/
+                         \          |          /
+
+                          +Zst2            +Zst1
+                            ^      +Yst1    ^
+                             \        ^    /
+                              \     .'    /
+                             ._\__.'_____/_.
+                          +Xst2 o'      o +Xst1
+                             |           `.|
+                             |  +Zsc       `.  +Yst2
+   o==/ /==================o |      o----->|o`>================/ /==o
+     -Y Solar Array          |      |   +Ysc        +Y Solar Array
+                             |      |      |
+                             .______|______.
+                                 .--V +Xsc
+                          HGA  .'       `.
+                              /___________\
+                                  `.|.'           +Zsc, +Xst1 and +Xst2 are
+                                                      out of the page
+
+
+   As seen on the diagram two rotations -- first by -90 degrees about Y
+   and second by -30 degree (for ST1) or +30 degrees (for ST2) about X
+   -- are needed to align the s/c frame with the star tracker frames.
+
+   This nominal alignment was provided in the officially released 
+   FK versions 0.1 to 0.8.
+
+   Per MCR-111570, 03/18/11, the nominal alignments were replaced with
+   the following actual alignments provided in [8] and [9].
+
+      Star Tracker 1 wrt Spacecraft Frame: R_ST1_2,SF in the "Inputs"
+      section of [8]:
+
+         -0.00167591111459615  -0.00865834105070781  -0.999961111469934
+          0.497384915940654     0.867489831468208    -0.00834492024941222
+          0.867528349229375    -0.497379558716992     0.00285269238533509
+ 
+      Star Tracker 2 wrt Spacecraft Frame: QBdyToSta[1] and
+      DcmBdyToSta[1] on page 24 in the "Appendix A" of [9]:
+
+          0.003428012232148947 -0.002975996167250916 -0.9999896960363887
+         -0.5035582110269716    0.8639506124714249   -0.004297361698267110
+          0.8639544992876952    0.5035677537899567    0.001463045961520582
+
+   Because these alignments are for the ACS star tracker frames with
+   the boresight along -Z they had to be rotated by 180 degrees about Y
+   to agree with the frame definition described above (boresight along
+   +Z). Such rotation is equivalent to flipping the sign for each
+   component in the top and bottom rows of the matrices. These
+   alignments were incorporated into the FK starting with version 1.0
+   (March 2011).
+
+   The sets of keywords below defines the star tracker frames.
+
+   \begindata
+
+      FRAME_DAWN_ST1                   =  -203071
+      FRAME_-203071_NAME               = 'DAWN_ST1'
+      FRAME_-203071_CLASS              =  4
+      FRAME_-203071_CLASS_ID           =  -203071
+      FRAME_-203071_CENTER             =  -203
+      TKFRAME_-203071_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203071_SPEC             = 'MATRIX'
+      TKFRAME_-203071_MATRIX           = (
+
+          0.00167591111459615   0.00865834105070781   0.999961111469934
+          0.497384915940654     0.867489831468208    -0.00834492024941222
+         -0.867528349229375     0.497379558716992    -0.00285269238533509
+
+                                         )
+
+
+      FRAME_DAWN_ST2                   =  -203072
+      FRAME_-203072_NAME               = 'DAWN_ST2'
+      FRAME_-203072_CLASS              =  4
+      FRAME_-203072_CLASS_ID           =  -203072
+      FRAME_-203072_CENTER             =  -203
+      TKFRAME_-203072_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203072_SPEC             = 'MATRIX'
+      TKFRAME_-203072_MATRIX           = (
+
+         -0.003428012232148947  0.002975996167250916  0.9999896960363887
+         -0.5035582110269716    0.8639506124714249   -0.004297361698267110
+         -0.8639544992876952   -0.5035677537899567   -0.001463045961520582
+
+                                         )
+
+   \begintext
+
+
+Dawn Flight Thruster Frames
+--------------------------------------
+
+   Although the flight thrusters (FT1, FT2, and FT3) are mounted on
+   gimbals and can be articulated within a small angular range (+/- 5
+   degrees during flight), in this version of the FK their frames --
+   DAWN_FT1, DAWN_FT2, and DAWN_FT3 -- are defined as fixed offset
+   frames with respect to the spacecraft frame.
+
+   Each of the flight thruster frames is defined in the same way as
+   follows:
+
+      -  +Z axis is in the thrust direction;
+
+      -  +Y axis nominally points along the s/c +Y axis;
+
+      -  +X axis completes the right handed frame;
+
+      -  the origin of the frame is located at the geometric center of
+         the thruster nozzle outer rim circle.
+
+   This diagram illustrates the flight thruster frames:
+
+   +Y s/c side view:
+   -----------------
+                               Science Deck
+                             ._____________.
+                        .    |      .      |
+                        |`.  |      |+Y solar array
+                        |  \ |      |      |
+                      .'|   .|      |      |
+                      --|    |      o      |
+                      `.|   '|      |      |     .> +Xft1
+                        |  / |  +Zsc^      |   .'
+                        |.'  |      |      | .'
+                             o______|______o'
+                            / `.  / | \     \
+                           /  <-----o----->  \
+                          / +Xsc  `>|  +Xft3  \
+                         V     +Xft1|          V +Zft1
+                     +Zft2          |
+                                    V +Zft3
+
+                      /    48 deg   |   48 deg    \     +Ysc, +Yft1, +Yft2,
+                     /<------------>|<------------>\   and +Yft3 are out of
+                    /               |               \       the page
+
+
+   As seen on the diagram one rotation -- about +Y by -132 degrees for
+   FT1, +132 degrees for FT2, or 180 degrees for FT3 -- is needed to
+   align the s/c frame with the individual thruster frame.
+
+   The sets of keywords below defines the flight thruster frames:
+
+   \begindata
+
+      FRAME_DAWN_FT1                   =  -203081
+      FRAME_-203081_NAME               = 'DAWN_FT1'
+      FRAME_-203081_CLASS              =  4
+      FRAME_-203081_CLASS_ID           =  -203081
+      FRAME_-203081_CENTER             =  -203
+      TKFRAME_-203081_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203081_SPEC             = 'ANGLES'
+      TKFRAME_-203081_UNITS            = 'DEGREES'
+      TKFRAME_-203081_ANGLES           = (   0.000,  132.000,   0.000 )
+      TKFRAME_-203081_AXES             = (   3,        2,       1     )
+
+      FRAME_DAWN_FT2                   =  -203082
+      FRAME_-203082_NAME               = 'DAWN_FT2'
+      FRAME_-203082_CLASS              =  4
+      FRAME_-203082_CLASS_ID           =  -203082
+      FRAME_-203082_CENTER             =  -203
+      TKFRAME_-203082_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203082_SPEC             = 'ANGLES'
+      TKFRAME_-203082_UNITS            = 'DEGREES'
+      TKFRAME_-203082_ANGLES           = (   0.000, -132.000,   0.000 )
+      TKFRAME_-203082_AXES             = (   3,        2,       1     )
+
+      FRAME_DAWN_FT3                   =  -203083
+      FRAME_-203083_NAME               = 'DAWN_FT3'
+      FRAME_-203083_CLASS              =  4
+      FRAME_-203083_CLASS_ID           =  -203083
+      FRAME_-203083_CENTER             =  -203
+      TKFRAME_-203083_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203083_SPEC             = 'ANGLES'
+      TKFRAME_-203083_UNITS            = 'DEGREES'
+      TKFRAME_-203083_ANGLES           = (   0.000,  180.000,   0.000 )
+      TKFRAME_-203083_AXES             = (   3,        2,       1     )
+
+   \begintext
+
+
+FC1 and FC2 Frames
+========================================================================
+
+   This section of the file contains the definitions of the Framing
+   Camera 1 (FC1) and Framing Camera 2 (FC2) frames.
+
+
+FC1 and FC2 Frame Tree
+--------------------------------------
+
+   The diagram below shows the FC1 and FC2 frame hierarchy.
+
+     "VESTA_IAU_2000"
+     ----------------
+           ^     
+           |<-dynamic
+           |
+           |  "DAWN_CLAUDIA"
+           |  --------------
+           |     ^
+           |     |<-dynamic
+           |     |
+           |     |      
+           |     |             "J2000" INERTIAL
+           +-----------------------------------------------------+
+           |                |         |                          |
+           |<-pck           |<-pck    |                          |<-pck
+           |                |         |                          |
+           V                V         |                          V
+      "VESTA_FIXED"    "IAU_VESTA"    |                    "CERES_FIXED"
+      -------------   -------------   |                    -------------
+                                      |
+                                      |<-ck
+                                      |
+                                      V
+                               "DAWN_SPACECRAFT"
+           +-----------------------------------------------------+
+           |                                                     |
+           |<-fixed                                              |<-ck
+           |                                                     |
+           V                                                     V
+       "DAWN_FC1"                                            "DAWN_FC2"
+       ----------                                            ----------
+           |                                                     |
+           |<-fixed                                              |<-fixed
+           |                                                     |
+           V                                                     V
+       "DAWN_FC1_FILTER_[1..8]"                "DAWN_FC2_FILTER_[1..8]"
+       ------------------------                ------------------------
+
+
+FC1 and FC2 Frames
+--------------------------------------
+
+   The Framing Cameras 1 and 2 camera frames -- DAWN_FC1 and DAWN_FC2
+   -- are defined as follows:
+
+      -  +Z axis points along the camera boresight;
+
+      -  +X axis is parallel to the apparent image lines; it is
+         nominally co-aligned with the s/c +X axis;
+
+      -  +Y axis completes the right handed frame; it is nominally
+         parallel the to the apparent image columns and co-aligned with
+         the s/c +Y axis;
+
+      -  the origin of the frame is located at the camera focal point.
+
+   The Framing Cameras 1 and 2 filter frames -- DAWN_FC1_FILTER_[1..8]
+   and DAWN_FC2_FILTER_[1..8] -- are defined to be nominally co-aligned
+   with the corresponding camera frames.
+
+   This diagram illustrates the FC1 and FC2 camera frames:
+
+
+   +Z s/c side (science deck side) view:
+   -------------------------------------
+
+                                       +Yfc1
+                             ._____________.
+                             |    o---o->---> +Yfc2
+                             |    |   |    |
+                             |    |   |    |+Ysc
+   o==/ /==================o |    | o-|--->|o==================/ /==o
+     -Y Solar Array          |    V | V    |        +Y Solar Array
+                             |+Xfc1 | +Xfc2
+                             .______|______.
+                                 .--V +Xsc
+                          HGA  .'       `.           +Zsc, +Zfc1, and
+                              /___________\            +Zfc2 are out
+                                  `.|.'                 of the page
+
+
+   Nominally, the FC1 and FC2 frames are co-aligned with the s/c frame.
+   The following nominal FC1 and FC2 frame definitions were provided in
+   the FK from October 11, 2004 to January 5, 2009 (ver. 0.0 to 0.5):
+
+      FRAME_DAWN_FC1                   =  -203110
+      FRAME_-203110_NAME               = 'DAWN_FC1'
+      FRAME_-203110_CLASS              =  4
+      FRAME_-203110_CLASS_ID           =  -203110
+      FRAME_-203110_CENTER             =  -203
+      TKFRAME_-203110_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203110_SPEC             = 'ANGLES'
+      TKFRAME_-203110_UNITS            = 'DEGREES'
+      TKFRAME_-203110_ANGLES           = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203110_AXES             = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC2                   =  -203120
+      FRAME_-203120_NAME               = 'DAWN_FC2'
+      FRAME_-203120_CLASS              =  4
+      FRAME_-203120_CLASS_ID           =  -203120
+      FRAME_-203120_CENTER             =  -203
+      TKFRAME_-203120_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203120_SPEC             = 'ANGLES'
+      TKFRAME_-203120_UNITS            = 'DEGREES'
+      TKFRAME_-203120_ANGLES           = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203120_AXES             = ( 1,   2,   3   )
+
+   These frame alignments were used by FC team at DLR, Germany to
+   process February 2009 Mars Gravity Assist data;
+
+      FRAME_DAWN_FC1                   =  -203110
+      FRAME_-203110_NAME               = 'DAWN_FC1'
+      FRAME_-203110_CLASS              =  4
+      FRAME_-203110_CLASS_ID           =  -203110
+      FRAME_-203110_CENTER             =  -203
+      TKFRAME_-203110_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203110_SPEC             = 'ANGLES'
+      TKFRAME_-203110_UNITS            = 'DEGREES'
+      TKFRAME_-203110_ANGLES          = ( -0.00302298, 0.07040644, 0.06472022 )
+      TKFRAME_-203110_AXES             = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC2                   =  -203120
+      FRAME_-203120_NAME               = 'DAWN_FC2'
+      FRAME_-203120_CLASS              =  4
+      FRAME_-203120_CLASS_ID           =  -203120
+      FRAME_-203120_CENTER             =  -203
+      TKFRAME_-203120_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203120_SPEC             = 'ANGLES'
+      TKFRAME_-203120_UNITS            = 'DEGREES'
+      TKFRAME_-203120_ANGLES          = ( -0.07360254, 0.19136667, 0.08369507 )
+      TKFRAME_-203120_AXES             = ( 1,   2,   3   )
+
+   The two matrices below represent the actual orientation of the FC1
+   and FC2 frames. These matrices rotate vectors from the s/c frame to
+   the corresponding camera frames. These matrices were determined by
+   Nick Mastrodemos, DAWN Optical Navigation Team, using the Functional,
+   Performance and Calibration test images taken in 2007-2008. They
+   were provided to NAIF on January 5, 2009 and were incorporated into
+   the FK starting with version 0.6 (January 2009):
+
+      FC1:
+
+          0.999998669076022  -0.001146506533836   0.001160762229150
+          0.001146467511555   0.999999342218256   0.000034282638084
+         -0.001160800770890  -0.000032951816272   0.999999325727647
+
+
+      FC2:
+
+          0.999993562497650  -0.001478972971767   0.003269189839768
+          0.001475079784942   0.999998200488307   0.001192962604301
+         -0.003270948316271  -0.001188132608755   0.999993944600674
+
+   Per MCR-111570, 03/18/11, the actual alignments above were replaced
+   with the following updated values provided in [8] and incorporated
+   in the FK with version 1.0 (March 2011):
+
+      FC1:
+
+          0.99999903640145     -0.00088624511873564   0.001068487703551
+          0.000886539816130183  0.999999569071098    -0.000275356733179061
+         -0.0010682432039777    0.000276303753185878  0.999999391254863
+
+      FC2:
+
+          0.999994211374513    -0.00121806017718856   0.00317701858659441
+          0.00121525960845842   0.999998871426382     0.000883293086781172
+         -0.00317809089965586  -0.000879427042947794  0.999994563157032
+
+   The FC1 matrix is provided in the frame definition below.
+
+   Per MCR-117124, 04/01/15, the FC2 alignment was adjusted based on an
+   analysis of 196 pictures from Ceres Opnavs 1-5, taken 01/13/15 to
+   03/02/15. The new alignment is:
+
+      FC2:
+
+         0.999994729254062      -0.00121791297955331    0.00300965983081698
+         0.00121554146625864     0.999998949394655      0.000789674082497601
+        -0.00301061841759422    -0.000786011525583021   0.999995159168256
+
+   Since two different FC2 alignments -- one applicable to the Vesta
+   mission time period and the other to the Ceres mission time period
+   -- cannot be incorporated into a single fixed-offset frame, in the
+   FK version 1.3 (April 2015) the DAWN_FC2 frame class was changed
+   from a fixed-offset (class 4) to CK based (class 3) and two
+   different FC2 alignments were stored in a CK file for ID -203120.
+
+   \begindata
+
+      FRAME_DAWN_FC1                   =  -203110
+      FRAME_-203110_NAME               = 'DAWN_FC1'
+      FRAME_-203110_CLASS              =  4
+      FRAME_-203110_CLASS_ID           =  -203110
+      FRAME_-203110_CENTER             =  -203
+      TKFRAME_-203110_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203110_SPEC             = 'MATRIX'
+      TKFRAME_-203110_MATRIX           = (
+
+          0.99999903640145     -0.00088624511873564   0.001068487703551
+          0.000886539816130183  0.999999569071098    -0.000275356733179061
+         -0.0010682432039777    0.000276303753185878  0.999999391254863
+
+                                         )
+
+      FRAME_DAWN_FC2                   =  -203120
+      FRAME_-203120_NAME               = 'DAWN_FC2'
+      FRAME_-203120_CLASS              =  3
+      FRAME_-203120_CLASS_ID           = -203120
+      FRAME_-203120_CENTER             = -203
+      CK_-203120_SCLK                  = -203
+      CK_-203120_SPK                   = -203
+
+   \begintext
+
+   The keywords below define the FC filter frames to be co-aligned with
+   the corresponding camera frames.
+
+   \begindata
+
+      FRAME_DAWN_FC1_FILTER_1       = -203111
+      FRAME_-203111_NAME            = 'DAWN_FC1_FILTER_1'
+      FRAME_-203111_CLASS           = 4
+      FRAME_-203111_CLASS_ID        = -203111
+      FRAME_-203111_CENTER          = -203
+      TKFRAME_-203111_RELATIVE      = 'DAWN_FC1'
+      TKFRAME_-203111_SPEC          = 'ANGLES'
+      TKFRAME_-203111_UNITS         = 'DEGREES'
+      TKFRAME_-203111_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203111_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC1_FILTER_2       = -203112
+      FRAME_-203112_NAME            = 'DAWN_FC1_FILTER_2'
+      FRAME_-203112_CLASS           = 4
+      FRAME_-203112_CLASS_ID        = -203112
+      FRAME_-203112_CENTER          = -203
+      TKFRAME_-203112_RELATIVE      = 'DAWN_FC1'
+      TKFRAME_-203112_SPEC          = 'ANGLES'
+      TKFRAME_-203112_UNITS         = 'DEGREES'
+      TKFRAME_-203112_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203112_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC1_FILTER_3       = -203113
+      FRAME_-203113_NAME            = 'DAWN_FC1_FILTER_3'
+      FRAME_-203113_CLASS           = 4
+      FRAME_-203113_CLASS_ID        = -203113
+      FRAME_-203113_CENTER          = -203
+      TKFRAME_-203113_RELATIVE      = 'DAWN_FC1'
+      TKFRAME_-203113_SPEC          = 'ANGLES'
+      TKFRAME_-203113_UNITS         = 'DEGREES'
+      TKFRAME_-203113_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203113_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC1_FILTER_4       = -203114
+      FRAME_-203114_NAME            = 'DAWN_FC1_FILTER_4'
+      FRAME_-203114_CLASS           = 4
+      FRAME_-203114_CLASS_ID        = -203114
+      FRAME_-203114_CENTER          = -203
+      TKFRAME_-203114_RELATIVE      = 'DAWN_FC1'
+      TKFRAME_-203114_SPEC          = 'ANGLES'
+      TKFRAME_-203114_UNITS         = 'DEGREES'
+      TKFRAME_-203114_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203114_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC1_FILTER_5       = -203115
+      FRAME_-203115_NAME            = 'DAWN_FC1_FILTER_5'
+      FRAME_-203115_CLASS           = 4
+      FRAME_-203115_CLASS_ID        = -203115
+      FRAME_-203115_CENTER          = -203
+      TKFRAME_-203115_RELATIVE      = 'DAWN_FC1'
+      TKFRAME_-203115_SPEC          = 'ANGLES'
+      TKFRAME_-203115_UNITS         = 'DEGREES'
+      TKFRAME_-203115_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203115_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC1_FILTER_6       = -203116
+      FRAME_-203116_NAME            = 'DAWN_FC1_FILTER_6'
+      FRAME_-203116_CLASS           = 4
+      FRAME_-203116_CLASS_ID        = -203116
+      FRAME_-203116_CENTER          = -203
+      TKFRAME_-203116_RELATIVE      = 'DAWN_FC1'
+      TKFRAME_-203116_SPEC          = 'ANGLES'
+      TKFRAME_-203116_UNITS         = 'DEGREES'
+      TKFRAME_-203116_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203116_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC1_FILTER_7       = -203117
+      FRAME_-203117_NAME            = 'DAWN_FC1_FILTER_7'
+      FRAME_-203117_CLASS           = 4
+      FRAME_-203117_CLASS_ID        = -203117
+      FRAME_-203117_CENTER          = -203
+      TKFRAME_-203117_RELATIVE      = 'DAWN_FC1'
+      TKFRAME_-203117_SPEC          = 'ANGLES'
+      TKFRAME_-203117_UNITS         = 'DEGREES'
+      TKFRAME_-203117_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203117_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC1_FILTER_8       = -203118
+      FRAME_-203118_NAME            = 'DAWN_FC1_FILTER_8'
+      FRAME_-203118_CLASS           = 4
+      FRAME_-203118_CLASS_ID        = -203118
+      FRAME_-203118_CENTER          = -203
+      TKFRAME_-203118_RELATIVE      = 'DAWN_FC1'
+      TKFRAME_-203118_SPEC          = 'ANGLES'
+      TKFRAME_-203118_UNITS         = 'DEGREES'
+      TKFRAME_-203118_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203118_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC2_FILTER_1       = -203121
+      FRAME_-203121_NAME            = 'DAWN_FC2_FILTER_1'
+      FRAME_-203121_CLASS           = 4
+      FRAME_-203121_CLASS_ID        = -203121
+      FRAME_-203121_CENTER          = -203
+      TKFRAME_-203121_RELATIVE      = 'DAWN_FC2'
+      TKFRAME_-203121_SPEC          = 'ANGLES'
+      TKFRAME_-203121_UNITS         = 'DEGREES'
+      TKFRAME_-203121_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203121_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC2_FILTER_2       = -203122
+      FRAME_-203122_NAME            = 'DAWN_FC2_FILTER_2'
+      FRAME_-203122_CLASS           = 4
+      FRAME_-203122_CLASS_ID        = -203122
+      FRAME_-203122_CENTER          = -203
+      TKFRAME_-203122_RELATIVE      = 'DAWN_FC2'
+      TKFRAME_-203122_SPEC          = 'ANGLES'
+      TKFRAME_-203122_UNITS         = 'DEGREES'
+      TKFRAME_-203122_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203122_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC2_FILTER_3       = -203123
+      FRAME_-203123_NAME            = 'DAWN_FC2_FILTER_3'
+      FRAME_-203123_CLASS           = 4
+      FRAME_-203123_CLASS_ID        = -203123
+      FRAME_-203123_CENTER          = -203
+      TKFRAME_-203123_RELATIVE      = 'DAWN_FC2'
+      TKFRAME_-203123_SPEC          = 'ANGLES'
+      TKFRAME_-203123_UNITS         = 'DEGREES'
+      TKFRAME_-203123_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203123_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC2_FILTER_4       = -203124
+      FRAME_-203124_NAME            = 'DAWN_FC2_FILTER_4'
+      FRAME_-203124_CLASS           = 4
+      FRAME_-203124_CLASS_ID        = -203124
+      FRAME_-203124_CENTER          = -203
+      TKFRAME_-203124_RELATIVE      = 'DAWN_FC2'
+      TKFRAME_-203124_SPEC          = 'ANGLES'
+      TKFRAME_-203124_UNITS         = 'DEGREES'
+      TKFRAME_-203124_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203124_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC2_FILTER_5       = -203125
+      FRAME_-203125_NAME            = 'DAWN_FC2_FILTER_5'
+      FRAME_-203125_CLASS           = 4
+      FRAME_-203125_CLASS_ID        = -203125
+      FRAME_-203125_CENTER          = -203
+      TKFRAME_-203125_RELATIVE      = 'DAWN_FC2'
+      TKFRAME_-203125_SPEC          = 'ANGLES'
+      TKFRAME_-203125_UNITS         = 'DEGREES'
+      TKFRAME_-203125_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203125_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC2_FILTER_6       = -203126
+      FRAME_-203126_NAME            = 'DAWN_FC2_FILTER_6'
+      FRAME_-203126_CLASS           = 4
+      FRAME_-203126_CLASS_ID        = -203126
+      FRAME_-203126_CENTER          = -203
+      TKFRAME_-203126_RELATIVE      = 'DAWN_FC2'
+      TKFRAME_-203126_SPEC          = 'ANGLES'
+      TKFRAME_-203126_UNITS         = 'DEGREES'
+      TKFRAME_-203126_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203126_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC2_FILTER_7       = -203127
+      FRAME_-203127_NAME            = 'DAWN_FC2_FILTER_7'
+      FRAME_-203127_CLASS           = 4
+      FRAME_-203127_CLASS_ID        = -203127
+      FRAME_-203127_CENTER          = -203
+      TKFRAME_-203127_RELATIVE      = 'DAWN_FC2'
+      TKFRAME_-203127_SPEC          = 'ANGLES'
+      TKFRAME_-203127_UNITS         = 'DEGREES'
+      TKFRAME_-203127_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203127_AXES          = ( 1,   2,   3   )
+
+      FRAME_DAWN_FC2_FILTER_8       = -203128
+      FRAME_-203128_NAME            = 'DAWN_FC2_FILTER_8'
+      FRAME_-203128_CLASS           = 4
+      FRAME_-203128_CLASS_ID        = -203128
+      FRAME_-203128_CENTER          = -203
+      TKFRAME_-203128_RELATIVE      = 'DAWN_FC2'
+      TKFRAME_-203128_SPEC          = 'ANGLES'
+      TKFRAME_-203128_UNITS         = 'DEGREES'
+      TKFRAME_-203128_ANGLES        = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203128_AXES          = ( 1,   2,   3   )
+
+   \begintext
+
+
+VIR frames:
+========================================================================
+
+   This section of the file contains the definitions of the VIR frames.
+
+
+VIR Frame Tree
+--------------------------------------
+
+   The diagram below shows the VIR frame hierarchy.
+
+     "VESTA_IAU_2000"
+     ----------------
+           ^     
+           |<-dynamic
+           |
+           |  "DAWN_CLAUDIA"
+           |  --------------
+           |     ^
+           |     |<-dynamic
+           |     |
+           |     |      
+           |     |             "J2000" INERTIAL
+           +-----------------------------------------------------+
+           |                |         |                          |
+           |<-pck           |<-pck    |                          |<-pck
+           |                |         |                          |
+           V                V         |                          V
+      "VESTA_FIXED"    "IAU_VESTA"    |                    "CERES_FIXED"
+      -------------   -------------   |                    -------------
+                                      |
+                                      |<-ck
+                                      |
+                                      V
+                               "DAWN_SPACECRAFT"
+                               -----------------
+                                      |
+                                      |<-fixed
+                                      |
+                                      V
+                                  DAWN_VIR
+           +-----------------------------------------------------+
+           |                          |                          |
+           |<-fixed                   |<-ck                      |<-fixed
+           |                          |                          |
+           V                          V                          V
+      "DAWN_VIR_VIS_ZERO"       DAWN_VIR_SCAN          "DAWN_VIR_IR_ZERO"
+      -------------------    +-----------------+       ------------------
+                             |                 |
+                             |<-fixed          |<-fixed
+                             |                 |
+                             V                 V
+                      "DAWN_VIR_VIS"     "DAWN_VIR_IR"
+                      --------------     -------------
+
+
+VIR Frames
+--------------------------------------
+
+   The following frames are defined for VIR instrument:
+
+      -  the instrument base frame -- DAWN_VIR (ID -203200) -- is
+         defined as a fixed offset frame relative to the
+         DAWN_SPACECRAFT frame. It is intended to capture the
+         instrument base and scan mirror rotation axis alignment
+         relative to the spacecraft.
+ 
+      -  the reflected scan mirror view direction frame --
+         DAWN_VIR_SCAN (ID -203201) -- is defined as a CK-based frame
+         with its orientation provided in CK files relative to the
+         DAWN_VIR frame. It is intended to capture change in the
+         instrument view direction due to the scan mirror motion.
+ 
+      -  the reflected instrument detector view frames -- DAWN_VIR_VIS
+         (ID -203211) and DAWN_VIR_IR (ID -203213) -- are defined as
+         fixed offset frames relative to the DAWN_VIR_SCAN frame. They
+         are intended to capture reflected instrument boresights and
+         detector misalignments at any scan mirror position.
+ 
+      -  the non-moving instrument detector view frames -- DAWN_VIR_VIS_ZERO
+         (ID -203221) and DAWN_VIR_IR_ZERO (ID -203223) -- are defined as
+         fixed offset frames relative to the DAWN_VIR frame. They are
+         intended to capture instrument boresights and detector
+         misalignments at the "0" scan mirror position and are used for
+         defining FOVs corresponding the full (256-step) and partial
+         (128-, 64-, 16-, 96-, and 32-step) scan mirror sweeps.
+ 
+   The +Y axes of the base and scan mirror frames (DAWN_VIR and
+   DAWN_VIR_SCAN) are co-aligned with the scan mirror rotation axis.
+
+   The +Z axes of the reflected and non-moving instrument detector view
+   frames are in the direction of the instrument boresight at any (for
+   DAWN_VIR_VIS and DAWN_VIR_IR) or the "0" (for DAWN_VIR_VIS_ZERO and
+   DAWN_VIR_IR_ZERO) scan mirror position. The +Y axes of these frames
+   are in the direction of spatial resolution and the +X axes complete
+   the right-handed frames.
+   
+   Nominally, at the "0" scan mirror position all VIR frames are co-aligned 
+   with each other and with the s/c frame as shown on this diagram:
+
+
+   +Z s/c side (science deck side) view:
+   -------------------------------------
+
+                                   o-----> +Yvir*
+                             ._____|_______.
+                             |     |       |
+                             +Xvir*|       |
+                             |     V      +Ysc
+   o==/ /==================o |      o----->|o==================/ /==o
+     -Y Solar Array          |      |      |        +Y Solar Array
+                             |      |      |
+                             .______|______.
+                                 .--V +Xsc
+                          HGA  .'       `.
+                              /___________\
+                                  `.|.'                 +Zsc and +Zvir*
+                                                      are out of the page
+
+   The keywords below define the VIR frames. In this version of the FK 
+   all misalignments are set be zero.
+
+   Preliminary alignment data for VIR-VIS indicate that the instrument 
+   boresight (center pixel view direction) is tilted with respect to the 
+   spacecraft +Z axis by 1.50 milliradians toward -Y axis and 1.25 
+   milliradians toward +X. This misalignment is incorporated as a two 
+   rotations, first by +1.50 milliradians about +X axis and then by 
+   +1.25 milliradians about +Y axis, into the definitions of the 
+   DAWN_VIR_VIS and DAWN_VIR_VIS_ZERO frames.
+
+   Preliminary alignment data for VIR-IR indicate that the instrument 
+   boresight (center pixel view direction) is tilted with respect to the 
+   spacecraft +Z axis by 0.75 milliradians toward -Y axis and 1.50 
+   milliradians toward +X. This misalignment is incorporated as a two 
+   rotations, first by +0.75 milliradians about +X axis and then by 
+   +1.50 milliradians about +Y axis, into the definitions of the
+   DAWN_VIR_IR and DAWN_VIR_IR_ZERO frames.
+
+   \begindata
+
+      FRAME_DAWN_VIR                   =  -203200
+      FRAME_-203200_NAME               = 'DAWN_VIR'
+      FRAME_-203200_CLASS              =  4
+      FRAME_-203200_CLASS_ID           =  -203200
+      FRAME_-203200_CENTER             =  -203
+      TKFRAME_-203200_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203200_SPEC             = 'ANGLES'
+      TKFRAME_-203200_UNITS            = 'DEGREES'
+      TKFRAME_-203200_ANGLES           = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203200_AXES             = ( 1,   2,   3   )
+
+      FRAME_DAWN_VIR_SCAN              = -203201
+      FRAME_-203201_NAME               = 'DAWN_VIR_SCAN'
+      FRAME_-203201_CLASS              =  3
+      FRAME_-203201_CLASS_ID           = -203201
+      FRAME_-203201_CENTER             = -203
+      CK_-203201_SCLK                  = -203
+      CK_-203201_SPK                   = -203
+
+      FRAME_DAWN_VIR_VIS               =  -203211
+      FRAME_-203211_NAME               = 'DAWN_VIR_VIS'
+      FRAME_-203211_CLASS              =  4
+      FRAME_-203211_CLASS_ID           =  -203211
+      FRAME_-203211_CENTER             =  -203
+      TKFRAME_-203211_RELATIVE         = 'DAWN_VIR_SCAN'
+      TKFRAME_-203211_SPEC             = 'ANGLES'
+      TKFRAME_-203211_UNITS            = 'DEGREES'
+      TKFRAME_-203211_ANGLES           = (-0.085943669, -0.071619724, 0.0)
+      TKFRAME_-203211_AXES             = ( 1,   2,   3   )
+
+      FRAME_DAWN_VIR_IR                =  -203213
+      FRAME_-203213_NAME               = 'DAWN_VIR_IR'
+      FRAME_-203213_CLASS              =  4
+      FRAME_-203213_CLASS_ID           =  -203213
+      FRAME_-203213_CENTER             =  -203
+      TKFRAME_-203213_RELATIVE         = 'DAWN_VIR_SCAN'
+      TKFRAME_-203213_SPEC             = 'ANGLES'
+      TKFRAME_-203213_UNITS            = 'DEGREES'
+      TKFRAME_-203213_ANGLES           = (-0.042971835, -0.085943669, 0.0)
+      TKFRAME_-203213_AXES             = ( 1,   2,   3   )
+
+      FRAME_DAWN_VIR_VIS_ZERO          = -203221
+      FRAME_-203221_NAME               = 'DAWN_VIR_VIS_ZERO'
+      FRAME_-203221_CLASS              =  4
+      FRAME_-203221_CLASS_ID           =  -203221
+      FRAME_-203221_CENTER             =  -203
+      TKFRAME_-203221_RELATIVE         = 'DAWN_VIR'
+      TKFRAME_-203221_SPEC             = 'ANGLES'
+      TKFRAME_-203221_UNITS            = 'DEGREES'
+      TKFRAME_-203221_ANGLES           = (-0.085943669, -0.071619724, 0.0)
+      TKFRAME_-203221_AXES             = ( 1,   2,   3   )
+
+      FRAME_DAWN_VIR_IR_ZERO           = -203223
+      FRAME_-203223_NAME               = 'DAWN_VIR_IR_ZERO'
+      FRAME_-203223_CLASS              =  4
+      FRAME_-203223_CLASS_ID           =  -203223
+      FRAME_-203223_CENTER             =  -203
+      TKFRAME_-203223_RELATIVE         = 'DAWN_VIR'
+      TKFRAME_-203223_SPEC             = 'ANGLES'
+      TKFRAME_-203223_UNITS            = 'DEGREES'
+      TKFRAME_-203223_ANGLES           = (-0.042971835, -0.085943669, 0.0)
+      TKFRAME_-203223_AXES             = ( 1,   2,   3   )
+
+   \begintext
+
+
+GRAND frames
+========================================================================
+
+   This section of the file contains the definitions of the GRAND
+   frames.
+
+
+GRAND Frame Tree
+--------------------------------------
+
+   The diagram below shows the GRAND frame hierarchy.
+
+     "VESTA_IAU_2000"
+     ----------------
+           ^     
+           |<-dynamic
+           |
+           |  "DAWN_CLAUDIA"
+           |  --------------
+           |     ^
+           |     |<-dynamic
+           |     |
+           |     |      
+           |     |             "J2000" INERTIAL
+           +-----------------------------------------------------+
+           |                |         |                          |
+           |<-pck           |<-pck    |                          |<-pck
+           |                |         |                          |
+           V                V         |                          V
+      "VESTA_FIXED"    "IAU_VESTA"    |                    "CERES_FIXED"
+      -------------   -------------   |                    -------------
+                                      |
+                                      |<-ck
+                                      |
+                                      V
+                               "DAWN_SPACECRAFT"
+           +-----------------------------------------------------+
+           |
+           |<-fixed
+           |
+           V
+     "DAWN_GRAND"
+     ------------
+
+
+GRAND Frame
+--------------------------------------
+
+   The GRAND frame is defined as follows:
+
+      -  +Z axis is nominally co-aligned with the s/c +Z axis;
+
+      -  +Y axis is nominally co-aligned with the s/c +Y axis;
+
+      -  +X axis completes the right handed frame; it is nominally
+         co-aligned with the s/c +X axis;
+
+      -  the origin of the frame is located at the instrument "FOV"
+         vertex.
+
+   This diagram illustrates the GRAND frame:
+
+
+   +Z s/c side (science deck side) view:
+   -------------------------------------
+
+                             ._____________.
+                             |             |
+                             |             |
+                             |  +Zsc    +Ysc
+   o==/ /==================o |      o----->|o==================/ /==o
+     -Y Solar Array     +Xgrand     |      |        +Y Solar Array
+                             |o-----> +Ygrand
+                             .|_____|______.
+                              |  .--V +Xsc
+                              | '       `.
+                              V __________\
+                        +Xgrand   `.|.'                 +Zsc and +Zgrand
+                                      HGA                   are out
+                                                          of the page
+
+   Nominally, the GRAND frame is co-aligned with the s/c frame.
+
+   \begindata
+
+      FRAME_DAWN_GRAND                 =  -203300
+      FRAME_-203300_NAME               = 'DAWN_GRAND'
+      FRAME_-203300_CLASS              =  4
+      FRAME_-203300_CLASS_ID           =  -203300
+      FRAME_-203300_CENTER             =  -203
+      TKFRAME_-203300_RELATIVE         = 'DAWN_SPACECRAFT'
+      TKFRAME_-203300_SPEC             = 'ANGLES'
+      TKFRAME_-203300_UNITS            = 'DEGREES'
+      TKFRAME_-203300_ANGLES           = ( 0.0, 0.0, 0.0 )
+      TKFRAME_-203300_AXES             = ( 1,   2,   3   )
+
+   \begintext
+
+
+Dawn Mission NAIF ID Codes -- Definition Section
+========================================================================
+
+   This section contains name to NAIF ID mappings for the Dawn mission.
+
+
+Dawn Target IDs:
+-------------------------------------------------------------
+
+   This table summarizes Dawn Target IDs:
+
+            Name                   ID       Synonyms
+            ---------------------  -------  ---------------------------
+            VESTA                  2000004  '4 VESTA'
+            CERES                  2000001  '1 CERES'
+
+   Name-ID Mapping keywords:
+
+         \begindata
+
+            NAIF_BODY_NAME += ( '4 VESTA' )
+            NAIF_BODY_CODE += ( 2000004 )
+
+            NAIF_BODY_NAME += ( 'VESTA' )
+            NAIF_BODY_CODE += ( 2000004 )
+
+            NAIF_BODY_NAME += ( '1 CERES' )
+            NAIF_BODY_CODE += ( 2000001 )
+
+            NAIF_BODY_NAME += ( 'CERES' )
+            NAIF_BODY_CODE += ( 2000001 )
+
+         \begintext
+
+
+Dawn Spacecraft ID
+-------------------------------------------------------------
+
+   This table summarizes Dawn Spacecraft IDs:
+
+            Name                   ID
+            ---------------------  -------
+            DAWN                   -203
+
+   Name-ID Mapping keywords:
+
+         \begindata
+
+            NAIF_BODY_NAME += ( 'DAWN' )
+            NAIF_BODY_CODE += ( -203 )
+
+         \begintext
+
+
+Dawn Spacecraft Structures IDs
+--------------------------------------
+
+   This table summarizes Dawn Spacecraft Structure IDs:
+
+            Name                   ID
+            ---------------------  -------
+            DAWN                   -203
+            DAWN_SPACECRAFT        -203000
+            DAWN_SA+Y              -203010
+            DAWN_SA+Y_GIMBAL       -203011
+            DAWN_SA+Y_C1           -203012
+            DAWN_SA+Y_C2           -203013
+            DAWN_SA+Y_C3           -203014
+            DAWN_SA+Y_C4           -203015
+            DAWN_SA-Y              -203020
+            DAWN_SA-Y_GIMBAL       -203021
+            DAWN_SA-Y_C1           -203022
+            DAWN_SA-Y_C2           -203023
+            DAWN_SA-Y_C3           -203024
+            DAWN_SA-Y_C4           -203025
+            DAWN_HGA               -203040
+            DAWN_LGA+Z             -203030
+            DAWN_LGA+X             -203050
+            DAWN_LGA-Z             -203060
+            DAWN_ST1               -203071
+            DAWN_ST2               -203072
+            DAWN_FT1               -203081
+            DAWN_FT2               -203082
+            DAWN_FT3               -203083
+
+   Name-ID Mapping keywords:
+
+         \begindata
+
+            NAIF_BODY_NAME += ( 'DAWN_SPACECRAFT' )
+            NAIF_BODY_CODE += ( -203000 )
+
+            NAIF_BODY_NAME += ( 'DAWN_SA+Y' )
+            NAIF_BODY_CODE += ( -203010 )
+
+            NAIF_BODY_NAME += ( 'DAWN_SA+Y_GIMBAL' )
+            NAIF_BODY_CODE += ( -203011 )
+
+            NAIF_BODY_NAME += ( 'DAWN_SA+Y_C1' )
+            NAIF_BODY_CODE += ( -203012 )
+
+            NAIF_BODY_NAME += ( 'DAWN_SA+Y_C2' )
+            NAIF_BODY_CODE += ( -203013 )
+
+            NAIF_BODY_NAME += ( 'DAWN_SA+Y_C3' )
+            NAIF_BODY_CODE += ( -203014 )
+
+            NAIF_BODY_NAME += ( 'DAWN_SA+Y_C4' )
+            NAIF_BODY_CODE += ( -203015 )
+
+            NAIF_BODY_NAME += ( 'DAWN_SA-Y' )
+            NAIF_BODY_CODE += ( -203020 )
+
+            NAIF_BODY_NAME += ( 'DAWN_SA-Y_GIMBAL' )
+            NAIF_BODY_CODE += ( -203021 )
+
+            NAIF_BODY_NAME += ( 'DAWN_SA-Y_C1' )
+            NAIF_BODY_CODE += ( -203022 )
+
+            NAIF_BODY_NAME += ( 'DAWN_SA-Y_C2' )
+            NAIF_BODY_CODE += ( -203023 )
+
+            NAIF_BODY_NAME += ( 'DAWN_SA-Y_C3' )
+            NAIF_BODY_CODE += ( -203024 )
+
+            NAIF_BODY_NAME += ( 'DAWN_SA-Y_C4' )
+            NAIF_BODY_CODE += ( -203025 )
+
+            NAIF_BODY_NAME += ( 'DAWN_HGA' )
+            NAIF_BODY_CODE += ( -203040 )
+
+            NAIF_BODY_NAME += ( 'DAWN_LGA+Z' )
+            NAIF_BODY_CODE += ( -203030 )
+
+            NAIF_BODY_NAME += ( 'DAWN_LGA+X' )
+            NAIF_BODY_CODE += ( -203050 )
+
+            NAIF_BODY_NAME += ( 'DAWN_LGA-Z' )
+            NAIF_BODY_CODE += ( -203060 )
+
+            NAIF_BODY_NAME += ( 'DAWN_ST1' )
+            NAIF_BODY_CODE += ( -203071 )
+
+            NAIF_BODY_NAME += ( 'DAWN_ST2' )
+            NAIF_BODY_CODE += ( -203072 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FT1' )
+            NAIF_BODY_CODE += ( -203081 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FT2' )
+            NAIF_BODY_CODE += ( -203082 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FT3' )
+            NAIF_BODY_CODE += ( -203083 )
+
+         \begintext
+
+
+FC1 and FC2 IDs
+--------------------------------------
+
+   This table summarizes FC1 and FC2 IDs:
+
+            Name                   ID
+            ---------------------  -------
+            DAWN_FC1               -203110
+            DAWN_FC1_FILTER_1      -203111
+            DAWN_FC1_FILTER_2      -203112
+            DAWN_FC1_FILTER_3      -203113
+            DAWN_FC1_FILTER_4      -203114
+            DAWN_FC1_FILTER_5      -203115
+            DAWN_FC1_FILTER_6      -203116
+            DAWN_FC1_FILTER_7      -203117
+            DAWN_FC1_FILTER_8      -203118
+            DAWN_FC1_RAD           -203119
+
+            DAWN_FC2               -203120
+            DAWN_FC2_FILTER_1      -203121
+            DAWN_FC2_FILTER_2      -203122
+            DAWN_FC2_FILTER_3      -203123
+            DAWN_FC2_FILTER_4      -203124
+            DAWN_FC2_FILTER_5      -203125
+            DAWN_FC2_FILTER_6      -203126
+            DAWN_FC2_FILTER_7      -203127
+            DAWN_FC2_FILTER_8      -203128
+            DAWN_FC2_RAD           -203129
+
+   Name-ID Mapping keywords:
+
+         \begindata
+
+            NAIF_BODY_NAME += ( 'DAWN_FC1' )
+            NAIF_BODY_CODE += ( -203110 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_1' )
+            NAIF_BODY_CODE += ( -203111 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_2' )
+            NAIF_BODY_CODE += ( -203112 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_3' )
+            NAIF_BODY_CODE += ( -203113 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_4' )
+            NAIF_BODY_CODE += ( -203114 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_5' )
+            NAIF_BODY_CODE += ( -203115 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_6' )
+            NAIF_BODY_CODE += ( -203116 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_7' )
+            NAIF_BODY_CODE += ( -203117 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC1_FILTER_8' )
+            NAIF_BODY_CODE += ( -203118 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC1_RAD' )
+            NAIF_BODY_CODE += ( -203119 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC2' )
+            NAIF_BODY_CODE += ( -203120 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_1' )
+            NAIF_BODY_CODE += ( -203121 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_2' )
+            NAIF_BODY_CODE += ( -203122 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_3' )
+            NAIF_BODY_CODE += ( -203123 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_4' )
+            NAIF_BODY_CODE += ( -203124 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_5' )
+            NAIF_BODY_CODE += ( -203125 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_6' )
+            NAIF_BODY_CODE += ( -203126 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_7' )
+            NAIF_BODY_CODE += ( -203127 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC2_FILTER_8' )
+            NAIF_BODY_CODE += ( -203128 )
+
+            NAIF_BODY_NAME += ( 'DAWN_FC2_RAD' )
+            NAIF_BODY_CODE += ( -203129 )
+
+         \begintext
+
+
+VIR IDs
+--------------------------------------
+
+   This table summarizes VIR IDs:
+
+            Name                   ID
+            ---------------------  -------
+            DAWN_VIR               -203200
+            DAWN_VIR_SCAN          -203201
+            DAWN_VIR_VIS           -203211
+            DAWN_VIR_IR            -203213
+            DAWN_VIR_VIS_SCAN      -203212
+            DAWN_VIR_IR_SCAN       -203214
+            DAWN_VIR_VIS_128       -203215
+            DAWN_VIR_VIS_64        -203216
+            DAWN_VIR_VIS_16        -203217
+            DAWN_VIR_VIS_96        -203218
+            DAWN_VIR_VIS_32        -203219
+            DAWN_VIR_RAD           -203209
+
+   Name-ID Mapping keywords:
+
+         \begindata
+
+            NAIF_BODY_NAME += ( 'DAWN_VIR' )
+            NAIF_BODY_CODE += ( -203200 )
+
+            NAIF_BODY_NAME += ( 'DAWN_VIR_SCAN' )
+            NAIF_BODY_CODE += ( -203201 )
+
+            NAIF_BODY_NAME += ( 'DAWN_VIR_VIS' )
+            NAIF_BODY_CODE += ( -203211 )
+
+            NAIF_BODY_NAME += ( 'DAWN_VIR_IR' )
+            NAIF_BODY_CODE += ( -203213 )
+
+            NAIF_BODY_NAME += ( 'DAWN_VIR_VIS_SCAN' )
+            NAIF_BODY_CODE += ( -203212 )
+
+            NAIF_BODY_NAME += ( 'DAWN_VIR_IR_SCAN' )
+            NAIF_BODY_CODE += ( -203214 )
+
+            NAIF_BODY_NAME += ( 'DAWN_VIR_VIS_128' )
+            NAIF_BODY_CODE += ( -203215 )
+
+            NAIF_BODY_NAME += ( 'DAWN_VIR_VIS_64' )
+            NAIF_BODY_CODE += ( -203216 )
+
+            NAIF_BODY_NAME += ( 'DAWN_VIR_VIS_16' )
+            NAIF_BODY_CODE += ( -203217 )
+
+            NAIF_BODY_NAME += ( 'DAWN_VIR_VIS_96' )
+            NAIF_BODY_CODE += ( -203218 )
+
+            NAIF_BODY_NAME += ( 'DAWN_VIR_VIS_32' )
+            NAIF_BODY_CODE += ( -203219 )
+
+            NAIF_BODY_NAME += ( 'DAWN_VIR_RAD' )
+            NAIF_BODY_CODE += ( -203209 )
+
+         \begintext
+
+
+GRAND IDs
+--------------------------------------
+
+   This table summarizes GRAND IDs:
+
+            Name                   ID
+            ---------------------  -------
+            DAWN_GRAND             -203300
+
+   Name-ID Mapping keywords:
+
+         \begindata
+
+            NAIF_BODY_NAME += ( 'DAWN_GRAND' )
+            NAIF_BODY_CODE += ( -203300 )
+
+         \begintext
+
+
+Dawn DSK Surface NAIF Names/ID Codes -- Definition Section
+========================================================================
+
+   This section contains name to NAIF ID mappings for the Vesta and 
+   Ceres DSK surfaces.
+
+   The following surface name-ID mappings are defined for Ceres:
+
+             Surface Name          Surface ID     Body ID
+      ---------------------------  ----------  -------------
+      DAWN_DLR_SPG_135METER_V1       10101        2000001
+
+      DAWN_GRAV_SPC_0128ICQ_V1       20101        2000001
+      DAWN_GRAV_SPC_0256ICQ_V1       20102        2000001
+      DAWN_GRAV_SPC_0512ICQ_V1       20103        2000001
+      DAWN_GRAV_SPC_1024ICQ_V1       20104        2000001
+      DAWN_GRAV_SPC_300METER_V1      20105        2000001
+      DAWN_GRAV_SPC_100METER_V1      20106        2000001
+      DAWN_GRAV_SPC_035METER_V1      20107        2000001
+      DAWN_GRAV_SPC_0128ICQ_V2       20108        2000001
+      DAWN_GRAV_SPC_0256ICQ_V2       20109        2000001
+      DAWN_GRAV_SPC_0512ICQ_V2       20110        2000001
+      DAWN_GRAV_SPC_1024ICQ_V2       20111        2000001
+
+
+   \begindata
+
+      NAIF_SURFACE_NAME += 'DAWN_DLR_SPG_135METER_V1'
+      NAIF_SURFACE_CODE += 10101
+      NAIF_SURFACE_BODY += 2000001
+
+      NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_0128ICQ_V1'
+      NAIF_SURFACE_CODE += 20101
+      NAIF_SURFACE_BODY += 2000001
+
+      NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_0256ICQ_V1'
+      NAIF_SURFACE_CODE += 20102
+      NAIF_SURFACE_BODY += 2000001
+
+      NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_0512ICQ_V1'
+      NAIF_SURFACE_CODE += 20103
+      NAIF_SURFACE_BODY += 2000001
+
+      NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_1024ICQ_V1'
+      NAIF_SURFACE_CODE += 20104
+      NAIF_SURFACE_BODY += 2000001
+
+      NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_300METER_V1'
+      NAIF_SURFACE_CODE += 20105
+      NAIF_SURFACE_BODY += 2000001
+
+      NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_100METER_V1'
+      NAIF_SURFACE_CODE += 20106
+      NAIF_SURFACE_BODY += 2000001
+
+      NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_035METER_V1'
+      NAIF_SURFACE_CODE += 20107
+      NAIF_SURFACE_BODY += 2000001
+
+      NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_0128ICQ_V2'
+      NAIF_SURFACE_CODE += 20108
+      NAIF_SURFACE_BODY += 2000001
+
+      NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_0256ICQ_V2'
+      NAIF_SURFACE_CODE += 20109
+      NAIF_SURFACE_BODY += 2000001
+
+      NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_0512ICQ_V2'
+      NAIF_SURFACE_CODE += 20110
+      NAIF_SURFACE_BODY += 2000001
+
+      NAIF_SURFACE_NAME += 'DAWN_GRAV_SPC_1024ICQ_V2'
+      NAIF_SURFACE_CODE += 20111
+      NAIF_SURFACE_BODY += 2000001
+
+   \begintext
+
+
+End of FK.
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v00.tf b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v00.tf
new file mode 100755
index 0000000..4160703
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v00.tf
@@ -0,0 +1,93 @@
+KPL/FK
+
+Dawn Frames Kernel for Asteroid Vesta
+========================================================================
+
+   This frame kernel contains definition of the body-fixed frame for 
+   asteroid Vesta.
+
+
+Version and Date
+========================================================================
+ 
+   Version 0.0 -- May 9, 2005 -- Boris Semenov, NAIF
+
+      Preliminary Version.
+
+
+References
+========================================================================
+
+   1. ``Frames Required Reading''
+
+   2. ``Kernel Pool Required Reading''
+
+   3. ``PC-Kernel Required Reading''
+
+
+Contact Information
+========================================================================
+
+   Boris V. Semenov, NAIF/JPL, (818)-354-8136, boris.semenov@jpl.nasa.gov
+
+
+Implementation Notes
+========================================================================
+
+   This file is used by the SPICE system as follows: programs that make
+   use of this frame kernel must `load' the kernel, normally during
+   program initialization. The SPICELIB routine FURNSH and CSPICE
+   function furnsh_c load a kernel file into the kernel pool as shown
+   below.
+
+      CALL FURNSH ( 'frame_kernel_name' )
+      furnsh_c    ( "frame_kernel_name" );
+
+   This file was created and may be updated with a text editor or word
+   processor.
+
+
+Dawn Frames
+========================================================================
+
+   The following Dawn frames are defined in this kernel file:
+
+           Name                  Relative to           Type       NAIF ID
+      ======================  ===================  ============   =======
+
+   Dawn Target frames:
+   -------------------
+      VESTA_FIXED             J2000                PCK            2000004
+
+
+Dawn Target Frames
+========================================================================
+
+   This section of the file contains the body-fixed frame definition
+   for one of the Dawn mission targets -- asteroids 4 Vesta.
+
+   A body-fixed frame is defined for Vesta using standard body-fixed,
+   PCK-based frame formation rules:
+   
+      -  +Z axis is toward the North pole;
+
+      -  +X axis is toward the prime meridian;
+
+      -  +Y axis 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 the PCK file(s).
+
+   \begindata
+
+      FRAME_VESTA_FIXED                =  2000004
+      FRAME_2000004_NAME               = 'VESTA_FIXED'
+      FRAME_2000004_CLASS              =  2
+      FRAME_2000004_CLASS_ID           =  2000004
+      FRAME_2000004_CENTER             =  2000004
+      OBJECT_2000004_FRAME             = 'VESTA_FIXED'
+
+   \begintext
+
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v06.tpc b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v06.tpc
new file mode 100755
index 0000000..d9bc466
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vesta_v06.tpc
@@ -0,0 +1,306 @@
+KPL/PCK
+
+\beginlabel
+PDS_VERSION_ID               = PDS3
+RECORD_TYPE                  = STREAM
+RECORD_BYTES                 = "N/A"
+^SPICE_KERNEL                = "dawn_vesta_v06.tpc"
+MISSION_NAME                 = "DAWN MISSION TO VESTA AND CERES"
+SPACECRAFT_NAME              = DAWN
+DATA_SET_ID                  = "DAWN-M/A-SPICE-6-V1.0"
+KERNEL_TYPE_ID               = PCK
+PRODUCT_ID                   = "dawn_vesta_v06.tpc"
+PRODUCT_CREATION_TIME        = 2012-09-27T14:04:32
+PRODUCER_ID                  = "NAIF/JPL"
+MISSION_PHASE_NAME           = {
+                               "INITIAL CHECKOUT (ICO)",
+                               "EARTH-MARS CRUISE (EMC)",
+                               "MARS GRAVITY ASSIST (MGA)",
+                               "MARS-VESTA CRUISE (MVC)",
+                               "VESTA ENCOUNTER",
+                               "VESTA-CERES CRUISE (VCC)",
+                               "CERES ENCOUNTER",
+                               "END OF MISSION"
+                               }
+PRODUCT_VERSION_TYPE         = ACTUAL
+PLATFORM_OR_MOUNTING_NAME    = "N/A"
+START_TIME                   = "N/A"
+STOP_TIME                    = "N/A"
+SPACECRAFT_CLOCK_START_COUNT = "N/A"
+SPACECRAFT_CLOCK_STOP_COUNT  = "N/A"
+TARGET_NAME                  = {
+                               "4 VESTA",
+                               "1 CERES"
+                               }
+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 PCK file containing constants for
+Vesta, created by NAIF, JPL. Vesta rotation constants provided in this PCK
+are for the ``Claudia Double-Prime'' coordinate system used in science
+products included in the DAWN Vesta mission PDS archives. "
+END_OBJECT                   = SPICE_KERNEL
+\endlabel
+
+
+Asteroid Vesta P_constants (PcK) SPICE kernel file
+===========================================================================
+ 
+ 
+Organization
+--------------------------------------------------------
+ 
+     The sections of this file are as follows.
+ 
+     Introductory Information:
+ 
+         --   Version description
+ 
+         --   Disclaimer
+ 
+         --   Sources
+ 
+     Pck Data:
+ 
+         --   Orientation constants for asteroid Vesta
+ 
+         --   Radii for asteroid Vesta
+
+
+Version description
+--------------------------------------------------------
+
+     Version 0.6 -- October 20, 2012 -- Dr. Carol Raymond, DAWN Deputy PI,
+                                        Boris Semenov, NAIF
+
+        Corrected the Claudia center longitudes provided in the comment
+        sections ``Values in the Version 0.5'' (136.7 -> 136.0) and
+        ``Values in the Version 0.6'' (146.7 -> 146.0) *WITHOUT*
+        changing the file version or file name.
+
+                    September 5, 2012  -- Dr. Carol Raymond, DAWN Deputy PI,
+                                  Dr. Steven Joy, Dawn Science Center Manager,
+                                  Boris Semenov, NAIF
+
+        Corrected W0 (295.39 -> 285.39). 
+
+     Version 0.5 -- May 2, 2012  -- Dr. Carol Raymond, DAWN Deputy PI,
+                                  Dr. Steven Joy, Dawn Science Center Manager,
+                                  Boris Semenov, NAIF
+
+        Corrected W0 (75.39 -> 295.39). 
+ 
+     Version 0.4 -- November 2, 2011 -- Dr. Carol Raymond, DAWN Deputy PI,
+                                        Boris Semenov, NAIF
+
+        Corrected W0 (76.06 -> 75.39). 
+
+     Version 0.3 -- September 29, 2011 -- Dr. Carol Raymond, DAWN Deputy PI,
+                                          Boris Semenov, NAIF
+
+        Per MCR-112436 Vesta pole orientation and prime meridian 
+        (Ra, Dec, W0) were changed to (309.031, 42.235, 76.06) degrees 
+
+     Version 0.2 -- February 25, 2011 -- Boris Semenov, NAIF
+
+        Vesta pole orientation (Ra, Dec) was changed to (305.8, 41.4)
+        degrees per MCR-111475 and "Dawn Planetary Constants and Models
+        Document" Revision 2.0, Feb 16, 2011
+
+     Version 0.1 -- October 12, 2004 -- Boris Semenov, NAIF
+
+        VESTA_FIXED frame definition was removed. It is now in the DAWN
+        Frames Kernel file.
+
+     Version 0.0 -- October 6, 2003 -- Boris Semenov, NAIF
+     
+        This is a preliminary PCK containing draft values for the pole
+        direction, prime meridian location, rotation period and shape
+        (from [1].)
+     
+ 
+Disclaimer
+--------------------------------------------------------
+ 
+     This constants file may not contain the parameter values that you
+     prefer. Note that this file may be readily modified by you or
+     anyone else. NAIF suggests that you inspect this file visually
+     before proceeding with any critical or extended data processing.
+ 
+     NAIF requests that you update the ``by line'' and date if you
+     modify the file.
+ 
+ 
+Sources
+--------------------------------------------------------
+ 
+     The sources for the constants listed in this and the earlier
+     versions of this file are:
+ 
+        1) Thomas, Peter C. et al. ``Vesta: Spin Pole, Size, and Shape
+           from HST Images.'' ICARUS 128, 1997. Article NO. IS975736. 
+           pp. 93-94.
+
+        2) "Dawn Planetary Constants and Models Document" Revision 2.0, 
+           Feb 16, 2011
+
+        3) Analysis of Data from Dawn's Survey Orbit, Sep 23, 2011.
+           (IOM attached to MCR-112436).
+
+
+Orientation constants for asteroid Vesta
+--------------------------------------------------------
+ 
+     The inertial reference frame for these constants is J2000; this is
+     the default reference frame for PCK orientation data.
+ 
+     The epoch of the constants is J2000; this is Julian ephemeris date
+     (JED) 2451545.0.
+ 
+     The NAIF integer code for Vesta is 2000004. See the NAIF_IDs
+     required reading for further information on NAIF integer codes.
+ 
+
+Values in the Versions 0.0 and 0.1
+
+     The pole direction, prime meridian location, and rotation period
+     in the versions 0.0 and 0.1 were set to the following values from
+     [1]:
+
+       "New data from the 1996 Hubble HST observations of Vesta allow a 
+        refinement of the pole solution to: RA = 301 deg, Dec = 41 deg,
+        +/- 5 deg. The prime meridian is now given by W = 292 deg +
+        1617.332776 deg * d; see Section 3a and Eq. 1. The new data,
+        and a scaling correction, change the fit radii to 289, 280,
+        229, +/- 5 km."
+
+
+Values in the Version 0.2
+
+     The pole direction, prime meridian location, and rotation period
+     in the version 0.2 were set to the following values from [2]:
+
+       "5.3 Vesta Pole and Prime Meridian
+
+        The Vesta pole and prime meridian values are shown below.
+
+        RA  Vesta = 305.8 +/- 3.1 deg      Right Ascension in EME2000 [25]
+        DEC Vesta = 41.4 +/- 1.5 deg       Declination in EME2000 [25]
+        W   Vesta = 292 + w * D deg        Prime Meridian
+        w   Vesta = 1617.332776 deg/day    Rotation rate
+
+
+        5.4 Vesta Shape Parameters
+
+        The Vesta shape is described as a triaxial ellipsoid with 
+        values 289, 280, 229 km [15] or as a sphere with a radius 
+        of 265 km [16]. ... 
+
+
+        9 References
+
+        ...
+        15. "Vesta: Spin Pole, Size, and Shape from HST Images", P. 
+            Thomas, et al., Icarus, v128, p88~94 (1997)."
+        16. "Impact Excavation on Asteroid 4 Vesta: Hubble Space 
+            Telescope Result", P. C. Thomas, et al, Science, 227, 
+            1492-1494, 1997.
+        ...
+        25. "Improved Measurement of Asteroid (4) Vesta's Rotational 
+            Axis Orientation", Jian-Yang Li, et al., Icarus, 211, 
+            528-534, 2010.."
+
+
+Values in the Version 0.3
+
+     The pole direction, prime meridian location, rotation period and
+     radii in this version are set to the following values from [3]:
+
+       "... 
+        The recommended new pole is:
+           -  RA: 309.031   Dec: 42.235
+           -  Error is estimated as +/-0.03deg 3-sigma
+
+        Data considered:
+           -  Konopoliv (Gravity)       309.029    42.225 
+           -  Preusker (DLR) Survey     309.031    42.235
+           -  OpNav                     309.025    42.245
+           -  NAV OD radio              309.025    42.247 
+
+        The rotation rate of Vesta was determined to be .222588677 +/-
+        .000000009 days/rev, which agrees very well with the weighted 
+        average of all previous determinations.
+        ...
+        A new prime meridian was chosen as defined by the small crater 
+        Claudia that is assigned a longitude of 356 deg East. This new system
+        was chosen because the old system was not well-defined and the
+        team wanted to make a clear distinction between the old and new
+        to avoid confusion. The offset between the old W0 (292) from
+        Thomas et al. (1997) and the new W0 (76.06) is about 144.06 deg."
+
+     These values are provided in the keywords below. The W1 was derived 
+     from .222588677 days/rev as follows:
+
+        W1 = 1 / 0.222588677 * 360 = 1617.3329428
+
+Values in the Version 0.4
+
+     The pole direction, rotation period, and radii in the version 0.4
+     are the same as in the version 0.3.
+
+     The W0 value is 75.39 deg (changed from 76.06 deg to match the
+     correct rotation rate while preserving the longitude of Claudia).
+     
+Values in the Version 0.5
+
+     The pole direction, rotation period, and radii in the version 0.5
+     are the same as in the previous version 0.4.
+
+     The W0 value is 295.39 deg (changed from 75.39 deg) so that the
+     prime meridian is roughly in the center of the feature originally
+     identified as Olbers and the Claudia crater is now defined to be at 
+     136.0 deg East.
+     
+        body2000004_pole_ra    = ( 309.031    0.0              0.0 )
+        body2000004_pole_dec   = (  42.235    0.0              0.0 )
+        body2000004_pm         = ( 295.39  1617.3329428        0.0 )
+
+
+Values in the Current Version 0.6
+
+     The pole direction, rotation period, and radii in the version 0.6
+     are the same as in the previous versions 0.4 and 0.5.
+
+     The W0 value is 285.39 deg (changed from 295.39 deg) to improve the
+     alignment of the prime meridian with the center of the albedo feature
+     originally identified as Olbers in the Hubble data, based on the 
+     analysis of P. Thomas and J.-Y. Li in July/August 2012. The center 
+     of Claudia crater is now defined to be at 146.0 deg East.
+
+     \begindata
+ 
+        BODY2000004_POLE_RA    = ( 309.031    0.0              0.0 )
+        BODY2000004_POLE_DEC   = (  42.235    0.0              0.0 )
+        BODY2000004_PM         = ( 285.39  1617.3329428        0.0 )
+
+     \begintext
+
+
+
+Radii for asteroid Vesta
+--------------------------------------------------------
+     
+     The Vesta radii from [2] are provided in the keyword below.
+
+     \begindata
+ 
+        BODY2000004_RADII      = ( 289.0  280.0  229.0  )
+ 
+     \begintext
+
+End of PCK file.
+
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_v05.ti b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_v05.ti
new file mode 100755
index 0000000..47e9755
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_v05.ti
@@ -0,0 +1,574 @@
+KPL/IK
+
+VIR Instrument kernel
+===========================================================================
+
+   This instrument kernel (I-kernel) contains Dawn VIR optics,
+   detector, and field-of-view parameters.
+
+
+Version and Date
+---------------------------------------------------------------------------
+
+   Version 0.5 -- March 2, 2011 -- Boris Semenov, NAIF
+
+     Rearranged comments and data blocks in the "FOV Definitions"
+     section to have all FOVs defined for full and partial scan mirror
+     sweeps described in a single comment block and defined in a
+     single data block to more clearly separate them from actual,
+     non-sweep FOV definitions.
+
+     NO CHANGES WERE MADE TO ANY KEYWORD VALUES. 
+
+   Version 0.4 -- October 7, 2009 -- Dr. Federico Tosi, INAF - IFSI
+                                     Boris Semenov, NAIF
+
+      Changed the reference frame for the full and partial VIS sweep
+      FOVs associated with IDs -203212, -203215 ... -203219 to
+      DAWN_VIR_VIS_ZERO.
+
+      Changed the reference frame for the full IR sweep FOV associated
+      with IDs -203214 to DAWN_VIR_IR_ZERO.
+
+      Replaced -226 with -203 in the keywords in the ``Platform ID''
+      section.
+
+      Replaced cross-track/along-track with along-slit/cross-slit
+      in all comments.
+
+      Filled in instrument description.
+
+   Version 0.3 -- July 3, 2009 -- Boris Semenov
+
+      Extended comments to cover partial VIS scan FOVs added by Steve
+      Joy.
+
+   Version 0.2T2 -- June 23, 2009 -- Steven Joy
+
+      Added FOVs for VIR_VIS_96 (-203218) and VIR_VIS_32 (-203219)
+
+   Version 0.2T -- April 09, 2009 -- Steven Joy
+
+      Added FOVs for VIR_VIS_16 (-203217)
+
+   Version 0.2 -- June 24, 2008 -- Steven Joy, DSC with Boris Semenov, NAIF/JPL
+
+      Added FOVs for VIR_VIS_128 (-203215) and VIR_VIS_64 (-203216).
+
+   Version 0.1 -- May 9, 2005 -- Boris Semenov, NAIF/JPL
+
+      Added radiator FOV.
+
+   Version 0.0 -- October 12, 2004 -- Boris Semenov, NAIF/JPL
+
+      Initial release.
+
+
+References
+---------------------------------------------------------------------------
+
+   1. ``Kernel Pool Required Reading''
+
+   2. ``C-kernel Required Reading''
+
+   3. VIR ICD/MICD, latest version as of 10/12/04
+
+   4. Dawn Frames Definition Kernel (FK), latest version.
+
+   5. VIR CDR Presentations
+
+   6. Rosetta VIRTIS Documentation (ROS-EST-RS-30015/EID B and RO-VIR-UM-001)
+
+   7. VIR Home Page http://www.ifsi-roma.inaf.it/vir/; accessed 10/07/09
+
+
+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. See [1] for details.
+
+   This file was created with, and can be updated with a text editor or
+   word processor.
+
+
+Conventions for Specifying Data
+--------------------------------------------------------
+
+   Data items are specified using ``keyword=value'' assignments [1].
+   All keywords referencing values in this I-kernel start with the
+   characters `INS' followed by the NAIF Dawn instrument ID code,
+   constructed using the spacecraft ID number (-226) followed by the
+   NAIF three digit ID number for VIR module. These IDs are defined in
+   [4] as follows:
+
+               Instrument name          ID
+               --------------------   -------
+               DAWN_VIR               -203200
+               DAWN_VIR_SCAN          -203201
+               DAWN_VIR_VIS           -203211
+               DAWN_VIR_IR            -203213
+
+               DAWN_VIR_VIS_SCAN      -203212 (*)
+               DAWN_VIR_IR_SCAN       -203214 (*)
+               DAWN_VIR_VIS_128       -203215 (*)
+               DAWN_VIR_VIS_64        -203216 (*)
+               DAWN_VIR_VIS_16        -203217 (*)
+               DAWN_VIR_VIS_96        -203218 (*)
+               DAWN_VIR_VIS_32        -203219 (*)
+
+               DAWN_VIR_RAD           -203209
+
+   (*) _SCAN, _128, _64, _16, _96 and _32 names/IDs are defined to
+       allow specifying FOVs circumscribing full or partial side scans
+       of the VIR scan mirror. These frames are used only for planning
+       purposes and have nothing to do with the real angular aperture
+       (FOV) of the VIR instrument.
+
+   The remainder of the keyword is an underscore character followed by
+   the unique name of the data item. For example, the focal length of
+   the VIR VIS optics is specified by
+
+               INS-203211_FOCAL_LENGTH
+
+   The upper bound on the length of all keywords is 32 characters.
+
+   If a keyword is included in more than one file, or if the same
+   keyword appears more than once within a single file, the last
+   assignment supersedes any earlier assignments.
+
+
+Overview
+--------------------------------------------------------
+
+   From [7]:
+
+      What is VIR?
+                
+      The Dawn mapping spectrometer VIR is a Visual and Infrared
+      Imaging Spectrometer that produces spectral images in the 0.25-1
+      mkm and 1-5 mkm ranges. VIR is a rebuild of the VIRTIS mapping
+      spectrometer on board the ESA Rosetta mission and it also derives
+      much design heritage from the Cassini VIMS spectrometer. The
+      design of the instrument fully accomplishes the mission's
+      scientific and measurement objectives with a simple
+      space-qualified low risk approach and high performance,
+      reliability, heritage and cost effectiveness.
+
+      Some technical details
+
+      VIR is a Visual and Infrared Imaging Spectrometer in a single
+      optical head. A Shafer telescope is mated to an Offner slit
+      spectrometer. Spectral images are formed on two matrix detectors
+      to cover the 0.25-1 mkm and 1-5 mkm ranges. The design uses a
+      dual arm optical and focal design with mapping ability to 5
+      mkm.The Dawn mapping spectrometer (VIR) is a rebuild of the
+      VIRTIS mapping spectrometer on board the ESA Rosetta mission with
+      an operational durations of 2y and flight time of 13y. The MS
+      spectrometer will only use the - M channel of VIRTIS, thus
+      allowing a great mass reduction. VIR also derives much of its
+      design from the Cassini VIMS spectrometer with an operational
+      lifetime of >4y and a mission life>10y.
+
+      VIR modules
+
+      The spectrometer consists of only three modules: the optical
+      system, 5.0 kg mass; the proximity electronics, 3.0 kg and 5 W;
+      the cryocooler including driving electronics, 1.3 kg and 12.6 W.
+      A mechanical and thermal mounting of 5.0 kg mass accommodates the
+      spectrometer subsystems. The optical system, which includes
+      foreoptics, dispersive elements, filters, focal plane assemblies
+      as well as the cryocooler and proximity electronics is a complete
+      re-build of the VIRTIS M instrument The data processing unit box
+      (DPU) is shared with the framing camera to save mass. The DPU
+      handles the data for both camera and spectrometer, compresses and
+      buffers them, and controls both the FCs and MS. Flight software
+      is based on Rosetta VIRTIS and ROLIS developments. The camera is
+      operated only when the spectrometer is not operating. As
+      VIRTIS-M, VIR does not use beam-splitters. Two different groove
+      densities are ruled on a single grating. The central part of the
+      grating (about 30% of the pupil) is ruled with a higher groove
+      density, which generate the higher spectral resolution needed in
+      the visible channel. The infrared channel utilizes the outer 70%
+      of the grating, which is ruled with a lower groove density. The
+      larger collecting area in the IR compensates for the lower solar
+      irradiance in this region. The visible detector array is based on
+      the Thomson-CSF type TH 7896 CCD detector. The IR detector used
+      in the MS is based on a bidimensional array of IR-sensitive
+      photovoltaic Mercury Cadmium Telluride coupled to silicon CMOS
+      multiplexer. This detector can operate at temperatures of the
+      order of 75 K. For this reason cryocoolers have to be used. The
+      calibration unit will make use of the cover, which -inside is
+      coated. It will diffuse the light coming from two internal
+      calibration lamps (one for the VISFPA and one for the IR-FPA),
+      calibrated at IAS.
+
+
+Mounting Alignment
+--------------------------------------------------------
+
+   Refer to the latest version of the Dawn Frames Definition Kernel
+   (FK) [4] for the VIR reference frame definitions and mounting
+   alignment information.
+
+
+Apparent FOV Layout
+--------------------------------------------------------
+
+   WARNING --- the description/diagram below have not been verified
+
+   This diagram illustrates the VIR apparent FOV layout for "zero"
+   scan mirror position in the corresponding reference frame.
+
+
+                                  ^ +Xvis
+                                  | +Xir
+        |                         |
+        | ~0.014 degrees          |
+        |                         |
+        v         Pixel 1         |      Pixel 256
+       ---              +---------|---------+
+        |       1 line  |         x-------------> +Yvis
+       ---              +-------------------+     +Yir
+        ^                   256 pixels/line
+        |
+                        |   ~3.67 degrees   |
+                        |<----------------->|
+                        |                   |      Boresight (+Z axis)
+                                                    is into the page
+
+
+   This diagram illustrates the VIR apparent FOV layout resulting from
+   a full, 256 step, +/- 1.83 degree scan mirror sweep about Y axis.
+   For partial scans of 16, 32, 64, 96, or 128 lines the cross-slit
+   FOV extent is proportionally decreased to 0.23, 0.46, 0.92, 1.38,
+   and 1.84 degrees correspondingly.
+
+
+                                  ^ +Xvis
+                                  | +Xir
+        |        Pixel 1,1        |
+       ---              *---------|---------+
+        ^               |         |         |
+        |  ~3.67        |         |         |
+        | degrees       |         |         |
+        |               |         |         |
+        |     256 lines |         x-------------> +Yvis
+        |     (each for |                   |     +Yir
+        |     a step in |                   |
+        |     scan seq.)|                   |
+        V               |                   |
+       ---              +-------------------+
+        |                  256 pixels/line
+
+
+                        |   ~3.67 degrees   |
+                        |<----------------->|
+                        |                   |      Boresight (+Z axis)
+                                                    is into the page
+
+
+Optical Parameters
+--------------------------------------------------------
+
+   The following VIR VIS and IR nominal first order optical parameters
+   are included in the data section below, from [6]:
+
+      -----------------------------------------------------------------
+             parameter            VIR/VIS        VIR/IR
+      -----------------------------------------------------------------
+      Focal Length, mm            152.0          152.0
+      f/ratio                     f/5.6          f/3.2
+      IFOV, rad/pixel
+          along-slit              0.00025        0.00025
+          cross-slit              0.00025        0.00025
+      Field of view (deg)
+          along-slit              3.6669         3.6669
+          cross-slit              0.0143         0.0143
+      Field of view (deg) - scan
+          along-slit              3.6669         3.6669
+          cross-slit              3.6669         3.6669
+      -----------------------------------------------------------------
+
+   The keywords below provide nominal values from the table above.
+   Angular size values in the keywords are given radians, with the
+   along-slit size being the first value and the cross-slit size
+   being the second value in each pair.
+
+      \begindata
+
+         INS-203211_FOCAL_LENGTH       = ( 152.0                )
+         INS-203211_F/RATIO            = (   5.6                )
+         INS-203211_FOV_ANGULAR_SIZE   = (   0.064000, 0.000250 )
+         INS-203211_IFOV               = (   0.000250, 0.000250 )
+
+         INS-203213_FOCAL_LENGTH       = ( 152.0                )
+         INS-203213_F/RATIO            = (   3.2                )
+         INS-203213_FOV_ANGULAR_SIZE   = (   0.064000, 0.000250 )
+         INS-203213_IFOV               = (   0.000250, 0.000250 )
+
+      \begintext
+
+
+Detector Parameters
+--------------------------------------------------------
+
+   The nominal VIR detector parameters from [6] are:
+
+      -----------------------------------------------------------------
+             parameter                VIR/VIS      VIR/IR
+      -----------------------------------------------------------------
+      Detector Array Size/Physical
+          along-slit                  508          270
+          cross-slit                 1024          436
+      Detector Array Size/Spatial
+          along-slit                  256 (1)      256 (2)
+          cross-slit                    1            1
+      Detector Array Center/Spatial
+          along-slit                  127.5        127.5
+          cross-slit                    0.5          0.5
+      Pixel Size, microns/Spatial
+          along-slit                   38 (3)       38
+          cross-slit                   38           38
+      -----------------------------------------------------------------
+
+   (1) VIS CCD pixels are 2x2 binned at detector level
+
+   (2) assuming IR reads out the same number of pixels as VIS
+
+   (3) size of a 2x2 binned pixel
+
+   The values are given in microns for PIXEL_SIZE keywords and in counts
+   for PIXEL_SAMPLES, PIXEL_LINES, and CENTER keywords.
+
+      \begindata
+
+         INS-203211_PIXEL_SIZE         = ( 38, 38 )
+         INS-203211_PIXEL_SAMPLES      = ( 256 )
+         INS-203211_PIXEL_LINES        = (   1 )
+         INS-203211_CCD_CENTER         = ( 127.5, 0.5 )
+
+         INS-203213_PIXEL_SIZE         = ( 38, 38 )
+         INS-203213_PIXEL_SAMPLES      = ( 256 )
+         INS-203213_PIXEL_LINES        = (   1 )
+         INS-203213_CCD_CENTER         = ( 127.5, 0.5 )
+
+      \begintext
+
+
+FOV Definitions
+---------------------------------------------------------------------------
+
+   This section contains definitions for the VIR FOVs. These
+   definitions are provided in a format required by the SPICE (CSPICE)
+   function GETFOV (getfov_c).
+
+   The set of assignments in the data section below defines the VIR VIS
+   and IR actual slit FOVs with respect to the corresponding moving
+   frames to be a rectangles with the corners defined by the first and
+   last pixels of the spatial line along +Y and the boresight along the
+   +Z axis. These FOV definitions use angular extent style
+   specification with the cross and along track angular sizes taken
+   from the ``Optics Parameters'' section above.
+
+      \begindata
+
+         INS-203211_FOV_FRAME                 = 'DAWN_VIR_VIS'
+         INS-203211_FOV_SHAPE                 = 'RECTANGLE'
+         INS-203211_BORESIGHT                 = (
+                                            0.000000     0.000000   152.000000
+                                                )
+         INS-203211_FOV_CLASS_SPEC            = 'ANGLES'
+         INS-203211_FOV_REF_VECTOR            = (
+                                            1.000000     0.000000     0.000000
+                                                )
+         INS-203211_FOV_REF_ANGLE             = ( 0.00716197 )
+         INS-203211_FOV_CROSS_ANGLE           = ( 1.83346494 )
+         INS-203211_FOV_ANGLE_UNITS           = 'DEGREES'
+
+
+         INS-203213_FOV_FRAME                 = 'DAWN_VIR_IR'
+         INS-203213_FOV_SHAPE                 = 'RECTANGLE'
+         INS-203213_BORESIGHT                 = (
+                                            0.000000     0.000000   152.000000
+                                                )
+         INS-203213_FOV_CLASS_SPEC            = 'ANGLES'
+         INS-203213_FOV_REF_VECTOR            = (
+                                            1.000000     0.000000     0.000000
+                                                )
+         INS-203213_FOV_REF_ANGLE             = ( 0.00716197 )
+         INS-203213_FOV_CROSS_ANGLE           = ( 1.83346494 )
+         INS-203213_FOV_ANGLE_UNITS           = 'DEGREES'
+
+      \begintext
+
+
+   The set of assignments in the data section below defines the VIR VIS
+   apparent FOVs resulting from a full, 256-step and partial 128-, 64-,
+   16-, 96-, and 32- step scan mirror sweeps about Y axis with respect
+   to the non-moving frame 'DAWN_VIR_VIS_ZERO' to be a rectangles with the
+   corners defined by the first and last pixels of the spatial line in
+   the first and last scan positions and the boresight along the +Z
+   axis. These FOV definitions use angular extent style specification
+   with the angular sizes taken from the ``Optics Parameters'' section
+   above.
+
+   Note that FOVs defined below are used only for planning purposes and 
+   have nothing to do with the real angular aperture (FOV) of the VIR 
+   instrument; therefore they should not be used to reproduce the geometry
+   of real VIR acquisitions.
+
+      \begindata
+
+         INS-203212_FOV_FRAME                 = 'DAWN_VIR_VIS_ZERO'
+         INS-203212_FOV_SHAPE                 = 'RECTANGLE'
+         INS-203212_BORESIGHT                 = (
+                                            0.000000     0.000000   152.000000
+                                                )
+         INS-203212_FOV_CLASS_SPEC            = 'ANGLES'
+         INS-203212_FOV_REF_VECTOR            = (
+                                            1.000000     0.000000     0.000000
+                                                )
+         INS-203212_FOV_REF_ANGLE             = ( 1.83346494 )
+         INS-203212_FOV_CROSS_ANGLE           = ( 1.83346494 )
+         INS-203212_FOV_ANGLE_UNITS           = 'DEGREES'
+
+
+         INS-203214_FOV_FRAME                 = 'DAWN_VIR_IR_ZERO'
+         INS-203214_FOV_SHAPE                 = 'RECTANGLE'
+         INS-203214_BORESIGHT                 = (
+                                            0.000000     0.000000   152.000000
+                                                )
+         INS-203214_FOV_CLASS_SPEC            = 'ANGLES'
+         INS-203214_FOV_REF_VECTOR            = (
+                                            1.000000     0.000000     0.000000
+                                                )
+         INS-203214_FOV_REF_ANGLE             = ( 1.83346494 )
+         INS-203214_FOV_CROSS_ANGLE           = ( 1.83346494 )
+         INS-203214_FOV_ANGLE_UNITS           = 'DEGREES'
+
+
+         INS-203215_FOV_FRAME                 = 'DAWN_VIR_VIS_ZERO'
+         INS-203215_FOV_SHAPE                 = 'RECTANGLE'
+         INS-203215_BORESIGHT                 = (
+                                            0.000000     0.000000   152.000000
+                                                )
+         INS-203215_FOV_CLASS_SPEC            = 'ANGLES'
+         INS-203215_FOV_REF_VECTOR            = (
+                                            1.000000     0.000000     0.000000
+                                                )
+         INS-203215_FOV_REF_ANGLE             = ( 0.91673247 )
+         INS-203215_FOV_CROSS_ANGLE           = ( 1.83346494 )
+         INS-203215_FOV_ANGLE_UNITS           = 'DEGREES'
+
+
+         INS-203216_FOV_FRAME                 = 'DAWN_VIR_VIS_ZERO'
+         INS-203216_FOV_SHAPE                 = 'RECTANGLE'
+         INS-203216_BORESIGHT                 = (
+                                            0.000000     0.000000   152.000000
+                                                )
+         INS-203216_FOV_CLASS_SPEC            = 'ANGLES'
+         INS-203216_FOV_REF_VECTOR            = (
+                                            1.000000     0.000000     0.000000
+                                                )
+         INS-203216_FOV_REF_ANGLE             = ( 0.45836624 )
+         INS-203216_FOV_CROSS_ANGLE           = ( 1.83346494 )
+         INS-203216_FOV_ANGLE_UNITS           = 'DEGREES'
+
+
+         INS-203217_FOV_FRAME                 = 'DAWN_VIR_VIS_ZERO'
+         INS-203217_FOV_SHAPE                 = 'RECTANGLE'
+         INS-203217_BORESIGHT                 = (
+                                            0.000000     0.000000   152.000000
+                                                )
+         INS-203217_FOV_CLASS_SPEC            = 'ANGLES'
+         INS-203217_FOV_REF_VECTOR            = (
+                                            1.000000     0.000000     0.000000
+                                                )
+         INS-203217_FOV_REF_ANGLE             = ( 0.11459156 )
+         INS-203217_FOV_CROSS_ANGLE           = ( 1.83346494 )
+         INS-203217_FOV_ANGLE_UNITS           = 'DEGREES'
+
+
+         INS-203218_FOV_FRAME                 = 'DAWN_VIR_VIS_ZERO'
+         INS-203218_FOV_SHAPE                 = 'RECTANGLE'
+         INS-203218_BORESIGHT                 = (
+                                            0.000000     0.000000   152.000000
+                                                )
+         INS-203218_FOV_CLASS_SPEC            = 'ANGLES'
+         INS-203218_FOV_REF_VECTOR            = (
+                                            1.000000     0.000000     0.000000
+                                                )
+         INS-203218_FOV_REF_ANGLE             = ( 0.68754935 )
+         INS-203218_FOV_CROSS_ANGLE           = ( 1.83346494 )
+         INS-203218_FOV_ANGLE_UNITS           = 'DEGREES'
+
+
+         INS-203219_FOV_FRAME                 = 'DAWN_VIR_VIS_ZERO'
+         INS-203219_FOV_SHAPE                 = 'RECTANGLE'
+         INS-203219_BORESIGHT                 = (
+                                            0.000000     0.000000   152.000000
+                                                )
+         INS-203219_FOV_CLASS_SPEC            = 'ANGLES'
+         INS-203219_FOV_REF_VECTOR            = (
+                                            1.000000     0.000000     0.000000
+                                                )
+         INS-203219_FOV_REF_ANGLE             = ( 0.22918312 )
+         INS-203219_FOV_CROSS_ANGLE           = ( 1.83346494 )
+         INS-203219_FOV_ANGLE_UNITS           = 'DEGREES'
+
+
+      \begintext
+
+
+Radiator Sun Avoidance FOV Definition
+--------------------------------------------------------
+
+   Sun avoidance for VIR radiator is 175 degree cone centered on
+   spacecraft -X axis [3].
+
+      \begindata
+
+         INS-203209_FOV_FRAME                 = 'DAWN_SPACECRAFT'
+         INS-203209_FOV_SHAPE                 = 'CIRCLE'
+         INS-203209_BORESIGHT                 = (
+                                           -1.000000     0.000000     0.000000
+                                                )
+         INS-203209_FOV_CLASS_SPEC            = 'ANGLES'
+         INS-203209_FOV_REF_VECTOR            = (
+                                            0.000000     1.000000     0.000000
+                                                )
+         INS-203209_FOV_REF_ANGLE             = ( 87.5 )
+         INS-203209_FOV_ANGLE_UNITS           = 'DEGREES'
+
+      \begintext
+
+
+Optical Distortion
+--------------------------------------------------------
+
+   [TBD]
+
+
+Platform ID
+---------------------------------------------------------------------------
+
+   This number is the NAIF instrument ID of the platform on which the
+   instrument mounted. All VIR components it is the spacecraft.
+
+      \begindata
+
+      INS-203200_PLATFORM_ID  = ( -203000 )
+      INS-203211_PLATFORM_ID  = ( -203000 )
+      INS-203213_PLATFORM_ID  = ( -203000 )
+
+      \begintext
+
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_zero_0_sliced_-203201.xc b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_zero_0_sliced_-203201.xc
new file mode 100644
index 0000000..ed21972
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawn_vir_zero_0_sliced_-203201.xc
@@ -0,0 +1,31 @@
+DAFETF NAIF DAF ENCODED TRANSFER FILE
+'DAF/CK  '
+'2'
+'6'
+'DAWN VIR ZERO OFFSET CK                                     '
+BEGIN_ARRAY 1 10
+'DAWN VIR ZERO OFFSET CK                 '
+'159E1065C3^A'
+'159E194B8A^A'
+'-319C1'
+'-319C0'
+'2'
+'1'
+10
+'1^1'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'0^0'
+'10000000001F14^-1'
+'159E1065C3^A'
+'159E194B8A^A'
+END_ARRAY 1 10
+TOTAL_ARRAYS 1
+ ~NAIF/SPC BEGIN COMMENTS~
+This CK is for testing with the image: /Users/astamile/testData/ale/dawnVIR/VIR_IR_1A_1_362681634_1_isis3.cub
+
+This CK was generated using the following command: {}
+ ~NAIF/SPC END COMMENTS~
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawnvirAddendum001.ti b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawnvirAddendum001.ti
new file mode 100755
index 0000000..e48d829
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/dawnvirAddendum001.ti
@@ -0,0 +1,22 @@
+\begindata
+
+ INS-203211_PIXEL_PITCH        = 0.038
+ INS-203211_BORESIGHT_SAMPLE  = 127.5
+ INS-203211_BORESIGHT_LINE    = 0.5
+
+ INS-203211_TRANSX  = (0.0, 0.0, 0.038)
+ INS-203211_TRANSY  = (0.0, 0.038, 0.0)
+ INS-203211_ITRANSS = (0.0, 0.0, 26.315789473684)
+ INS-203211_ITRANSL = (0.0, 26.315789473684, 0.0)
+
+ INS-203213_PIXEL_PITCH       = 0.038
+ INS-203213_BORESIGHT_SAMPLE  = 127.5
+ INS-203213_BORESIGHT_LINE    = 0.5
+
+ INS-203213_TRANSX  = (0.0, 0.0, 0.038)
+ INS-203213_TRANSY  = (0.0, 0.038, 0.0)
+ INS-203213_ITRANSS = (0.0, 0.0, 26.315789473684)
+ INS-203213_ITRANSL = (0.0, 26.315789473684, 0.0)
+
+\begintext
+
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/naif0012.tls b/tests/pytests/data/VIR_IR_1A_1_362681634_1/naif0012.tls
new file mode 100755
index 0000000..e1afdee
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/naif0012.tls
@@ -0,0 +1,152 @@
+KPL/LSK
+
+
+LEAPSECONDS KERNEL FILE
+===========================================================================
+
+Modifications:
+--------------
+
+2016, Jul. 14   NJB  Modified file to account for the leapsecond that
+                     will occur on December 31, 2016.
+
+2015, Jan. 5    NJB  Modified file to account for the leapsecond that
+                     will occur on June 30, 2015.
+
+2012, Jan. 5    NJB  Modified file to account for the leapsecond that
+                     will occur on June 30, 2012.
+                     
+2008, Jul. 7    NJB  Modified file to account for the leapsecond that
+                     will occur on December 31, 2008.
+                     
+2005, Aug. 3    NJB  Modified file to account for the leapsecond that
+                     will occur on December 31, 2005.
+                     
+1998, Jul  17   WLT  Modified file to account for the leapsecond that
+                     will occur on December 31, 1998.
+                     
+1997, Feb  22   WLT  Modified file to account for the leapsecond that
+                     will occur on June 30, 1997.
+                     
+1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
+                     to 1-1-96.
+
+1995, Oct  25   WLT  Modified file to account for the leapsecond that
+                     will occur on Dec 31, 1995.
+
+1994, Jun  16   WLT  Modified file to account for the leapsecond on
+                     June 30, 1994.
+
+1993, Feb. 22  CHA   Modified file to account for the leapsecond on
+                     June 30, 1993.
+
+1992, Mar. 6   HAN   Modified file to account for the leapsecond on
+                     June 30, 1992.
+
+1990, Oct. 8   HAN   Modified file to account for the leapsecond on 
+                     Dec. 31, 1990.  
+
+
+Explanation:
+------------
+
+The contents of this file are used by the routine DELTET to compute the 
+time difference
+
+[1]       DELTA_ET  =  ET - UTC                                         
+          
+the increment to be applied to UTC to give ET. 
+
+The difference between UTC and TAI,
+
+[2]       DELTA_AT  =  TAI - UTC
+
+is always an integral number of seconds. The value of DELTA_AT was 10
+seconds in January 1972, and increases by one each time a leap second
+is declared. Combining [1] and [2] gives
+
+[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)
+
+                    =  (ET - TAI) + DELTA_AT
+
+The difference (ET - TAI) is periodic, and is given by
+
+[4]       ET - TAI  =  DELTA_T_A  + K sin E 
+
+where DELTA_T_A and K are constant, and E is the eccentric anomaly of the 
+heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores 
+small-period fluctuations, is accurate to about 0.000030 seconds.
+
+The eccentric anomaly E is given by 
+
+[5]       E = M + EB sin M
+
+where M is the mean anomaly, which in turn is given by 
+
+[6]       M = M  +  M t
+               0     1
+
+where t is the number of ephemeris seconds past J2000.
+
+Thus, in order to compute DELTA_ET, the following items are necessary.
+
+          DELTA_TA
+          K
+          EB
+          M0
+          M1
+          DELTA_AT      after each leap second.
+
+The numbers, and the formulation, are taken from the following sources.
+
+     1) Moyer, T.D., Transformation from Proper Time on Earth to 
+        Coordinate Time in Solar System Barycentric Space-Time Frame
+        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
+        33-56 and 57-68.
+
+     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
+        Reference System on Algorithms for Computing Time Differences
+        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.
+
+The variable names used above are consistent with those used in the 
+Astronomical Almanac.
+
+\begindata
+
+DELTET/DELTA_T_A       =   32.184
+DELTET/K               =    1.657D-3
+DELTET/EB              =    1.671D-2
+DELTET/M               = (  6.239996D0   1.99096871D-7 )
+
+DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
+                           11,   @1972-JUL-1     
+                           12,   @1973-JAN-1     
+                           13,   @1974-JAN-1     
+                           14,   @1975-JAN-1          
+                           15,   @1976-JAN-1          
+                           16,   @1977-JAN-1          
+                           17,   @1978-JAN-1          
+                           18,   @1979-JAN-1          
+                           19,   @1980-JAN-1          
+                           20,   @1981-JUL-1          
+                           21,   @1982-JUL-1          
+                           22,   @1983-JUL-1          
+                           23,   @1985-JUL-1          
+                           24,   @1988-JAN-1 
+                           25,   @1990-JAN-1
+                           26,   @1991-JAN-1 
+                           27,   @1992-JUL-1
+                           28,   @1993-JUL-1
+                           29,   @1994-JUL-1
+                           30,   @1996-JAN-1 
+                           31,   @1997-JUL-1
+                           32,   @1999-JAN-1
+                           33,   @2006-JAN-1
+                           34,   @2009-JAN-1
+                           35,   @2012-JUL-1
+                           36,   @2015-JUL-1 
+                           37,   @2017-JAN-1 )
+
+\begintext
+
+
diff --git a/tests/pytests/data/VIR_IR_1A_1_362681634_1/pck00009.tpc b/tests/pytests/data/VIR_IR_1A_1_362681634_1/pck00009.tpc
new file mode 100755
index 0000000..bfadaab
--- /dev/null
+++ b/tests/pytests/data/VIR_IR_1A_1_362681634_1/pck00009.tpc
@@ -0,0 +1,3639 @@
+KPL/PCK
+ 
+
+P_constants (PcK) SPICE kernel file
+===========================================================================
+
+        By: Nat Bachman (NAIF)    2010 March 3
+ 
+ 
+Purpose
+--------------------------------------------------------
+
+     This file makes available for use in SPICE-based application
+     software orientation and size/shape data for natural bodies. The
+     principal source of the data is a published report by the IAU/IAG
+     Working Group on Cartographic Coordinates and Rotational Elements [1].
+
+     Orientation and size/shape data not provided by this file may be
+     available in mission-specific PCK files. Such PCKs may be the preferred
+     data source for mission-related applications. Mission-specific PCKs can
+     be found in PDS archives or on the NAIF web site at URL:
+
+        http://naif.jpl.nasa.gov
+
+
+File Organization
+--------------------------------------------------------
+ 
+     The contents of this file are as follows.
+ 
+     Introductory Information:
+
+         --   Purpose
+
+         --   File Organization
+ 
+         --   Version description
+ 
+         --   Disclaimer
+ 
+         --   Sources
+ 
+         --   Explanatory notes
+ 
+         --   Body numbers and names
+ 
+
+     PcK Data:
+ 
+
+        Orientation Data
+        ----------------
+
+         --   Orientation constants for the Sun and planets.        
+              Additional items included in this section:
+
+                 - Earth north geomagnetic centered dipole values
+                   for epochs 1945-2000
+
+                 - Mars prime meridian offset "lambda_a"
+
+         --   Orientation constants for satellites
+ 
+         --   Orientation constants for asteroids Eros, Gaspra, Ida,
+              Itokawa, and Vesta
+ 
+         --   Orientation constants for comets 19P/Borrelly
+              and 9P/Tempel 1
+
+
+        Radii of Bodies
+        ---------------
+
+         --   Radii of Sun and planets
+         
+         --   Radii of satellites, where available
+         
+         --   Radii of asteroids Ceres, Eros, Gaspra, Ida, Itokawa,
+              Mathilde, Toutatis, and Vesta.
+            
+         --   Radii of comets 19P/Borrelly, Halley, 9P/Tempel 1,
+              and 81P/Wild 2
+
+
+
+Version Description
+--------------------------------------------------------
+ 
+     This file was created on March 3, 2010. This version
+     incorporates data from reference [1].
+ 
+     This file contains size, shape, and orientation data for all
+     objects described by the previous version of the file, except
+     for Kleopatra: a shape model for this body is not provided in [1]
+     because, according to this source, it had been "modeled from
+     low resolution radar data, and cannot be mapped from those
+     data."
+
+     New objects covered by this file but not the previous
+     version are:
+        
+        19P/Borrelly
+        Halley
+        9P/Tempel 1
+        81P/Wild 2
+        Ceres
+        Itokawa
+        Mathilde
+        Toutatis
+                         
+ 
+Disclaimer
+--------------------------------------------------------
+ 
+Applicability of Data
+
+     This P_constants file may not contain the parameter values that
+     you prefer. NAIF suggests that you inspect this file visually
+     before proceeding with any critical or extended data processing.
+
+File Modifications by Users
+
+     Note that this file may be readily modified by you to change
+     values or add/delete parameters. NAIF requests that you update the
+     "by line," date, and version description section if you modify
+     this file.
+     
+Known Limitations and Caveats
+
+     Accuracy
+     --------
+
+     In general, the orientation models given here are claimed by the
+     IAU/IAG Working Group Report [1] to be accurate to 0.1 degree
+     ([1], p.158). However, NAIF notes that orientation models for
+     natural satellites and asteroids have in some cases changed
+     substantially with the availability of new observational data, so
+     users are urged to investigate the suitability for their
+     applications of the models presented here.
+
+     Earth orientation
+     -----------------
+
+     NAIF strongly cautions against using the earth rotation model
+     (from [1]) for work demanding high accuracy. This model has been
+     determined by NAIF to have an error in the prime meridian location
+     of magnitude at least 150 arcseconds, with a local minimum
+     occurring during the year 1999. Regarding availability of better
+     earth orientation data for use with the SPICE system:
+
+        Earth orientation data are available from NAIF in the form of
+        binary earth PCK files. NAIF employs an automated process to
+        create these files; each time JPL's Tracking Systems and
+        Applications Section produces a new earth orientation parameter
+        (EOP) file, a new PCK is produced. These PCKs cover a roughly
+        10 year time span starting at Jan. 1, 2000. In these PCK files,
+        the following effects are accounted for in modeling the earth's
+        rotation:
+
+           - Precession:                   1976 IAU model
+
+           - Nutation:                     1980 IAU model, plus interpolated
+                                           EOP nutation corrections
+
+           - Polar motion:                 interpolated from EOP file
+
+           - True sidereal time:
+
+                  UT1 - UT1R (if needed):  given by analytic formula
+                + TAI - UT1 (or UT1R):     interpolated from EOP file
+                + UT1 - GMST:              given by analytic formula
+                + equation of equinoxes:   given by analytic formula
+
+             where
+
+                TAI    =   International Atomic Time
+                UT1    =   Greenwich hour angle of computed mean sun - 12h
+                UT1R   =   Regularized UT1
+                GMST   =   Greenwich mean sidereal time                   
+
+        These kernels are available from the NAIF web site
+
+           http://naif.jpl.nasa.gov
+
+        (follow the links to Data, generic_kernels, and PCK data) or
+
+           ftp://naif.jpl.nasa.gov/pub/naif/generic_kernels/pck
+
+        or via anonymous ftp from the server
+ 
+           naif.jpl.nasa.gov
+
+        The kernels are in the path
+
+           pub/naif/generic_kernels/pck
+
+        At this time, these kernels have file names of the form
+
+           earth_000101_yymmdd_yymmdd.bpc
+
+        The second and third dates are, respectively, the file's 
+        coverage end time and the epoch of the last datum.
+ 
+        These binary PCK files are very accurate (error < 0.1
+        microradian) for epochs preceding the epoch of the last datum.
+        For later epochs, the error rises to several microradians.
+
+        Binary PCK files giving accurate earth orientation from 1972 to
+        2007 and *low accuracy* predicted earth orientation from
+        2007 to 2037 are also available in the same location. See the
+        aareadme.txt file at the "pck" URL above for details.
+
+        Characteristics and names of the binary kernels described here
+        are subject to change. See the "pck" URL above for information
+        on current binary earth PCKs.
+
+
+     Lunar orientation
+     -----------------
+
+     The lunar orientation formula provided by this file is a
+     trigonometric polynomial approximation yielding the orientation of
+     the lunar "Mean Earth/Polar Axis" (ME) reference frame. A more
+     accurate approximation can be obtained by using both the NAIF
+     lunar frame kernel and the binary lunar orientation PCK file,
+     which are available on the NAIF web site (see URLS above)
+     and in the NAIF server's ftp area. The lunar frame kernel
+     is located in the path
+
+        pub/naif/generic_kernels/fk/satellites
+
+     and has a name of the form
+
+        moon_yymmdd.tf
+
+     The binary lunar PCK is in the path
+
+        pub/naif/generic_kernels/pck
+
+     and has a name of the form
+
+        moon_pa_dennn_yyyy-yyyy.bpc
+
+     See the "aareadme.txt" files in the paths shown above for details
+     on file contents and versions. We also suggest you refer to the
+     SPICE tutorial named "lunar_earth_pck-fk," which is available from
+     the NAIF web site.
+
+
+     Earth geomagnetic dipole
+     ------------------------
+
+     The SPICE Toolkit doesn't currently contain software to model the
+     earth's north geomagnetic centered dipole as a function of time.
+     As a convenience for users, the north dipole location from the
+     J2000 epoch was selected as a representative datum, and the
+     planetocentric longitude and latitude of this location have been
+     associated with the keywords
+       
+        BODY399_N_GEOMAG_CTR_DIPOLE_LON
+        BODY399_N_GEOMAG_CTR_DIPOLE_LAT
+     
+     Values for the earth's north geomagnetic centered dipole are
+     presented in comments as a discrete time series for the time range
+     1945-2000. For details concerning the geomagnetic field model from
+     which these values were derived, including a discussion of the
+     model's accuracy, see [9].
+ 
+
+     Mars prime meridian offset
+     --------------------------
+
+     The Mars prime meridian offset given by [5] is not used by
+     SPICE geometry software for computations involving the shape
+     of Mars (for example, in sub-observer point or surface intercept
+     computations). The value is provided for informational
+     purposes only.
+
+
+     Software limitations
+     --------------------
+
+     SPICE Toolkits prior to version N0057 cannot make use of
+     trigonometric polynomial terms in the formulas for orientation of
+     the planets. The only planets for which such terms are used are
+     Jupiter and Neptune. Use of trigonometric polynomial terms for
+     natural satellites is and has been supported for all SPICE Toolkit
+     versions.
+ 
+     The second nutation precession angle (M2) for Mars is represented
+     by a quadratic polynomial in the 2006 IAU report. The SPICELIB
+     subroutine BODEUL can not handle this term (which is extremely
+     small), so we truncate the polynomial to a linear one. The 
+     resulting orientation error has a maximum magnitude of less
+     than 0.0032 degrees over the time span 1996-2015 and less than
+     0.0082 degrees over the time span 1986-2025.
+
+
+Sources
+--------------------------------------------------------
+ 
+     The sources for the constants listed in this file are:
+
+
+        [1]   Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F., 
+              Conrad, A., Consolmagno, G.J., Hestroffer, D.,
+              Hilton, J.L., Krasinsky, G.A., Neumann, G.,
+              Oberst, J., Stooke, P., Tedesco, E.F., Tholen, D.J., 
+              and Thomas, P.C. "Report of the IAU/IAG Working Group 
+              on cartographic coordinates and rotational elements: 2006."
+
+        [2]   Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F., 
+              Cruikshank, D.P., Hilton, J.L., Keller, H.U., Oberst, J.,
+              Simon, J.L., Stooke, P., Tholen, D.J., and Thomas, P.C.
+              "Report of the IAU/IAG Working Group on Cartographic
+              Coordinates and Rotational Elements of the Planets and
+              Satellites: 2003."
+ 
+        [3]   Nautical Almanac Office, United States Naval Observatory
+              and H.M. Nautical Almanac Office, Rutherford Appleton
+              Laboratory (2010). "The Astronomical Almanac for
+              the Year 2010," U.S. Government Printing Office,
+              Washington, D.C.: and The Stationary Office, London.
+
+        [4]   Nautical Almanac Office, United States Naval Observatory,
+              H.M. Nautical Almanac Office, Royal Greenwich
+              Observatory, Jet Propulsion Laboratory, Bureau des
+              Longitudes, and The Time Service and Astronomy
+              Departments, United States Naval Observatory (1992).
+              "Explanatory Supplement to the Astronomical Almanac," P.
+              Kenneth Seidelmann, ed. University Science Books, 20
+              Edgehill Road, Mill Valley, CA 9494.
+
+        [5]   Duxbury, Thomas C. (2001). "IAU/IAG 2000 Mars Cartographic
+              Conventions,"  presentation to the Mars Express Data
+              Archive Working Group, Dec. 14, 2001.
+
+        [6]   Russell, C.T. and Luhmann, J.G. (1990). "Earth: Magnetic 
+              Field and Magnetosphere." <http://www-ssc.igpp.ucla.
+              edu/personnel/russell/papers/earth_mag>. Originally
+              published in "Encyclopedia of Planetary Sciences," J.H.
+              Shirley and R.W. Fainbridge, eds. Chapman and Hall,
+              New York, pp 208-211.
+
+        [7]   Russell, C.T. (1971). "Geophysical Coordinate 
+              Transformations," Cosmic Electrodynamics 2  184-186.
+              NAIF document 181.0.
+     
+        [8]   ESA/ESTEC Space Environment Information System (SPENVIS)
+              (2003). Web page:  "Dipole approximations of the
+              geomagnetic field."  <http://www.spenvis.oma.be/spenvis/
+              help/background/magfield/cd.html>.
+ 
+        [9]   International Association of Geomagnetism and Aeronomy
+              and International Union of Geodesy and Geophysics (2004).
+              Web page:  "The 9th Generation International Geomagnetic
+              Reference Field." <http://www.ngdc.noaa.gov/
+              IAGA/vmod/igrf.html>.
+                             
+        [10]  Davies, M.E., Abalakin, V.K., Bursa, M., Hunt, G.E.,
+              and Lieske, J.H. (1989). "Report of the IAU/IAG/COSPAR
+              Working Group on Cartographic Coordinates and Rotational
+              Elements of the Planets and Satellites: 1988," Celestial
+              Mechanics and Dynamical Astronomy, v.46, no.2, pp.
+              187-204.
+
+         
+     Most values are from [1]. All exceptions are 
+     commented where they occur in this file. The exceptions are:
+ 
+                 
+         --   Radii for the Sun are from [3].
+             
+         --   The second nutation precession angle (M2) for Mars is
+              represented by a quadratic polynomial in the 2000
+              IAU report. The SPICELIB subroutine BODEUL can not
+              handle this term (which is extremely small), so we
+              truncate the polynomial to a linear one.
+           
+          --  Earth north geomagnetic centered dipole values are from
+              [8]. The article [6] was used to check most of 
+              these values, and the values were also re-computed from 
+              the 9th generation IGRF [9] by Nat Bachman.
+         
+          -- The Mars prime meridian offset angle is from [5].
+
+
+     "Old values" listed are from the SPICE P_constants file
+     pck00008.tpc dated September 21, 2004. Most of these values came
+     from the 2003 IAU report [2].
+ 
+ 
+ 
+ 
+Explanatory Notes
+--------------------------------------------------------
+
+     This file, which is logically part of the SPICE P-kernel, contains
+     constants used to model the orientation, size and shape of the
+     Sun, planets, natural satellites, and selected comets and
+     asteroids. The orientation models express the direction of the
+     pole and location of the prime meridian of a body as a function of
+     time. The size/shape models ("shape models" for short) represent
+     all bodies as ellipsoids, using two equatorial radii and a polar
+     radius. Spheroids and spheres are obtained when two or all three
+     radii are equal.
+
+     The SPICE Toolkit routines that use this file are documented in
+     the SPICE "Required Reading" file pck.req. They are also 
+     documented in the "PCK" SPICE tutorial, which is available on
+     the NAIF web site.
+
+File Format
+        
+     A terse description of the PCK file format is given here. See the
+     SPICE "Required Reading" files pck.req and kernel.req for a
+     detailed explanation of the SPICE text kernel file format. The
+     files pck.req and kernel.req are included in the documentation
+     provided with the SPICE Toolkit.
+
+     The file starts out with the ``ID word'' string
+
+        KPL/PCK
+
+     This string identifies the file as a text kernel containing PCK 
+     data.
+
+     This file consists of a series of comment blocks and data blocks.
+     Comment blocks, which contain free-form descriptive or explanatory
+     text, are preceded by a \begintext token. Data blocks follow a
+     \begindata token. In order to be recognized, each of these tokens
+     must be placed on a line by itself.
+
+     The portion of the file preceding the first data block is treated
+     as a comment block; it doesn't require an initial \begintext
+     token.
+
+     This file identifies data using a series of
+
+        KEYWORD = VALUE
+
+     assignments. The left hand side of each assignment is a
+     "kernel variable" name; the right hand side is an associated value
+     or list of values. The SPICE subroutine API allows SPICE routines
+     and user applications to retrieve the set of values associated
+     with each kernel variable name.
+
+     Kernel variable names are case-sensitive and are limited to
+     32 characters in length. 
+
+     Numeric values may be integer or floating point. String values
+     are normally limited to 80 characters in length; however, SPICE
+     provides a mechanism for identifying longer, "continued" strings.
+     See the SPICE routine STPOOL for details.
+
+     String values are single quoted.
+
+     When the right hand side of an assignment is a list of values,
+     the list items may be separated by commas or simply by blanks.
+     The list must be bracketed by parentheses. Example:
+
+        BODY399_RADII = ( 6378.14 6378.14 6356.75 )
+ 
+     Any blanks preceding or following keyword names, values and equal
+     signs are ignored.
+  
+     Assignments may be spread over multiple lines, for example:
+
+        BODY399_RADII = ( 6378.14 
+                          6378.14 
+                          6356.75 )
+
+     This file may contain blank lines anywhere. Non-printing
+     characters including TAB should not be present in the file: the
+     presence of such characters may cause formatting errors when the
+     file is viewed.
+
+Time systems and reference frames
+
+     The 2006 IAU/IAG Working Group Report [1] states the time scale
+     used as the independent variable for the rotation formulas is
+     Barycentric Dynamical Time (TDB) and that the epoch of variable
+     quantities is J2000 TDB (2000 Jan 1 12:00 TDB). Throughout SPICE
+     documentation and in this file, we use the names "J2000 TDB" and
+     "J2000" for this epoch. The name "J2000.0" is equivalent.
+
+     SPICE documentation refers to the time system used in this file 
+     as either "ET" or "TDB." SPICE software makes no distinction 
+     between TDB and the time system associated with the independent
+     variable of the JPL planetary ephemerides T_eph.
+ 
+     The inertial reference frame used for the rotational elements in
+     this file is identified by [1] as the ICRF (International
+     Celestial Reference Frame). 
+
+     The SPICE PCK software that reads this file uses the label "J2000"
+     to refer to the ICRF; this is actually a mislabeling which has
+     been retained in the interest of backward compatibility. Using
+     data from this file, by means of calls to the SPICE frame
+     transformation routines, will actually compute orientation
+     relative to the ICRF.
+
+     The difference between the J2000 frame and the ICRF is
+     on the order of tens of milliarcseconds and is well below the
+     accuracy level of the formulas in this file.
+
+Orientation models
+ 
+     All of the orientation models use three Euler angles to describe
+     the orientation of the coordinate axes of the "Body Equator and
+     Prime Meridian" system with respect to an inertial system. By
+     default, the inertial system is the ICRF (labeled as "J2000"), but
+     other frames can be specified in the file. See the PCK Required
+     Reading for details.
+ 
+     The first two angles, in order, are the ICRF right ascension and
+     declination (henceforth RA and DEC) of the north pole of a body as
+     a function of time. The third angle is the prime meridian location
+     (represented by "W"), which is expressed as a rotation about the
+     north pole, and is also a function of time.
+ 
+     For each body, the expressions for the north pole's right
+     ascension and declination, as well as prime meridian location, are
+     sums (as far as the models that appear in this file are concerned)
+     of quadratic polynomials and trigonometric polynomials, where the
+     independent variable is time.
+ 
+     In this file, the time arguments in expressions always refer to
+     Barycentric Dynamical Time (TDB), measured in centuries or days
+     past a reference epoch. By default, the reference epoch is the
+     J2000 epoch, which is Julian ephemeris date 2451545.0, but other
+     epochs can be specified in the file. See the PCK Required Reading
+     for details.
+
+     Orientation models for satellites and some planets (including
+     Jupiter) involve both polynomial terms and trigonometric terms.
+     The arguments of the trigonometric terms are linear polynomials.
+     In this file, we call the arguments of these trigonometric terms
+     "nutation precession angles."
+
+     Example: 2006 IAU Model for orientation of Jupiter.  Note that 
+     these values are used as an example only; see the data area below 
+     for current values.
+
+        Right ascension
+        ---------------
+ 
+        alpha   =  268.056595 - 0.006499 T        +  0.000117 sin(Ja) 
+             0                + 0.000938 sin(Jb)  +  0.001432 sin(Jc)
+                              + 0.000030 sin(Jd)  +  0.002150 sin(Je)
+
+        Declination
+        -----------
+ 
+        delta   =   64.495303 + 0.002413 T        +  0.000050 cos(Ja)
+             0                + 0.000404 cos(Jb)  +  0.000617 cos(Jc)
+                              - 0.000013 cos(Jd)  +  0.000926 cos(Je)
+
+        Prime meridian
+        --------------
+
+        W       =  284.95  + 870.5366420 d
+ 
+
+     Here
+
+        T represents centuries past J2000 ( TDB ),
+ 
+        d represents days past J2000 ( TDB ).
+
+        Ja-Je are nutation precession angles.
+
+     In this file, the polynomials' coefficients above are assigned 
+     to kernel variable names (left-hand-side symbols) as follows
+
+        BODY599_POLE_RA        = (   268.056595     -0.006499       0. )
+        BODY599_POLE_DEC       = (    64.495303      0.002413       0. )
+        BODY599_PM             = (   284.95        870.5366420      0. )
+
+     and the trigonometric polynomials' coefficients are assigned 
+     as follows
+
+        BODY599_NUT_PREC_RA  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000117
+                                                                0.000938
+                                                                0.001432
+                                                                0.000030
+                                                                0.002150 )
+
+        BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000050
+                                                                0.000404
+                                                                0.000617
+                                                               -0.000013
+                                                                0.000926 )
+
+        BODY599_NUT_PREC_PM  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.0
+                                                                0.0
+                                                                0.0
+                                                                0.0
+                                                                0.0  ) 
+
+     Note the number "599"; this is the NAIF ID code for Jupiter.
+
+     In this file, the polynomial expressions for the nutation
+     precession angles are listed along with the planet's RA, DEC, and
+     prime meridian terms. Below are the 2006 IAU nutation precession
+     angles for the Jupiter system.
+
+        J1  =   73.32      +  91472.9 T
+        J2  =   24.62      +  45137.2 T
+        J3  =  283.90      +   4850.7 T
+        J4  =  355.80      +   1191.3 T
+        J5  =  119.90      +    262.1 T
+        J6  =  229.80      +     64.3 T
+        J7  =  352.25      +   2382.6 T
+        J8  =  113.35      +   6070.0 T
+
+        J9  =  146.64      + 182945.8 T
+        J10 =   49.24      +  90274.4 T 
+
+        Ja  =   99.360714  +   4850.4046 T
+        Jb  =  175.895369  +   1191.9605 T
+        Jc  =  300.323162  +    262.5475 T
+        Jd  =  114.012305  +   6070.2476 T
+        Je  =   49.511251  +     64.3000 T
+
+     Here
+
+        T represents centuries past J2000 ( TDB )
+
+        J1-J10 and Ja-Je are the nutation precession angles. The angles
+        J9 and J10 are equal to 2*J1 and 2*J2, respectively.
+ 
+        Angles J9 and J10 are not present in [1]; they have been added
+        to fit the terms 2*J1 and 2*J2, which appear in the orientation
+        models of several satellites, into a form that can be accepted
+        by the PCK system.
+
+     The assignment of the nutation precession angles for the
+     Jupiter system is as follows:
+ 
+        BODY5_NUT_PREC_ANGLES  = (    73.32      91472.9
+                                      24.62      45137.2
+                                     283.90       4850.7
+                                     355.80       1191.3
+                                     119.90        262.1
+                                     229.80         64.3
+                                     352.25       2382.6
+                                     113.35       6070.0   
+                                     146.64     182945.8
+                                      49.24      90274.4  
+                                      99.360714   4850.4046
+                                     175.895369   1191.9605
+                                     300.323162    262.5475
+                                     114.012305   6070.2476
+                                      49.511251     64.3000  )
+
+     You'll see an additional symbol grouped with the ones listed
+     above; it is
+ 
+        BODY599_LONG_AXIS
+ 
+     This term is zero for all bodies except Mars. It represents the
+     angular offset between the meridian containing the longest axis of
+     the triaxial ellipsoid used to model a body's surface and the
+     prime meridian of the body.
+
+     The pattern of the formulas for satellite orientation is similar
+     to that for Jupiter. Example: 2006 IAU values for Io. Again, these
+     values are used as an example only; see the data area below for
+     current values.
+ 
+        Right ascension
+        ---------------
+
+        alpha  = 268.05  -  0.009 T  + 0.094 sin(J3)  +  0.024 sin(J4)
+             0  
+
+        Declination
+        -----------
+
+        delta  =  64.50  +  0.003 T  + 0.040 cos(J3)  +  0.011 cos(J4)
+             0           
+                          
+        Prime meridian
+        --------------
+
+        W      = 200.39  +  203.4889538 d  -  0.085 sin(J3)  -  0.022 sin(J4)
+
+ 
+        d represents days past J2000.
+ 
+        J3 and J4 are nutation precession angles.
+ 
+     The polynomial terms are assigned to symbols by the statements
+ 
+        BODY501_POLE_RA       = (  268.05          -0.009      0. )
+        BODY501_POLE_DEC      = (   64.50           0.003      0. )
+        BODY501_PM            = (  200.39         203.4889538  0. )
+ 
+     The coefficients of the trigonometric terms are assigned to symbols by
+     the statements
+
+        BODY501_NUT_PREC_RA   = (    0.   0.     0.094    0.024   )
+        BODY501_NUT_PREC_DEC  = (    0.   0.     0.040    0.011   )
+        BODY501_NUT_PREC_PM   = (    0.   0.    -0.085   -0.022   )
+
+     501 is the NAIF ID code for Io.
+ 
+     SPICE software expects the models for satellite orientation to
+     follow the form of the model shown here: the polynomial portions of the
+     RA, DEC, and W expressions are expected to be quadratic, the 
+     trigonometric terms for RA and W (satellite prime meridian) are expected 
+     to be linear combinations of sines of nutation precession angles, the 
+     trigonometric terms for DEC are expected to be linear combinations of 
+     cosines of nutation precession angles, and the polynomials for the 
+     nutation precession angles themselves are expected to be linear.
+ 
+     Eventually, the software will handle more complex expressions, we
+     expect.
+ 
+ 
+Shape models
+ 
+     There is only one kind of shape model supported by the SPICE Toolkit
+     software at present: the triaxial ellipsoid. The 2006 IAU report does
+     not use any other models, except in the case of Mars, where 
+     separate values are given for the north and south polar radii.
+ 
+     For each body, three radii are listed:  The first number is
+     the largest equatorial radius (the length of the semi-axis
+     containing the prime meridian), the second number is the smaller
+     equatorial radius, and the third is the polar radius.
+ 
+     Example: Radii of the Earth.
+ 
+        BODY399_RADII     = (     6378.14    6378.14      6356.75   )
+ 
+ 
+Body Numbers and Names
+--------------------------------------------------------
+ 
+ 
+        1  Mercury barycenter
+        2  Venus barycenter
+        3  Earth barycenter
+        4  Mars barycenter
+        5  Jupiter barycenter
+        6  Saturn barycenter
+        7  Uranus barycenter
+        8  Neptune barycenter
+        9  Pluto barycenter
+        10 Sun
+
+ 
+        199 Mercury
+ 
+ 
+        299 Venus
+ 
+ 
+        399 Earth
+ 
+        301 Moon
+ 
+ 
+        499 Mars
+ 
+        401 Phobos      402 Deimos
+ 
+ 
+        599 Jupiter
+ 
+        501 Io          502 Europa      503 Ganymede    504 Callisto
+        505 Amalthea    506 Himalia     507 Elara       508 Pasiphae
+        509 Sinope      510 Lysithea    511 Carme       512 Ananke
+        513 Leda        514 Thebe       515 Adrastea    516 Metis
+ 
+ 
+        699 Saturn
+ 
+        601 Mimas       602 Enceladus   603 Tethys      604 Dione
+        605 Rhea        606 Titan       607 Hyperion    608 Iapetus
+        609 Phoebe      610 Janus       611 Epimetheus  612 Helene
+        613 Telesto     614 Calypso     615 Atlas       616 Prometheus
+        617 Pandora     618 Pan
+ 
+ 
+        799 Uranus
+ 
+        701 Ariel       702 Umbriel     703 Titania     704 Oberon
+        705 Miranda     706 Cordelia    707 Ophelia     708 Bianca
+        709 Cressida    710 Desdemona   711 Juliet      712 Portia
+        713 Rosalind    714 Belinda     715 Puck
+ 
+ 
+        899 Neptune
+ 
+        801 Triton      802 Nereid      803 Naiad       804 Thalassa
+        805 Despina     806 Galatea     807 Larissa     808 Proteus
+ 
+ 
+        999 Pluto
+ 
+        901 Charon
+ 
+ 
+        1000005 Comet 19P/Borrelly
+        1000036 Comet Halley
+        1000093 Comet 9P/Tempel 1
+        1000107 Comet 81P/Wild 2
+
+        2000001 Asteroid Ceres
+        2000004 Asteroid Vesta
+        2000216 Asteroid Kleopatra
+        2000253 Asteroid Mathilde
+        2000433 Asteroid Eros
+        2004179 Asteroid Toutatis
+        2025143 Asteroid Itokawa
+        2431010 Asteroid Ida
+        9511010 Asteroid Gaspra
+        
+ 
+Orientation Constants for the Sun and Planets
+--------------------------------------------------------
+ 
+ 
+Sun
+ 
+     Old values:
+
+        Values are from the 2003 IAU report.
+
+  
+        body10_pole_ra         = (  286.13       0.          0. )
+        body10_pole_dec        = (   63.87       0.          0. )
+        body10_pm              = (   84.10      14.18440     0. )
+        body10_long_axis       = (    0.                        )
+
+     Current values:
+ 
+        \begindata
+ 
+        BODY10_POLE_RA         = (  286.13       0.          0. )
+        BODY10_POLE_DEC        = (   63.87       0.          0. )
+        BODY10_PM              = (   84.176     14.18440     0. )
+        BODY10_LONG_AXIS       = (    0.                        )
+
+        \begintext
+ 
+Mercury
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+
+
+     Current values:
+  
+        \begindata
+
+        BODY199_POLE_RA          = (  281.01     -0.033      0. )
+        BODY199_POLE_DEC         = (   61.45     -0.005      0. )
+        BODY199_PM               = (  329.548     6.1385025  0. )
+ 
+        BODY199_LONG_AXIS        = (    0.                        )
+ 
+        \begintext
+ 
+  
+Venus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY299_POLE_RA          = (  272.76       0.          0. )
+        BODY299_POLE_DEC         = (   67.16       0.          0. )
+        BODY299_PM               = (  160.20      -1.4813688   0. )
+ 
+        BODY299_LONG_AXIS        = (    0.                        )
+ 
+        \begintext
+
+
+Earth
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 report.
+ 
+ 
+     Current values:
+ 
+        \begindata 
+ 
+        BODY399_POLE_RA        = (    0.      -0.641         0. )
+        BODY399_POLE_DEC       = (   90.      -0.557         0. )
+        BODY399_PM             = (  190.147  360.9856235     0. )
+        BODY399_LONG_AXIS      = (    0.                        )
+
+        \begintext
+
+
+        Nutation precession angles for the Earth-Moon system:
+
+           The linear coefficients have been scaled up from degrees/day
+           to degrees/century, because the SPICELIB PCK reader expects
+           these units.  The original constants were:
+        
+                                    125.045D0   -0.0529921D0
+                                    250.089D0   -0.1059842D0
+                                    260.008D0   13.0120009D0
+                                    176.625D0   13.3407154D0
+                                    357.529D0    0.9856003D0
+                                    311.589D0   26.4057084D0
+                                    134.963D0   13.0649930D0
+                                    276.617D0    0.3287146D0
+                                     34.226D0    1.7484877D0
+                                     15.134D0   -0.1589763D0
+                                    119.743D0    0.0036096D0
+                                    239.961D0    0.1643573D0
+                                     25.053D0   12.9590088D0 
+
+
+        \begindata
+
+       
+        BODY3_NUT_PREC_ANGLES  = (  125.045         -1935.5364525000
+                                    250.089         -3871.0729050000
+                                    260.008        475263.3328725000  
+                                    176.625        487269.6299850000
+                                    357.529         35999.0509575000
+                                    311.589        964468.4993100000
+                                    134.963        477198.8693250000
+                                    276.617         12006.3007650000
+                                     34.226         63863.5132425000 
+                                     15.134         -5806.6093575000
+                                    119.743           131.8406400000
+                                    239.961          6003.1503825000 
+                                     25.053        473327.7964200000 )
+
+
+        \begintext
+ 
+
+     Earth north geomagnetic centered dipole:
+
+        Old values:
+
+           Values are from [7].  Note the year of publication was 1971.
+
+           body399_mag_north_pole_lon  =  ( -69.761 )
+           body399_mag_north_pole_lat  =  (  78.565 )
+
+
+        Current values:
+
+           The north dipole location is time-varying.  The values shown
+           below, taken from [8], represent a discrete sampling of the
+           north dipole location from 1945 to 2000. The terms DGRF and
+           IGRF refer to, respectively, "Definitive Geomagnetic
+           Reference Field" and "International Geomagnetic Reference
+           Field."  See references [6], [8], and [9] for details.
+
+           Coordinates are planetocentric. 
+
+             Data source    Lat      Lon
+             -----------   -----    ------
+              DGRF 1945    78.47    291.47
+              DGRF 1950    78.47    291.15
+              DGRF 1955    78.46    290.84
+              DGRF 1960    78.51    290.53
+              DGRF 1965    78.53    290.15
+              DGRF 1970    78.59    289.82
+              DGRF 1975    78.69    289.53
+              DGRF 1980    78.81    289.24 
+              DGRF 1985    78.97    289.10
+              DGRF 1990    79.13    288.89
+              IGRF 1995    79.30    288.59
+              IGRF 2000    79.54    288.43      
+
+
+        Values are given for the epoch 2000 and are from the final row
+        of the above table, which is from [8]. As shown by the table
+        these values constitute a low-accuracy approximation for epochs
+        not close to 2000.
+
+        \begindata
+       
+        BODY399_N_GEOMAG_CTR_DIPOLE_LON  =  ( 288.43 )
+        BODY399_N_GEOMAG_CTR_DIPOLE_LAT  =  (  79.54 )
+
+        \begintext
+
+ 
+Mars
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+   
+     Current values:
+ 
+        \begindata
+ 
+        BODY499_POLE_RA          = (  317.68143   -0.1061      0.  )
+        BODY499_POLE_DEC         = (   52.88650   -0.0609      0.  )
+        BODY499_PM               = (  176.630    350.89198226  0.  )
+
+        \begintext
+ 
+        Source [5] specifies the following value for the lambda_a term
+        (BODY499_LONG_AXIS ) for Mars. This term is the POSITIVE EAST
+        LONGITUDE, measured from the prime meridian, of the meridian
+        containing the longest axis of the reference ellipsoid.
+        (CAUTION: previous values were POSITIVE WEST.)
+
+           body499_long_axis        = (  252.  )
+ 
+        We list this lambda_a value for completeness. The IAU report
+        [1] gives equal values for both equatorial radii, so the
+        lambda_a offset does not apply to the IAU model.
+ 
+        The 2003 IAU report defines M2, the second nutation precession angle,
+        by:
+ 
+                                                2
+           192.93  +  1128.4096700 d  +  8.864 T
+ 
+        We truncate the M2 series to a linear expression, because the PCK
+        software cannot handle the quadratic term.
+ 
+        Again, the linear terms are scaled by 36525.0:
+ 
+            -0.4357640000000000       -->     -15916.28010000000
+          1128.409670000000           -->   41215163.19675000
+            -1.8151000000000000E-02   -->       -662.9652750000000
+ 
+        We also introduce a fourth nutation precession angle, which
+        is the pi/2-complement of the third angle.  This angle is used
+        in computing the prime meridian location for Deimos.  See the
+        discussion of this angle below in the section containing orientation
+        constants for Deimos.
+ 
+        \begindata
+
+        BODY4_NUT_PREC_ANGLES  = (  169.51     -15916.2801
+                                    192.93   41215163.19675
+                                     53.47       -662.965275
+                                     36.53        662.965275  )
+ 
+        \begintext
+ 
+ 
+Jupiter
+ 
+     Old values:
+ 
+        Values are from the 2003 IAU report.
+
+
+           body599_pole_ra        = (   268.05      -0.009       0. )
+           body599_pole_dec       = (    64.49       0.003       0. )
+           body599_pm             = (   284.95     870.5366420   0. )
+           body599_long_axis      = (     0.                        )
+
+           body5_nut_prec_angles  = (    73.32   91472.9
+                                         24.62   45137.2
+                                        283.90    4850.7
+                                        355.80    1191.3
+                                        119.90     262.1
+                                        229.80      64.3
+                                        352.35    2382.6
+                                        113.35    6070.0   
+                                        146.64  182945.8
+                                         49.24   90274.4  )
+ 
+
+                   
+     Current values:
+ 
+        The number of nutation precession angles is 15. The ninth and
+        tenth are twice the first and second, respectively. The
+        eleventh through fifteenth correspond to angles JA-JE in
+        the 2006 IAU report; angles JA-JE were not used prior to that
+        report.
+
+        \begindata
+ 
+ 
+        BODY599_POLE_RA        = (   268.056595     -0.006499       0. )
+        BODY599_POLE_DEC       = (    64.495303      0.002413       0. )
+        BODY599_PM             = (   284.95        870.5366420      0. )
+        BODY599_LONG_AXIS      = (     0.                        )
+ 
+        BODY599_NUT_PREC_RA  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000117
+                                                                0.000938
+                                                                0.001432
+                                                                0.000030
+                                                                0.002150 )
+
+        BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000050
+                                                                0.000404
+                                                                0.000617
+                                                               -0.000013
+                                                                0.000926 )
+
+        BODY599_NUT_PREC_PM  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.0
+                                                                0.0
+                                                                0.0
+                                                                0.0
+                                                                0.0  ) 
+
+
+        BODY5_NUT_PREC_ANGLES  = (    73.32      91472.9
+                                      24.62      45137.2
+                                     283.90       4850.7
+                                     355.80       1191.3
+                                     119.90        262.1
+                                     229.80         64.3
+                                     352.25       2382.6
+                                     113.35       6070.0   
+                                     146.64     182945.8
+                                      49.24      90274.4  
+                                      99.360714   4850.4046
+                                     175.895369   1191.9605
+                                     300.323162    262.5475
+                                     114.012305   6070.2476
+                                      49.511251     64.3000  )
+        \begintext
+ 
+ 
+Saturn
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+
+     Current values:
+ 
+        \begindata
+
+        BODY699_POLE_RA        = (    40.589    -0.036      0.  )
+        BODY699_POLE_DEC       = (    83.537    -0.004      0.  )
+        BODY699_PM             = (    38.90    810.7939024  0.  )
+        BODY699_LONG_AXIS      = (     0.                       )
+ 
+        \begintext
+ 
+        The first seven angles given here are the angles S1 
+        through S7 from the 2000 report; the eighth and
+        ninth angles are 2*S1 and 2*S2, respectively.
+ 
+ 
+        \begindata
+
+        BODY6_NUT_PREC_ANGLES  = (  353.32   75706.7
+                                     28.72   75706.7  
+                                    177.40  -36505.5 
+                                    300.00   -7225.9 
+                                    316.45     506.2
+                                    345.20   -1016.3  
+                                     29.80     -52.1
+                                    706.64  151413.4
+                                     57.44  151413.4  )
+        \begintext
+ 
+ 
+Uranus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY799_POLE_RA        = (  257.311     0.         0.  )
+        BODY799_POLE_DEC       = (  -15.175     0.         0.  )
+        BODY799_PM             = (  203.81   -501.1600928  0.  )
+        BODY799_LONG_AXIS      = (    0.                       )
+ 
+        \begintext
+        
+        The first 16 angles given here are the angles U1 
+        through U16 from the 2000 report; the 17th and
+        18th angles are 2*U11 and 2*U12, respectively.
+        
+        \begindata
+         
+        BODY7_NUT_PREC_ANGLES  = (  115.75   54991.87
+                                    141.69   41887.66
+                                    135.03   29927.35
+                                     61.77   25733.59  
+                                    249.32   24471.46
+                                     43.86   22278.41 
+                                     77.66   20289.42  
+                                    157.36   16652.76  
+                                    101.81   12872.63   
+                                    138.64    8061.81
+                                    102.23   -2024.22 
+                                    316.41    2863.96  
+                                    304.01     -51.94  
+                                    308.71     -93.17 
+                                    340.82     -75.32 
+                                    259.14    -504.81 
+                                    204.46   -4048.44
+                                    632.82    5727.92     )
+                                    
+        \begintext
+ 
+ 
+ 
+Neptune
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+ 
+     Current values:
+
+        \begindata        
+ 
+           BODY899_POLE_RA        = (  299.36     0.         0. )
+           BODY899_POLE_DEC       = (   43.46     0.         0. )
+           BODY899_PM             = (  253.18   536.3128492  0. )
+           BODY899_LONG_AXIS      = (    0.                     )
+
+
+           BODY899_NUT_PREC_RA    = (  0.70 0. 0. 0. 0. 0. 0. 0. ) 
+           BODY899_NUT_PREC_DEC   = ( -0.51 0. 0. 0. 0. 0. 0. 0. )
+           BODY899_NUT_PREC_PM    = ( -0.48 0. 0. 0. 0. 0. 0. 0. )
+
+        \begintext
+ 
+           The 2000 report defines the nutation precession angles
+ 
+              N, N1, N2, ... , N7
+ 
+           and also uses the multiples of N1 and N7
+ 
+              2*N1
+ 
+           and
+ 
+              2*N7, 3*N7, ..., 9*N7
+ 
+           In this file, we treat the angles and their multiples as
+           separate angles.  In the kernel variable
+ 
+              BODY8_NUT_PREC_ANGLES
+ 
+           the order of the angles is
+ 
+              N, N1, N2, ... , N7, 2*N1, 2*N7, 3*N7, ..., 9*N7
+ 
+           Each angle is defined by a linear polynomial, so two
+           consecutive array elements are allocated for each
+           angle.  The first term of each pair is the constant term,
+           the second is the linear term.
+ 
+        \begindata 
+
+              BODY8_NUT_PREC_ANGLES = (   357.85         52.316
+                                          323.92      62606.6
+                                          220.51      55064.2 
+                                          354.27      46564.5
+                                           75.31      26109.4 
+                                           35.36      14325.4
+                                          142.61       2824.6  
+                                          177.85         52.316 
+                                          647.840    125213.200
+                                          355.700       104.632
+                                          533.550       156.948
+                                          711.400       209.264
+                                          889.250       261.580
+                                         1067.100       313.896
+                                         1244.950       366.212
+                                         1422.800       418.528
+                                         1600.650       470.844   )
+                                         
+        \begintext
+ 
+ 
+ 
+Pluto
+ 
+     Old values:
+ 
+        Values are from the 2003 IAU report. 
+ 
+        BODY999_POLE_RA        = (  313.02    0.         0.   )
+        BODY999_POLE_DEC       = (    9.09    0.         0.   )
+        BODY999_PM             = (  236.77  -56.3623195  0.   )
+        BODY999_LONG_AXIS      = (    0.                      )
+
+
+     Current values:
+ 
+        \begindata
+ 
+        BODY999_POLE_RA        = (  312.993   0.          0. )
+        BODY999_POLE_DEC       = (    6.163   0.          0. )
+        BODY999_PM             = (  237.305  -56.3625225  0. )
+        BODY999_LONG_AXIS      = (    0.                     )
+
+        \begintext
+ 
+ 
+ 
+ 
+Orientation constants for the satellites
+--------------------------------------------------------
+ 
+ 
+Satellites of Earth
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+
+ 
+     New values:
+ 
+        \begindata
+ 
+ 
+
+
+
+        BODY301_POLE_RA      = (  269.9949        0.0031        0.      )
+        BODY301_POLE_DEC     = (   66.5392        0.0130        0.      )
+        BODY301_PM           = (   38.3213       13.17635815   -1.4D-12 )
+        BODY301_LONG_AXIS    = (    0.                                  )
+   
+        BODY301_NUT_PREC_RA  = (   -3.8787   -0.1204   0.0700   -0.0172
+                                    0.0       0.0072   0.0       0.0
+                                    0.0      -0.0052   0.0       0.0
+                                    0.0043                              )
+        
+        BODY301_NUT_PREC_DEC = (   1.5419     0.0239  -0.0278    0.0068
+                                   0.0       -0.0029   0.0009    0.0
+                                   0.0        0.0008   0.0       0.0     
+                                  -0.0009                               )
+        
+        BODY301_NUT_PREC_PM  = (   3.5610     0.1208  -0.0642    0.0158
+                                   0.0252    -0.0066  -0.0047   -0.0046
+                                   0.0028     0.0052   0.0040    0.0019
+                                  -0.0044                               )
+        \begintext
+ 
+
+ 
+Satellites of Mars
+ 
+ 
+     Phobos
+ 
+          Old values:
+ 
+             Values are unchanged in the 2006 IAU report.
+ 
+          Current values:
+ 
+            The quadratic prime meridian term is scaled by 1/36525**2:
+ 
+               8.864000000000000   --->   6.6443009930565219E-09
+ 
+        \begindata
+ 
+          BODY401_POLE_RA  = ( 317.68    -0.108     0.                     )
+          BODY401_POLE_DEC = (  52.90    -0.061     0.                     )
+          BODY401_PM       = (  35.06  1128.8445850 6.6443009930565219E-09 )
+                                       
+          BODY401_LONG_AXIS     = (    0.   )
+ 
+          BODY401_NUT_PREC_RA   = (   1.79    0.    0.   0. )
+          BODY401_NUT_PREC_DEC  = (  -1.08    0.    0.   0. )
+          BODY401_NUT_PREC_PM   = (  -1.42   -0.78  0.   0. )
+
+
+        \begintext
+ 
+ 
+     Deimos
+ 
+        Old values:
+ 
+           Values are unchanged in the 2006 IAU report.
+ 
+ 
+        New values:
+ 
+           The Deimos prime meridian expression is:
+ 
+ 
+                                                     2
+              W = 79.41  +  285.1618970 d  -  0.520 T  -  2.58 sin M
+                                                                    3
+ 
+                                                       +  0.19 cos M .
+                                                                    3
+ 
+ 
+           At the present time, the PCK kernel software (the routine
+           BODEUL in particular) cannot handle the cosine term directly,
+           but we can represent it as
+ 
+              0.19 sin M
+                        4
+ 
+           where
+ 
+              M   =  90.D0 - M
+               4              3
+ 
+           Therefore, the nutation precession angle assignments for Phobos
+           and Deimos contain four coefficients rather than three.
+ 
+           The quadratic prime meridian term is scaled by 1/36525**2:
+ 
+              -0.5200000000000000  --->   -3.8978300049519307E-10
+ 
+        \begindata
+ 
+           BODY402_POLE_RA       = (  316.65     -0.108       0.           )
+           BODY402_POLE_DEC      = (   53.52     -0.061       0.           )
+           BODY402_PM            = (   79.41    285.1618970  -3.897830D-10 )
+           BODY402_LONG_AXIS     = (    0.                                 )
+ 
+           BODY402_NUT_PREC_RA   = (    0.   0.   2.98    0.   )
+           BODY402_NUT_PREC_DEC  = (    0.   0.  -1.78    0.   )
+           BODY402_NUT_PREC_PM   = (    0.   0.  -2.58    0.19 )
+
+        \begintext
+ 
+ 
+ 
+ 
+Satellites of Jupiter
+ 
+ 
+     Io
+ 
+          Old values:
+ 
+             Values are unchanged in the 2006 IAU report.
+ 
+          Current values:
+         
+        \begindata
+ 
+        BODY501_POLE_RA       = (  268.05          -0.009      0. )
+        BODY501_POLE_DEC      = (   64.50           0.003      0. )
+        BODY501_PM            = (  200.39         203.4889538  0. )
+        BODY501_LONG_AXIS     = (    0.                           )
+ 
+        BODY501_NUT_PREC_RA   = (    0.   0.     0.094    0.024   )
+        BODY501_NUT_PREC_DEC  = (    0.   0.     0.040    0.011   )
+        BODY501_NUT_PREC_PM   = (    0.   0.    -0.085   -0.022   )
+
+        \begintext
+ 
+ 
+ 
+     Europa
+ 
+ 
+        Old values:
+
+           Values are from the 2003 IAU report.
+
+
+        body502_pole_ra       = (  268.08          -0.009      0.   )
+        body502_pole_dec      = (   64.51           0.003      0.   )
+        body502_pm            = (   35.67         101.3747235  0.   )
+        body502_long_axis     = (    0.                             )
+ 
+        body502_nut_prec_ra   = ( 0. 0. 0.   1.086   0.060   0.015   0.009 )
+        body502_nut_prec_dec  = ( 0. 0. 0.   0.468   0.026   0.007   0.002 )
+        body502_nut_prec_pm   = ( 0. 0. 0.  -0.980  -0.054  -0.014  -0.008 )
+        
+
+        Current values:
+ 
+        \begindata 
+ 
+        BODY502_POLE_RA       = (  268.08          -0.009      0.   )
+        BODY502_POLE_DEC      = (   64.51           0.003      0.   )
+        BODY502_PM            = (   36.022        101.3747235  0.   )
+        BODY502_LONG_AXIS     = (    0.                             )
+ 
+        BODY502_NUT_PREC_RA   = ( 0. 0. 0.   1.086   0.060   0.015   0.009 )
+        BODY502_NUT_PREC_DEC  = ( 0. 0. 0.   0.468   0.026   0.007   0.002 )
+        BODY502_NUT_PREC_PM   = ( 0. 0. 0.  -0.980  -0.054  -0.014  -0.008 )
+ 
+        \begintext
+ 
+ 
+     Ganymede
+ 
+        Old values:
+ 
+             Values are unchanged in the 2006 IAU report.
+ 
+
+        Current values:
+        
+        \begindata
+    
+        BODY503_POLE_RA       = (  268.20         -0.009       0.  )
+        BODY503_POLE_DEC      = (   64.57          0.003       0.  )
+        BODY503_PM            = (   44.064        50.3176081   0.  )
+        BODY503_LONG_AXIS     = (    0.                            )
+
+        BODY503_NUT_PREC_RA   = ( 0. 0. 0.  -0.037   0.431   0.091   )
+        BODY503_NUT_PREC_DEC  = ( 0. 0. 0.  -0.016   0.186   0.039   )
+        BODY503_NUT_PREC_PM   = ( 0. 0. 0.   0.033  -0.389  -0.082   )
+ 
+        \begintext
+ 
+ 
+     Callisto
+ 
+        Old values:
+
+             Values are unchanged in the 2006 IAU report.
+        
+        
+        Current values:
+        
+        
+        \begindata
+  
+        BODY504_POLE_RA       = (   268.72    -0.009       0.  )
+        BODY504_POLE_DEC      = (    64.83     0.003       0.  )
+        BODY504_PM            = (   259.51    21.5710715   0.  )
+        BODY504_LONG_AXIS     = (     0.                       )
+ 
+        BODY504_NUT_PREC_RA   = ( 0. 0. 0. 0.  -0.068   0.590  0.   0.010 )
+        BODY504_NUT_PREC_DEC  = ( 0. 0. 0. 0.  -0.029   0.254  0.  -0.004 )
+        BODY504_NUT_PREC_PM   = ( 0. 0. 0. 0.   0.061  -0.533  0.  -0.009 )
+ 
+        \begintext
+ 
+ 
+     Amalthea
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report.        
+        
+        Current values:
+         
+        \begindata
+ 
+        BODY505_POLE_RA       = (   268.05    -0.009      0.  )
+        BODY505_POLE_DEC      = (    64.49     0.003      0.  )
+        BODY505_PM            = (   231.67   722.6314560  0.  )
+        BODY505_LONG_AXIS     = (     0.                      )
+ 
+        BODY505_NUT_PREC_RA  = ( -0.84  0. 0. 0. 0. 0. 0. 0.   0.01  0. )
+        BODY505_NUT_PREC_DEC = ( -0.36  0. 0. 0. 0. 0. 0. 0.   0.    0. )
+        BODY505_NUT_PREC_PM  = (  0.76  0. 0. 0. 0. 0. 0. 0.  -0.01  0. )
+ 
+        \begintext
+ 
+ 
+     Thebe
+ 
+ 
+        Old values:
+                
+           Values are unchanged in the 2006 IAU report.                
+          
+        Current values:
+        
+        \begindata
+ 
+        BODY514_POLE_RA       = (  268.05     -0.009       0.  )
+        BODY514_POLE_DEC      = (   64.49      0.003       0.  )
+        BODY514_PM            = (    8.56    533.7004100   0.  )
+        BODY514_LONG_AXIS     = (    0.                        )
+ 
+        BODY514_NUT_PREC_RA  = ( 0.  -2.11  0. 0. 0. 0. 0. 0. 0.  0.04 )
+        BODY514_NUT_PREC_DEC = ( 0.  -0.91  0. 0. 0. 0. 0. 0. 0.  0.01 )
+        BODY514_NUT_PREC_PM  = ( 0.   1.91  0. 0. 0. 0. 0. 0. 0. -0.04 )
+ 
+        \begintext
+ 
+ 
+     Adrastea
+ 
+        Old values:
+                
+           Values are unchanged in the 2006 IAU report.                
+        
+        Current values:
+        
+        \begindata
+ 
+ 
+ 
+        BODY515_POLE_RA       = (  268.05     -0.009       0.  )
+        BODY515_POLE_DEC      = (   64.49      0.003       0.  )
+        BODY515_PM            = (   33.29   1206.9986602   0.  )
+        BODY515_LONG_AXIS     = (    0.                        )
+
+        \begintext
+ 
+ 
+     Metis
+  
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report.  
+              
+        Current values:
+           
+        \begindata
+
+        BODY516_POLE_RA       = (  268.05     -0.009       0.  )
+        BODY516_POLE_DEC      = (   64.49      0.003       0.  )
+        BODY516_PM            = (  346.09   1221.2547301   0.  )
+        BODY516_LONG_AXIS     = (    0.                        )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Saturn
+      
+     
+     Mimas
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report.  
+               
+        Current values:
+ 
+        \begindata
+  
+           BODY601_POLE_RA       = (   40.66     -0.036      0.  )
+           BODY601_POLE_DEC      = (   83.52     -0.004      0.  )
+           BODY601_PM            = (  337.46    381.9945550  0.  )
+           BODY601_LONG_AXIS     = (     0.                      )
+ 
+           BODY601_NUT_PREC_RA   = ( 0. 0.   13.56  0.    0.    0. 0. 0. 0. )
+           BODY601_NUT_PREC_DEC  = ( 0. 0.   -1.53  0.    0.    0. 0. 0. 0. )
+           BODY601_NUT_PREC_PM   = ( 0. 0.  -13.48  0.  -44.85  0. 0. 0. 0. )
+
+        \begintext
+ 
+ 
+     Enceladus
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report.  
+               
+        Current values:
+ 
+        \begindata
+ 
+           BODY602_POLE_RA       = (   40.66    -0.036       0. )
+           BODY602_POLE_DEC      = (   83.52    -0.004       0. )
+           BODY602_PM            = (    2.82   262.7318996   0. )
+           BODY602_LONG_AXIS     = (    0.                      )
+
+        \begintext
+ 
+ 
+ 
+     Tethys
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+ 
+        Current values:
+ 
+        \begindata
+ 
+           BODY603_POLE_RA       = (   40.66    -0.036       0. )
+           BODY603_POLE_DEC      = (   83.52    -0.004       0. )
+           BODY603_PM            = (   10.45   190.6979085   0. )
+           BODY603_LONG_AXIS     = (    0.                      )
+ 
+           BODY603_NUT_PREC_RA   = ( 0. 0. 0.   9.66   0.    0.  0.  0.  0. )
+           BODY603_NUT_PREC_DEC  = ( 0. 0. 0.  -1.09   0.    0.  0.  0.  0. )
+           BODY603_NUT_PREC_PM   = ( 0. 0. 0.  -9.60   2.23  0.  0.  0.  0. )
+
+        \begintext
+ 
+ 
+     Dione
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+ 
+        Current values:
+ 
+        \begindata
+   
+           BODY604_POLE_RA       = (  40.66      -0.036      0.  )
+           BODY604_POLE_DEC      = (  83.52      -0.004      0.  )
+           BODY604_PM            = (  357.00    131.5349316  0.  )
+           BODY604_LONG_AXIS     = (    0.                       )
+
+        \begintext
+ 
+ 
+ 
+     Rhea
+     
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+ 
+        Current values:
+ 
+        \begindata
+   
+           BODY605_POLE_RA       = (   40.38   -0.036       0. )
+           BODY605_POLE_DEC      = (   83.55   -0.004       0. )
+           BODY605_PM            = (  235.16   79.6900478   0. )
+           BODY605_LONG_AXIS     = (    0.                     )
+ 
+           BODY605_NUT_PREC_RA   = ( 0. 0. 0. 0. 0.   3.10   0. 0. 0. )
+           BODY605_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0.  -0.35   0. 0. 0. )
+           BODY605_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  -3.08   0. 0. 0. )
+ 
+        \begintext
+ 
+ 
+ 
+     Titan
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY606_POLE_RA       = (    36.41   -0.036      0. )
+           BODY606_POLE_DEC      = (    83.94   -0.004      0. )
+           BODY606_PM            = (   189.64   22.5769768  0. )
+           BODY606_LONG_AXIS     = (     0.                    )
+ 
+           BODY606_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 0.  2.66  0. 0 )
+           BODY606_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 0. -0.30  0. 0 )
+           BODY606_NUT_PREC_PM   = ( 0. 0. 0. 0. 0. 0. -2.64  0. 0 )
+
+        \begintext
+ 
+ 
+ 
+     Hyperion
+ 
+         The IAU report does not give an orientation model for Hyperion.
+         Hyperion's rotation is in chaotic and is not predictable for
+         long periods.
+
+ 
+     Iapetus
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY608_POLE_RA       = (   318.16  -3.949      0.  )
+           BODY608_POLE_DEC      = (    75.03  -1.143      0.  )
+           BODY608_PM            = (   350.20   4.5379572  0.  )
+           BODY608_LONG_AXIS     = (     0.                    )
+
+        \begintext
+ 
+ 
+ 
+     Phoebe
+ 
+
+        Old values:
+        
+           Values are from the 2003 IAU report. 
+  
+           body609_pole_ra       = ( 355.00       0.         0.  )
+           body609_pole_dec      = (  68.70       0.         0.  )
+           body609_pm            = ( 304.70     930.8338720  0.  )
+           body609_long_axis     = (    0.                       )
+
+        Current values:
+ 
+        \begindata 
+  
+           BODY609_POLE_RA       = ( 356.90       0.         0.  )
+           BODY609_POLE_DEC      = (  77.80       0.         0.  )
+           BODY609_PM            = ( 178.58     931.639      0.  )
+           BODY609_LONG_AXIS     = (    0.                       )
+
+        \begintext
+ 
+ 
+     Janus
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY610_POLE_RA       = (  40.58    -0.036       0. )
+           BODY610_POLE_DEC      = (  83.52    -0.004       0. )
+           BODY610_PM            = (  58.83   518.2359876   0. )
+           BODY610_LONG_AXIS     = (   0.                      )
+ 
+           BODY610_NUT_PREC_RA   = ( 0. -1.623  0. 0. 0. 0. 0. 0.  0.023 )
+           BODY610_NUT_PREC_DEC  = ( 0. -0.183  0. 0. 0. 0. 0. 0.  0.001 )
+           BODY610_NUT_PREC_PM   = ( 0.  1.613  0. 0. 0. 0. 0. 0. -0.023 )
+ 
+        \begintext
+ 
+ 
+ 
+     Epimetheus
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+         
+        Current values:
+ 
+        \begindata 
+  
+           BODY611_POLE_RA       = (  40.58    -0.036        0. )
+           BODY611_POLE_DEC      = (  83.52    -0.004        0. )
+           BODY611_PM            = ( 293.87   518.4907239    0. )
+           BODY611_LONG_AXIS     = (   0.                       )
+ 
+           BODY611_NUT_PREC_RA   = ( -3.153   0. 0. 0. 0. 0. 0.   0.086  0. )
+           BODY611_NUT_PREC_DEC  = ( -0.356   0. 0. 0. 0. 0. 0.   0.005  0. )
+           BODY611_NUT_PREC_PM   = (  3.133   0. 0. 0. 0. 0. 0.  -0.086  0. )
+
+        \begintext
+ 
+ 
+ 
+     Helene
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+ 
+           BODY612_POLE_RA       = (  40.85     -0.036        0. )
+           BODY612_POLE_DEC      = (  83.34     -0.004        0. )
+           BODY612_PM            = ( 245.12    131.6174056    0. )
+           BODY612_LONG_AXIS     = (   0.                        )
+
+        \begintext
+ 
+ 
+ 
+     Telesto
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+ 
+           BODY613_POLE_RA       = ( 50.51    -0.036      0.  )
+           BODY613_POLE_DEC      = ( 84.06    -0.004      0.  )
+           BODY613_PM            = ( 56.88   190.6979332  0.  )
+           BODY613_LONG_AXIS     = (  0.                      )
+
+        \begintext
+
+ 
+ 
+     Calypso
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY614_POLE_RA       = (   36.41    -0.036        0.  )
+           BODY614_POLE_DEC      = (   85.04    -0.004        0.  )
+           BODY614_PM            = (  153.51   190.6742373    0.  )
+           BODY614_LONG_AXIS     = (    0.                        )
+ 
+        \begintext
+ 
+ 
+ 
+     Atlas
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY615_POLE_RA       = (   40.58     -0.036      0. )
+           BODY615_POLE_DEC      = (   83.53     -0.004      0. )  
+           BODY615_PM            = (  137.88    598.3060000  0. )
+           BODY615_LONG_AXIS     = (    0.                      )
+
+        \begintext
+ 
+ 
+ 
+     Prometheus
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY616_POLE_RA       = (  40.58      -0.036    )
+           BODY616_POLE_DEC      = (  83.53      -0.004    )
+           BODY616_PM            = ( 296.14     587.289000 )
+           BODY616_LONG_AXIS     = (   0.                  )
+ 
+        \begintext
+ 
+ 
+ 
+     Pandora
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY617_POLE_RA       = (   40.58     -0.036      0.  )
+           BODY617_POLE_DEC      = (   83.53     -0.004      0.  )
+           BODY617_PM            = (  162.92    572.7891000  0.  )
+           BODY617_LONG_AXIS     = (     0.                      )
+ 
+        \begintext
+ 
+ 
+ 
+     Pan
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY618_POLE_RA       = (   40.6     -0.036       0. )
+           BODY618_POLE_DEC      = (   83.5     -0.004       0. )
+           BODY618_PM            = (   48.8    626.0440000   0. )
+           BODY618_LONG_AXIS     = (    0.                      )
+
+        \begintext
+ 
+ 
+ 
+ 
+ 
+Satellites of Uranus
+ 
+  
+ 
+     Ariel
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+ 
+        Current values:
+
+        \begindata 
+
+           BODY701_POLE_RA       = ( 257.43     0.          0. )
+           BODY701_POLE_DEC      = ( -15.10     0.          0. )
+           BODY701_PM            = ( 156.22  -142.8356681   0. )
+           BODY701_LONG_AXIS     = (   0.                      )
+ 
+           BODY701_NUT_PREC_RA   = (  0. 0. 0. 0. 0.
+                                      0. 0. 0. 0. 0.  0.    0.    0.29 )
+ 
+           BODY701_NUT_PREC_DEC  = (  0. 0. 0. 0. 0.
+                                      0. 0. 0. 0. 0.  0.    0.    0.28 )
+ 
+           BODY701_NUT_PREC_PM   = (  0. 0. 0. 0. 0.
+                                      0. 0. 0. 0. 0.  0.   0.05   0.08 )
+        \begintext
+ 
+ 
+ 
+     Umbriel
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+ 
+           BODY702_POLE_RA       = (  257.43     0.          0. )
+           BODY702_POLE_DEC      = (  -15.10     0.          0. )
+           BODY702_PM            = (  108.05   -86.8688923   0. )
+           BODY702_LONG_AXIS     = (    0.                      )
+ 
+           BODY702_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0.   0.    0.   0.21 )
+ 
+           BODY702_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0.   0.    0.   0.20 )
+ 
+           BODY702_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  
+                                     0. 0. 0. 0. 0.   0.  -0.09  0.   0.06 )
+
+        \begintext
+ 
+ 
+ 
+     Titania
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY703_POLE_RA       = (  257.43    0.          0. )
+           BODY703_POLE_DEC      = (  -15.10    0.          0. )
+           BODY703_PM            = (   77.74  -41.3514316   0. )
+           BODY703_LONG_AXIS     = (    0.                     )
+ 
+           BODY703_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0. 0. 0. 0.   0.29 )
+ 
+           BODY703_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0. 0. 0. 0.   0.28 )
+ 
+           BODY703_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  
+                                     0. 0. 0. 0. 0.   0. 0. 0. 0.   0.08 )
+        \begintext
+ 
+ 
+ 
+     Oberon
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY704_POLE_RA       = (  257.43    0.          0. )
+           BODY704_POLE_DEC      = (  -15.10    0.          0. )
+           BODY704_PM            = (    6.77  -26.7394932   0. )
+           BODY704_LONG_AXIS     = (    0.                     )
+ 
+ 
+           BODY704_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0.16 )
+ 
+           BODY704_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0. 
+                                     0. 0. 0. 0. 0.   0.16 )
+ 
+           BODY704_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  
+                                     0. 0. 0. 0. 0.  
+                                     0. 0. 0. 0. 0.   0.04 )
+        \begintext
+ 
+ 
+ 
+     Miranda
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+
+           BODY705_POLE_RA      = (  257.43     0.         0. )
+           BODY705_POLE_DEC     = (  -15.08     0.         0. )
+           BODY705_PM           = (   30.70  -254.6906892  0. )
+           BODY705_LONG_AXIS    = (    0.                     )
+ 
+           BODY705_NUT_PREC_RA  = ( 0.     0.     0.    0.    0.  
+                                    0.     0.     0.    0.    0. 
+                                    4.41   0.     0.    0.    0. 
+                                    0.    -0.04   0.             )
+ 
+           BODY705_NUT_PREC_DEC = ( 0.     0.     0.    0.    0.  
+                                    0.     0.     0.    0.    0. 
+                                    4.25   0.     0.    0.    0. 
+                                    0.    -0.02   0.             )
+ 
+           BODY705_NUT_PREC_PM  = ( 0.     0.     0.    0.    0.  
+                                    0.     0.     0.    0.    0. 
+                                    1.15  -1.27   0.    0.    0.  
+                                    0.    -0.09   0.15           )
+        \begintext
+ 
+ 
+ 
+     Cordelia
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY706_POLE_RA      = (   257.31      0.         0.  )
+           BODY706_POLE_DEC     = (   -15.18      0.         0.  )
+           BODY706_PM           = (   127.69  -1074.5205730  0.  )
+           BODY706_LONG_AXIS    = (     0.                       )
+ 
+           BODY706_NUT_PREC_RA  = (   -0.15    0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )
+
+           BODY706_NUT_PREC_DEC = (    0.14    0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )  
+
+           BODY706_NUT_PREC_PM  = (   -0.04    0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             ) 
+ 
+        \begintext
+ 
+ 
+
+     Ophelia
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+   
+           BODY707_POLE_RA      = (  257.31     0.         0. )
+           BODY707_POLE_DEC     = (  -15.18     0.         0. )
+           BODY707_PM           = (  130.35  -956.4068150  0. )
+           BODY707_LONG_AXIS    = (    0.                     )
+ 
+           BODY707_NUT_PREC_RA  = (    0.     -0.09   0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )
+
+           BODY707_NUT_PREC_DEC = (    0.      0.09   0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )
+
+           BODY707_NUT_PREC_PM  = (    0.     -0.03   0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.    0.    0.
+                                       0.      0.     0.             )
+ 
+        \begintext
+ 
+ 
+ 
+     Bianca
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY708_POLE_RA      = (  257.31     0.         0.  )
+           BODY708_POLE_DEC     = (  -15.18     0.         0.  )
+           BODY708_PM           = (  105.46  -828.3914760  0.  )
+           BODY708_LONG_AXIS    = (    0.                      )
+ 
+           BODY708_NUT_PREC_RA  = (    0.      0.    -0.16    0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.               )
+
+           BODY708_NUT_PREC_DEC = (    0.      0.     0.16    0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.               )
+
+           BODY708_NUT_PREC_PM  = (    0.      0.    -0.04    0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.      0.    0.
+                                       0.      0.     0.               )
+
+        \begintext
+ 
+ 
+ 
+     Cressida
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+ 
+           BODY709_POLE_RA      = (  257.31      0.          0.  )
+           BODY709_POLE_DEC     = (  -15.18      0.          0.  )
+           BODY709_PM           = (   59.16   -776.5816320   0.  )
+           BODY709_LONG_AXIS    = (    0.                        )
+ 
+
+           BODY709_NUT_PREC_RA  = (    0.      0.     0.     -0.04   0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.                )
+
+
+           BODY709_NUT_PREC_DEC = (    0.      0.     0.      0.04   0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.                )
+
+
+           BODY709_NUT_PREC_PM  = (    0.      0.     0.     -0.01   0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.      0.     0.
+                                       0.      0.     0.                )
+
+
+        \begintext
+ 
+ 
+ 
+     Desdemona
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+  
+           BODY710_POLE_RA      = ( 257.31      0.           0.  )
+           BODY710_POLE_DEC     = ( -15.18      0.           0.  )
+           BODY710_PM           = (  95.08   -760.0531690    0.  )
+           BODY710_LONG_AXIS    = (   0.                         )
+ 
+           BODY710_NUT_PREC_RA  = (   0.      0.     0.      0.    -0.17 
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+
+           BODY710_NUT_PREC_DEC = (   0.      0.     0.      0.     0.16 
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+
+           BODY710_NUT_PREC_PM  = (   0.      0.     0.      0.    -0.04  
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                 )
+
+        \begintext
+ 
+ 
+ 
+     Juliet
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY711_POLE_RA      = (  257.31     0.           0.   )
+           BODY711_POLE_DEC     = (  -15.18     0.           0.   )
+           BODY711_PM           = (  302.56  -730.1253660    0.   )
+           BODY711_LONG_AXIS    = (    0.                         )
+ 
+           BODY711_NUT_PREC_RA  = (   0.      0.     0.      0.     0.  
+                                     -0.06    0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                 )
+ 
+           BODY711_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.06    0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                 )
+  
+           BODY711_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                     -0.02    0.     0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                 )
+ 
+        \begintext
+ 
+ 
+ 
+     Portia
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+    
+           BODY712_POLE_RA      = (  257.31      0.           0.   )
+           BODY712_POLE_DEC     = (  -15.18      0.           0.   )
+           BODY712_PM           = (   25.03   -701.4865870    0.   )
+           BODY712_LONG_AXIS    = (    0.                          )
+ 
+           BODY712_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
+                                      0.     -0.09   0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                )
+
+           BODY712_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.      0.09   0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.               )
+
+           BODY712_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                      0.     -0.02   0.      0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.               )
+
+        \begintext
+ 
+ 
+ 
+     Rosalind
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+   
+           BODY713_POLE_RA      = ( 257.31      0.          0.  )
+           BODY713_POLE_DEC     = ( -15.18      0.          0.  )
+           BODY713_PM           = ( 314.90   -644.6311260   0.  )
+           BODY713_LONG_AXIS    = (   0.                        )
+ 
+           BODY713_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
+                                      0.      0.    -0.29    0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.               )
+
+           BODY713_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.28    0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.              )
+
+           BODY713_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                      0.      0.    -0.08    0.     0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.              )
+ 
+        \begintext
+ 
+ 
+ 
+     Belinda
+ 
+       Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata 
+ 
+           BODY714_POLE_RA      = (   257.31      0.         0. )
+           BODY714_POLE_DEC     = (   -15.18      0.         0. )
+           BODY714_PM           = (   297.46   -577.3628170  0. )
+           BODY714_LONG_AXIS    = (     0.                      )
+ 
+           BODY714_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.     -0.03   0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                )
+
+           BODY714_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.      0.03   0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                )
+
+           BODY714_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.     -0.01   0.
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                )
+        \begintext
+ 
+ 
+ 
+     Puck
+ 
+       Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+  
+           BODY715_POLE_RA      = (  257.31      0.         0.  )
+           BODY715_POLE_DEC     = (  -15.18      0.         0.  )
+           BODY715_PM           = (   91.24   -472.5450690  0.  )
+           BODY715_LONG_AXIS    = (    0.                       )
+ 
+           BODY715_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.      0.    -0.33 
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+
+           BODY715_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.      0.     0.31
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+
+           BODY715_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
+                                      0.      0.     0.      0.    -0.09
+                                      0.      0.     0.      0.     0.
+                                      0.      0.     0.                  )
+  
+        \begintext
+ 
+ 
+ 
+ 
+Satellites of Neptune
+ 
+ 
+     Triton
+ 
+       Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+ 
+        Current values:
+ 
+        \begindata
+
+           BODY801_POLE_RA       = ( 299.36     0.         0.  )
+           BODY801_POLE_DEC      = (  41.17     0.         0.  )
+           BODY801_PM            = ( 296.53   -61.2572637  0.  )
+           BODY801_LONG_AXIS     = (   0.                      )
+ 
+ 
+           BODY801_NUT_PREC_RA   = (  0.      0.      0.      0.  
+                                      0.      0.      0.    -32.35    
+                                      0.     -6.28   -2.08   -0.74       
+                                     -0.28   -0.11   -0.07   -0.02    
+                                     -0.01                         )
+ 
+ 
+           BODY801_NUT_PREC_DEC  = (  0.      0.      0.      0.  
+                                      0.      0.      0.     22.55    
+                                      0.      2.10    0.55    0.16   
+                                      0.05    0.02    0.01    0.
+                                      0.                           )
+ 
+ 
+           BODY801_NUT_PREC_PM   = (  0.      0.      0.      0.  
+                                      0.      0.      0.     22.25   
+                                      0.      6.73    2.05    0.74   
+                                      0.28    0.11    0.05    0.02
+                                      0.01                         )
+  
+        \begintext
+ 
+ 
+ 
+ 
+     Nereid
+ 
+        Old values:
+ 
+           Values are from the 1988 IAU report [10].  Note that this 
+           rotation model pre-dated the 1989 Voyager 2 Neptune
+           encounter.
+
+ 
+           body802_pole_ra       = (    273.48    0.        0.  )
+           body802_pole_dec      = (     67.22    0.        0.  )
+           body802_pm            = (    237.22    0.9996465 0.  )
+           body802_long_axis     = (      0.                    )
+ 
+ 
+           The report seems to have a typo:  in the nut_prec_ra expression,
+           where the report gives  -0.51 sin 3N3, we use -0.51 3N2.
+ 
+           body802_nut_prec_ra   = (  0.    -17.81
+                                      0.      0.     0.      0.
+                                      0.      0.     0.
+                                      2.56   -0.51   0.11   -0.03  )
+ 
+           body802_nut_prec_dec  = (  0.     -6.67
+                                      0.      0.     0.      0.
+                                      0.      0.     0.
+                                      0.47   -0.07   0.01          )
+ 
+           body802_nut_prec_pm   = (  0.     16.48
+                                      0.      0.     0.      0.
+                                      0.      0.     0.
+                                     -2.57    0.51 -0.11    0.02  )
+ 
+ 
+ 
+        Current values:
+ 
+           The 2006 report [1] states that values for Nereid are not
+           given because Nereid is not in synchronous rotation with Neptune
+           (p. 167).
+ 
+ 
+ 
+     Naiad
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+ 
+        \begindata
+  
+           BODY803_POLE_RA       = (  299.36      0.          0.  )
+           BODY803_POLE_DEC      = (   43.36      0.          0.  )
+           BODY803_PM            = (  254.06  +1222.8441209   0.  )
+           BODY803_LONG_AXIS     = (    0.                        )
+ 
+ 
+           BODY803_NUT_PREC_RA   = (    0.70     -6.49     0.      0.
+                                        0.        0.       0.      0.
+                                        0.25      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+ 
+           BODY803_NUT_PREC_DEC  = (   -0.51     -4.75     0.      0.
+                                        0.        0.       0.      0.
+                                        0.09      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+ 
+           BODY803_NUT_PREC_PM   = (   -0.48      4.40     0.      0.
+                                        0.        0.       0.      0.
+                                       -0.27      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+    
+        \begintext
+ 
+ 
+ 
+ 
+     Thalassa
+ 
+
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY804_POLE_RA       = (  299.36      0.          0. )
+           BODY804_POLE_DEC      = (   43.45      0.          0. )
+           BODY804_PM            = (  102.06   1155.7555612   0. )  
+           BODY804_LONG_AXIS     = (    0.                       )
+ 
+ 
+           BODY804_NUT_PREC_RA   = (    0.70      0.      -0.28    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+   
+  
+           BODY804_NUT_PREC_DEC  = (   -0.51      0.      -0.21    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0. 
+                                        0.                             )
+ 
+           BODY804_NUT_PREC_PM   = (   -0.48      0.       0.19    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0. 
+                                        0.                             )
+                                                                 
+        \begintext
+ 
+ 
+ 
+     Despina
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+ 
+        \begindata
+  
+           BODY805_POLE_RA       = (  299.36      0.          0. )
+           BODY805_POLE_DEC      = (   43.45      0.          0. )
+           BODY805_PM            = (  306.51  +1075.7341562   0. )
+           BODY805_LONG_AXIS     = (    0.                       )
+ 
+ 
+           BODY805_NUT_PREC_RA   = (    0.70      0.       0.     -0.09
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                              )
+ 
+           BODY805_NUT_PREC_DEC  = (   -0.51      0.       0.     -0.07
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                              )
+ 
+           BODY805_NUT_PREC_PM   = (   -0.49      0.       0.      0.06
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                              )
+        \begintext
+ 
+ 
+ 
+     Galatea
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+ 
+        \begindata
+  
+           BODY806_POLE_RA       = (   299.36      0.          0. )
+           BODY806_POLE_DEC      = (    43.43      0.          0. )
+           BODY806_PM            = (   258.09    839.6597686   0. )
+           BODY806_LONG_AXIS     = (     0.                       )
+ 
+ 
+           BODY806_NUT_PREC_RA   = (    0.70      0.       0.      0.
+                                       -0.07      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+ 
+           BODY806_NUT_PREC_DEC  = (   -0.51      0.       0.      0.
+                                       -0.05      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+ 
+           BODY806_NUT_PREC_PM   = (   -0.48      0.       0.      0.
+                                        0.05      0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             ) 
+        \begintext
+
+ 
+     Larissa
+ 
+ 
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+  
+        \begindata
+
+           BODY807_POLE_RA       = (   299.36     0.           0. )
+           BODY807_POLE_DEC      = (    43.41     0.           0. )
+           BODY807_PM            = (   179.41  +649.0534470    0. )
+           BODY807_LONG_AXIS     = (     0.                       )
+ 
+ 
+           BODY807_NUT_PREC_RA   = (    0.70      0.       0.      0.
+                                        0.       -0.27     0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+ 
+           BODY807_NUT_PREC_DEC  = (   -0.51      0.       0.      0.
+                                        0.       -0.20     0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+ 
+           BODY807_NUT_PREC_PM   = (   -0.48      0.       0.      0.
+                                        0.        0.19     0.      0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                            )
+        \begintext
+ 
+ 
+ 
+     Proteus
+ 
+
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY808_POLE_RA       = (  299.27      0.          0.  )
+           BODY808_POLE_DEC      = (   42.91      0.          0.  )
+           BODY808_PM            = (   93.38   +320.7654228   0.  )
+           BODY808_LONG_AXIS     = (    0.                        )
+ 
+ 
+           BODY808_NUT_PREC_RA   = (    0.70      0.       0.      0.
+                                        0.        0.      -0.05    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+ 
+           BODY808_NUT_PREC_DEC  = (   -0.51      0.       0.      0.
+                                        0.        0.      -0.04    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+ 
+           BODY808_NUT_PREC_PM   = (   -0.48      0.       0.      0.
+                                        0.        0.       0.04    0.
+                                        0.        0.       0.      0.
+                                        0.        0.       0.      0.
+                                        0.                             )
+   
+        \begintext
+  
+ 
+ 
+ 
+ 
+Satellites of Pluto
+ 
+     Charon
+ 
+        Old values:
+        
+           Values are from the 2003 IAU report. 
+ 
+           body901_pole_ra       = (   313.02     0.         0. )
+           body901_pole_dec      = (     9.09     0.         0. )
+           body901_pm            = (    56.77   -56.3623195  0. )
+           body901_long_axis     = (     0.                     )
+               
+        Current values:
+ 
+        \begindata
+ 
+           BODY901_POLE_RA       = (   312.993    0.         0. )
+           BODY901_POLE_DEC      = (     6.163    0.         0. )
+           BODY901_PM            = (    57.305  -56.3625225  0. )
+           BODY901_LONG_AXIS     = (     0.                     )
+
+        \begintext
+ 
+ 
+ 
+Orientation constants for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+
+19P/Borrelly
+
+
+        Current values:
+ 
+        \begindata
+
+           BODY1000005_POLE_RA       = (   218.5      0.         0.  )
+           BODY1000005_POLE_DEC      = (   -12.5      0.         0.  )
+           BODY1000005_PM            = (   000.     390.0        0.  )
+           BODY1000005_LONG_AXIS     = (     0.                      )
+ 
+        \begintext
+
+
+
+9P/Tempel 1
+
+
+        Current values:
+ 
+        \begindata
+
+           BODY1000093_POLE_RA       = (   294.       0.         0.  )
+           BODY1000093_POLE_DEC      = (    73.       0.         0.  )
+           BODY1000093_PM            = (   252.63   212.064      0.  )
+           BODY1000093_LONG_AXIS     = (     0.                      )
+ 
+        \begintext
+
+
+Vesta
+
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY2000004_POLE_RA       = (   301.      0.         0.  )
+           BODY2000004_POLE_DEC      = (    41.      0.         0.  )
+           BODY2000004_PM            = (   292.   1617.332776   0.  )
+           BODY2000004_LONG_AXIS     = (     0.                     )
+ 
+        \begintext
+
+Eros
+
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+
+           BODY2000433_POLE_RA       = (   11.35       0.           0. )
+           BODY2000433_POLE_DEC      = (   17.22       0.           0. )
+           BODY2000433_PM            = (  326.07    1639.38864745   0. )
+           BODY2000433_LONG_AXIS     = (    0.                         )
+ 
+        \begintext
+
+
+Itokawa
+
+
+        Current values:
+ 
+        \begindata
+
+           BODY2025143_POLE_RA       = (   90.53       0.           0. )
+           BODY2025143_POLE_DEC      = (  -66.30       0.           0. )
+           BODY2025143_PM            = (  000.0      712.143        0. )
+           BODY2025143_LONG_AXIS     = (    0.                         )
+ 
+        \begintext
+
+
+
+Ida
+
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+
+        Current values:
+ 
+        \begindata
+ 
+           BODY2431010_POLE_RA       = (  168.76      0.         0. )
+           BODY2431010_POLE_DEC      = (   -2.88      0.         0. )
+           BODY2431010_PM            = (  265.95  +1864.6280070  0. )
+           BODY2431010_LONG_AXIS     = (    0.                      )
+ 
+        \begintext
+
+Gaspra
+
+        Old values:
+        
+           Values are unchanged in the 2006 IAU report. 
+               
+        Current values:
+ 
+        \begindata 
+ 
+           BODY9511010_POLE_RA       = (   9.47     0.         0. )
+           BODY9511010_POLE_DEC      = (  26.70     0.         0. )
+           BODY9511010_PM            = (  83.67  1226.9114850  0. )
+           BODY9511010_LONG_AXIS     = (   0.                     )
+
+        \begintext
+
+
+
+
+
+
+
+
+
+ 
+Radii of Sun and Planets
+--------------------------------------------------------
+ 
+ 
+Sun
+ 
+     Value for the Sun is from the [3], page K7.
+ 
+        \begindata
+ 
+        BODY10_RADII      = (   696000.     696000.      696000.     )
+ 
+        \begintext
+ 
+ 
+Mercury
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY199_RADII     = ( 2439.7   2439.7   2439.7 )
+ 
+        \begintext
+ 
+ 
+Venus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY299_RADII     = ( 6051.8   6051.8   6051.8 )
+ 
+        \begintext
+ 
+ 
+Earth
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+
+        \begindata
+ 
+        BODY399_RADII     = ( 6378.14   6378.14   6356.75 )
+ 
+        \begintext
+ 
+ 
+Mars
+ 
+ 
+     Old values:
+
+        body499_radii       = (     3397.      3397.         3375.     )
+ 
+     Current values:
+
+
+        The IAU report gives separate values for the north and south
+        polar radii:
+
+           north:  3373.19
+           south:  3379.21 
+
+        We use the average of these values as the polar radius for
+        the triaxial model.
+ 
+        \begindata
+ 
+        BODY499_RADII       = ( 3396.19   3396.19   3376.20 )
+ 
+        \begintext
+ 
+ 
+ 
+Jupiter
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY599_RADII     = ( 71492   71492   66854 )
+ 
+        \begintext
+ 
+ 
+ 
+Saturn
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY699_RADII     = ( 60268   60268   54364 )
+ 
+        \begintext
+ 
+ 
+ 
+Uranus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY799_RADII     = ( 25559   25559   24973 )
+ 
+        \begintext
+ 
+ 
+ 
+Neptune
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+  
+     Current values:
+ 
+        (Values are for the 1 bar pressure level.)
+ 
+        \begindata
+ 
+        BODY899_RADII     = ( 24764   24764  24341 )
+ 
+        \begintext
+ 
+ 
+ 
+Pluto
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY999_RADII     = ( 1195   1195   1195 )
+ 
+        \begintext
+ 
+
+
+
+Radii of Satellites
+--------------------------------------------------------
+ 
+ 
+Moon
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY301_RADII     = ( 1737.4   1737.4   1737.4 )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Mars
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY401_RADII     = ( 13.4    11.2    9.2 )
+        BODY402_RADII     = (  7.5     6.1    5.2 )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Jupiter
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report.
+ 
+     Current values:
+         
+        \begindata
+ 
+        BODY501_RADII     = ( 1829.4   1819.3   1815.7  )
+        BODY502_RADII     = ( 1564.13  1561.23  1560.93 )
+        BODY503_RADII     = ( 2632.4   2632.29  2632.35 )
+        BODY504_RADII     = ( 2409.4   2409.2   2409.3  )
+        BODY505_RADII     = (  125       73       64    )
+ 
+        \begintext
+ 
+        Only mean radii are available in the 2003 IAU report for bodies
+        506-513.
+ 
+        \begindata
+ 
+        BODY506_RADII    = (    85       85       85   )
+        BODY507_RADII    = (    40       40       40   )
+        BODY508_RADII    = (    18       18       18   )
+        BODY509_RADII    = (    14       14       14   )
+        BODY510_RADII    = (    12       12       12   )
+        BODY511_RADII    = (    15       15       15   )
+        BODY512_RADII    = (    10       10       10   )
+        BODY513_RADII    = (     5        5        5   )
+        BODY514_RADII    = (    58       49       42   )
+        BODY515_RADII    = (    10        8        7   )
+ 
+        \begintext
+ 
+        The value for the second radius for body 516 is not given in 
+        2003 IAU report.   The values given are:
+ 
+           BODY516_RADII    = (  30   ---   20   )
+ 
+        For use within the SPICE system, we use only the mean radius.
+        \begindata
+ 
+        BODY516_RADII    = (  21.5   21.5  21.5  )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Saturn
+ 
+ 
+     Old values:
+ 
+        Values are from the 2003 IAU report.
+    
+        body601_radii     = (  209.1   196.2   191.4 )
+        body602_radii     = (  256.3   247.3   244.6 )
+        body603_radii     = (  535.6   528.2   525.8 )
+        body604_radii     = (  560     560     560   )
+        body605_radii     = (  764     764     764   )
+        body606_radii     = ( 2575    2575    2575   )
+        body607_radii     = (  164     130     107   )
+        body608_radii     = (  718     718     718   )
+        body609_radii     = (  115     110     105   )
+        body610_radii     = (   97.0    95.0    77.0 )
+        body611_radii     = (   69.0    55.0    55.0 )
+ 
+ 
+        Only the first equatorial radius for Helene (body 612) was given in the
+        2003 IAU report:
+ 
+            body612_radii     = (       17.5        ---          ---     )
+ 
+        The mean radius was 16km; we used this radius for all three axes, as
+        we do for the satellites for which only the mean radius is available.
+ 
+ 
+        body612_radii     = (   16      16       16  )
+        body613_radii     = (   15      12.5     7.5 )
+        body614_radii     = (   15.0     8.0     8.0 )
+        body615_radii     = (   18.5    17.2    13.5 )
+        body616_radii     = (   74.0    50.0    34.0 )
+        body617_radii     = (   55.0    44.0    31.0 )
+  
+      
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY601_RADII     = (  207.4     196.8     190.6  )
+        BODY602_RADII     = (  256.6     251.4     248.3  )
+        BODY603_RADII     = (  540.4     531.1     527.5  )
+        BODY604_RADII     = (  563.8     561.0     560.3  )
+        BODY605_RADII     = (  767.2     762.5     763.1  )
+        BODY606_RADII     = ( 2575      2575      2575    )
+        BODY607_RADII     = (  164       130       107    )
+        BODY608_RADII     = (  747.4     747.4     712.4  )
+        BODY609_RADII     = (  108.6     107.7     101.5  )
+        BODY610_RADII     = (   97.0      95.0      77.0  )
+        BODY611_RADII     = (   69.0      55.0      55.0  )
+ 
+        \begintext
+ 
+        Only the first equatorial radius for Helene (body 612) is given in the
+        2006 IAU report:
+ 
+            BODY612_RADII     = (       17.5        ---          ---     )
+ 
+        The mean radius is 16km; we use this radius for all three axes, as
+        we do for the satellites for which only the mean radius is available.
+ 
+ 
+        \begindata
+ 
+        BODY612_RADII     = (  17.5      17.5      17.5  )
+        BODY613_RADII     = (  15        12.5       7.5  )
+        BODY614_RADII     = (  15.0       8.0       8.0  )
+        BODY615_RADII     = (  18.5      17.2      13.5  )
+        BODY616_RADII     = (  74.0      50.0      34.0  )
+        BODY617_RADII     = (  55.0      44.0      31.0  )
+ 
+        \begintext
+ 
+ 
+         For Pan, only a mean radius is given in the 2006 report.
+ 
+        \begindata
+ 
+        BODY618_RADII     = (   10       10     10   )
+ 
+        \begintext
+ 
+ 
+ 
+Satellites of Uranus
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+ 
+     Current values:
+ 
+        \begindata
+ 
+        BODY701_RADII     = (  581.1   577.9   577.7 )
+        BODY702_RADII     = (  584.7   584.7   584.7 )
+        BODY703_RADII     = (  788.9   788.9   788.9 )
+        BODY704_RADII     = (  761.4   761.4   761.4 )
+        BODY705_RADII     = (  240.4   234.2   232.9 )
+ 
+        \begintext
+ 
+        The 2000 report gives only mean radii for satellites 706--715.
+ 
+        \begindata
+ 
+        BODY706_RADII     = (   13      13      13 )
+        BODY707_RADII     = (   15      15      15 )
+        BODY708_RADII     = (   21      21      21 )
+        BODY709_RADII     = (   31      31      31 )
+        BODY710_RADII     = (   27      27      27 )
+        BODY711_RADII     = (   42      42      42 )
+        BODY712_RADII     = (   54      54      54 )
+        BODY713_RADII     = (   27      27      27 )
+        BODY714_RADII     = (   33      33      33 )
+        BODY715_RADII     = (   77      77      77 )
+ 
+        \begintext
+ 
+ 
+ 
+ 
+Satellites of Neptune
+ 
+ 
+     Old values:
+ 
+        Values are unchanged in the 2006 IAU report. 
+ 
+     Current values:
+ 
+        The 2000 report gives mean radii only for bodies 801-806.
+ 
+        \begindata
+ 
+        BODY801_RADII     = ( 1352.6  1352.6  1352.6 )
+        BODY802_RADII     = (  170     170     170   )
+        BODY803_RADII     = (   29      29     29    )
+        BODY804_RADII     = (   40      40     40    )
+        BODY805_RADII     = (   74      74     74    )
+        BODY806_RADII     = (   79      79     79    )
+ 
+        \begintext
+ 
+ 
+        The second equatorial radius for Larissa is not given in the 2000
+        report.  The available values are:
+ 
+            BODY807_RADII     = (   104     ---     89   )
+ 
+        For use within the SPICE system, we use only the mean radius.
+        \begindata
+ 
+        BODY807_RADII     = (   96      96     96   )
+        BODY808_RADII     = (  218     208    201   )
+ 
+        \begintext
+ 
+ 
+ 
+ 
+Satellites of Pluto
+ 
+     
+     Old values:
+ 
+        Values are from the 2003 IAU report. 
+
+        BODY901_RADII     = (  593     593    593   )
+             
+     Current values:
+ 
+        \begindata
+ 
+        BODY901_RADII     = (  605     605    605   )
+ 
+        \begintext
+ 
+
+
+Radii for Selected Comets and Asteroids
+--------------------------------------------------------
+
+
+19P/Borrelly
+
+
+     Current values:
+ 
+
+        The value in the data assignment below is the 
+        "effective radius."
+
+        The first principal axis length is 
+
+           3.5 km
+
+        The lengths of the other semi-axes are not provided
+        by [1].
+
+        \begindata
+ 
+        BODY1000005_RADII     = (  4.22   4.22   4.22  )
+ 
+        \begintext
+
+
+
+Halley
+
+
+     Current values:
+
+        \begindata
+ 
+        BODY1000036_RADII     = (  8.0   4.0   4.0  )
+ 
+        \begintext
+
+
+
+9P/Tempel 1
+
+
+     Current values:
+
+
+        The value in the data assignment below is the 
+        "effective radius."
+            
+        According to [1]:
+
+           The maximum and minimum radii are not properly 
+           the values of the principal semi-axes, they
+           are half the maximum and minimum values of the
+           diameter. Due to the large deviations from a
+           simple ellipsoid, they may not correspond with
+           measurements along the principal axes, or be
+           orthogonal to each other.
+
+        \begindata
+ 
+        BODY1000093_RADII     = (  3.0   3.0   3.0  )
+ 
+        \begintext
+
+
+81P/Wild 2
+
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY1000107_RADII     = (  2.7   1.9   1.5 )
+ 
+        \begintext
+
+
+Ceres
+
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2000001_RADII     = ( 487.3  487.3  454.7 )
+ 
+        \begintext
+
+
+Vesta
+
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2000004_RADII     = ( 289.  280.  229.  )
+ 
+        \begintext
+
+
+Toutatis
+
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2004179_RADII     = (  2.13  1.015  0.85  )
+ 
+        \begintext
+
+ 
+Kleopatra
+
+
+     Old values:
+
+        Values are from the 2003 report.
+
+ 
+        body2000216_radii     = (   108.5      47    40.5  )
+ 
+
+     Current values:
+ 
+ 
+        No values are provided in the 2006 report.
+
+
+Mathilde
+
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2000253_RADII     = (  33.   24.   23.  )
+ 
+        \begintext
+       
+Eros
+ 
+
+     Current values:
+ 
+ 
+        \begindata
+ 
+        BODY2000433_RADII     = (  17.0   5.5   5.5  )
+ 
+        \begintext
+
+
+Itokawa
+
+
+     Current values:
+
+
+        \begindata
+ 
+        BODY2025143_RADII     = (  0.535   0.294   0.209  )
+ 
+        \begintext
+
+
+
+Gaspra
+
+     
+     Current values:
+ 
+ 
+        \begindata
+ 
+        BODY9511010_RADII     = (    9.1    5.2    4.4 )
+ 
+        \begintext
+
+        
+        
+        
+Ida
+
+     
+     Current values:
+ 
+ 
+        \begindata
+ 
+        BODY2431010_RADII     = (   26.8   12.0    7.6 )
+ 
+        \begintext
+
+        
+
+===========================================================================
+End of file pck00009.tpc
+===========================================================================
+
+
+
diff --git a/tests/pytests/data/isds/dawnvir_isd.json b/tests/pytests/data/isds/dawnvir_isd.json
new file mode 100644
index 0000000..90674bb
--- /dev/null
+++ b/tests/pytests/data/isds/dawnvir_isd.json
@@ -0,0 +1,1972 @@
+{
+  "isis_camera_version": 1,
+  "image_lines": 60,
+  "image_samples": 256,
+  "name_platform": "DAWN",
+  "name_sensor": "VIR",
+  "reference_height": {
+    "maxheight": 1000,
+    "minheight": -1000,
+    "unit": "m"
+  },
+  "name_model": "USGS_ASTRO_LINE_SCANNER_SENSOR_MODEL",
+  "interpolation_method": "lagrange",
+  "line_scan_rate": [
+    [
+      0.5,
+      -480.24997586011887,
+      16
+    ],
+    [
+      1.5,
+      -464.24997663497925,
+      16
+    ],
+    [
+      2.5,
+      -448.2499774694443,
+      16
+    ],
+    [
+      3.5,
+      -432.24997824430466,
+      16
+    ],
+    [
+      4.5,
+      -416.2499790787697,
+      16
+    ],
+    [
+      5.5,
+      -400.24997985363007,
+      16
+    ],
+    [
+      6.5,
+      -384.2499806880951,
+      16
+    ],
+    [
+      7.5,
+      -368.2499814629555,
+      16
+    ],
+    [
+      8.5,
+      -352.24998223781586,
+      16
+    ],
+    [
+      9.5,
+      -336.2499830722809,
+      16
+    ],
+    [
+      10.5,
+      -320.24998384714127,
+      16
+    ],
+    [
+      11.5,
+      -304.24998474121094,
+      16
+    ],
+    [
+      12.5,
+      -288.2499855160713,
+      16
+    ],
+    [
+      13.5,
+      -272.24998635053635,
+      16
+    ],
+    [
+      14.5,
+      -256.24998712539673,
+      16
+    ],
+    [
+      15.5,
+      -240.2499879002571,
+      16
+    ],
+    [
+      16.5,
+      -224.24998873472214,
+      16
+    ],
+    [
+      17.5,
+      -208.24998950958252,
+      16
+    ],
+    [
+      18.5,
+      -192.24999034404755,
+      16
+    ],
+    [
+      19.5,
+      -176.24999111890793,
+      16
+    ],
+    [
+      20.5,
+      -160.24999195337296,
+      16
+    ],
+    [
+      21.5,
+      -144.24999272823334,
+      16
+    ],
+    [
+      22.5,
+      -128.249993622303,
+      16
+    ],
+    [
+      23.5,
+      -112.24999439716339,
+      16
+    ],
+    [
+      24.5,
+      -96.24999517202377,
+      16
+    ],
+    [
+      25.5,
+      -80.2499960064888,
+      16
+    ],
+    [
+      26.5,
+      -64.24999678134918,
+      16
+    ],
+    [
+      27.5,
+      -48.24999761581421,
+      16
+    ],
+    [
+      28.5,
+      -32.24999839067459,
+      16
+    ],
+    [
+      29.5,
+      -16.249999225139618,
+      16
+    ],
+    [
+      30.5,
+      -0.25,
+      16
+    ],
+    [
+      31.5,
+      15.749999225139618,
+      16
+    ],
+    [
+      32.5,
+      31.74999839067459,
+      16
+    ],
+    [
+      33.5,
+      47.74999761581421,
+      16
+    ],
+    [
+      34.5,
+      63.74999672174454,
+      16
+    ],
+    [
+      35.5,
+      79.74999594688416,
+      16
+    ],
+    [
+      36.5,
+      95.74999511241913,
+      16
+    ],
+    [
+      37.5,
+      111.74999433755875,
+      16
+    ],
+    [
+      38.5,
+      127.74999356269836,
+      16
+    ],
+    [
+      39.5,
+      143.74999272823334,
+      16
+    ],
+    [
+      40.5,
+      159.74999195337296,
+      16
+    ],
+    [
+      41.5,
+      175.74999111890793,
+      16
+    ],
+    [
+      42.5,
+      191.74999034404755,
+      16
+    ],
+    [
+      43.5,
+      207.74998950958252,
+      16
+    ],
+    [
+      44.5,
+      223.74998873472214,
+      16
+    ],
+    [
+      45.5,
+      239.7499879002571,
+      16
+    ],
+    [
+      46.5,
+      255.74998706579208,
+      16
+    ],
+    [
+      47.5,
+      271.7499862909317,
+      16
+    ],
+    [
+      48.5,
+      287.7499854564667,
+      16
+    ],
+    [
+      49.5,
+      303.7499846816063,
+      16
+    ],
+    [
+      50.5,
+      319.74998384714127,
+      16
+    ],
+    [
+      51.5,
+      335.7499830722809,
+      16
+    ],
+    [
+      52.5,
+      351.7499822974205,
+      16
+    ],
+    [
+      53.5,
+      367.7499814629555,
+      16
+    ],
+    [
+      54.5,
+      383.7499806880951,
+      16
+    ],
+    [
+      55.5,
+      399.74997985363007,
+      16
+    ],
+    [
+      56.5,
+      415.7499790787697,
+      16
+    ],
+    [
+      57.5,
+      431.7499781847,
+      16
+    ],
+    [
+      58.5,
+      447.74997740983963,
+      16
+    ],
+    [
+      59.5,
+      463.7499765753746,
+      16
+    ],
+    [
+      60.5,
+      479.7499765753746,
+      16
+    ]
+  ],
+  "starting_ephemeris_time": 362681633.6134121,
+  "center_ephemeris_time": 362682113.86338794,
+  "radii": {
+    "semimajor": 289.0,
+    "semiminor": 229.0,
+    "unit": "km"
+  },
+  "body_rotation": {
+    "time_dependent_frames": [
+      2000004,
+      1
+    ],
+    "ck_table_start_time": 362681633.6134121,
+    "ck_table_end_time": 362682578.1133645,
+    "ck_table_original_size": 2,
+    "ephemeris_times": [
+      362681633.6134121,
+      362682578.1133645
+    ],
+    "quaternions": [
+      [
+        -0.08339426680875163,
+        0.2825790922154143,
+        -0.2899354389711647,
+        0.9105667982826637
+      ],
+      [
+        -0.05753008804150366,
+        -0.23466576568440176,
+        0.32991738442289315,
+        -0.9125660451941258
+      ]
+    ],
+    "angular_velocities": [
+      [
+        0.00015233084023562584,
+        -0.0001879049550186647,
+        0.0002196059580430743
+      ],
+      [
+        0.00015233084023562581,
+        -0.00018790495501866468,
+        0.00021960595804307426
+      ]
+    ],
+    "reference_frame": 1
+  },
+  "instrument_pointing": {
+    "time_dependent_frames": [
+      -203223,
+      1
+    ],
+    "ck_table_start_time": 362681633.8634121,
+    "ck_table_end_time": 362682577.8633645,
+    "ck_table_original_size": 60,
+    "ephemeris_times": [
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+    ],
+    "quaternions": [
+      [
+        0.12043634994578895,
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+      ],
+      [
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+      ],
+      [
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+      ],
+      [
+        0.12036200012115673,
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+        -0.6369149474098392
+      ],
+      [
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+      ],
+      [
+        0.12018019095675472,
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+        0.7128543880963021,
+        -0.6368405333934426
+      ],
+      [
+        0.12009236919512459,
+        -0.2680970403949592,
+        0.7128678608412475,
+        -0.6368054748290009
+      ],
+      [
+        0.12000733160344947,
+        -0.2681740477163368,
+        0.7128812737601151,
+        -0.6367740651243671
+      ],
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+        -1.5764102324061096
+      ],
+      [
+        -18.061712341666222,
+        -9.88740987084806,
+        -1.5768379395399243
+      ]
+    ],
+    "reference_frame": 1
+  }
+}
\ No newline at end of file
diff --git a/tests/pytests/test_dawn_drivers.py b/tests/pytests/test_dawn_drivers.py
index 62f2e8b..d311d6f 100644
--- a/tests/pytests/test_dawn_drivers.py
+++ b/tests/pytests/test_dawn_drivers.py
@@ -6,16 +6,44 @@ from importlib import reload
 import json
 
 import unittest
+from unittest import mock
 from unittest.mock import patch
 from ale.drivers import AleJsonEncoder
 from conftest import get_image_label, get_image_kernels, get_isd, convert_kernels, compare_dicts
 
 import ale
-from ale.drivers.dawn_drivers import DawnFcPds3NaifSpiceDriver, DawnFcIsisLabelNaifSpiceDriver
+from ale.drivers.dawn_drivers import DawnFcPds3NaifSpiceDriver, DawnFcIsisLabelNaifSpiceDriver, DawnVirIsisLabelNaifSpiceDriver
 
+housekeeping_dict = {'ScetTimeClock': ['362681634.09', '362681650.09', '362681666.09', '362681682.09', '362681698.09', '362681714.09', 
+                                       '362681730.09', '362681746.09', '362681762.09', '362681778.09', '362681794.09', '362681810.09', 
+                                       '362681826.09', '362681842.09', '362681858.09', '362681874.09', '362681890.09', '362681906.09', 
+                                       '362681922.09', '362681938.09', '362681954.09', '362681970.09', '362681986.09', '362682002.09', 
+                                       '362682018.09', '362682034.09', '362682050.09', '362682066.09', '362682082.09', '362682098.09', 
+                                       '362682114.09', '362682130.09', '362682146.09', '362682162.09', '362682178.09', '362682194.09', 
+                                       '362682210.09', '362682226.09', '362682242.09', '362682258.09', '362682274.09', '362682290.09', 
+                                       '362682306.09', '362682322.09', '362682338.09', '362682354.09', '362682370.09', '362682386.09', 
+                                       '362682402.09', '362682418.09', '362682434.09', '362682450.09', '362682466.09', '362682482.09', 
+                                       '362682498.09', '362682514.09', '362682530.09', '362682546.09', '362682562.09', '362682578.09'], 
+                     'ShutterStatus': ['closed', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 
+                                       'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 
+                                       'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 
+                                       'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 
+                                       'open', 'open', 'open', 'open', 'open', 'open', 'open', 'open', 'closed'], 
+                     'MirrorSin': [0.066178, -0.037118, -0.037118, -0.032479, -0.028083, -0.023443, -0.019048, -0.014652, -0.010012, -0.005617, 
+                                  -0.000977, 0.003175, 0.007814, 0.01221, 0.016606, 0.021245, 0.025641, 0.030281, 0.034676, 0.039072, 0.043712, 
+                                  0.048107, 0.052747, 0.057143, 0.061538, 0.066178, 0.070574, 0.075214, 0.079609, 0.084005, 0.088645, 0.09304, 
+                                  0.097436, 0.102076, 0.106471, 0.110867, 0.115507, 0.119902, 0.124298, 0.128938, 0.133333, 0.137729, 0.142124, 
+                                  0.146764, 0.15116, 0.155555, 0.159951, 0.164347, 0.168986, 0.173382, 0.177778, 0.182173, 0.186569, 0.190964, 
+                                  0.19536, 0.199756, 0.204151, 0.208547, 0.212942, 0.217338], 
+                     'MirrorCos': [0.997557, 0.999266, 0.999266, 0.999266, 0.999511, 0.999511, 0.999755, 0.999755, 0.999755, 0.999755, 0.999755, 
+                                   0.999755, 0.999755, 0.999755, 0.999755, 0.999755, 0.999511, 0.999511, 0.999266, 0.999022, 0.999022, 0.998778, 
+                                   0.998534, 0.99829, 0.998045, 0.997557, 0.997313, 0.997069, 0.99658, 0.996336, 0.995848, 0.995603, 0.995115, 
+                                   0.994627, 0.994138, 0.99365, 0.993161, 0.992673, 0.992185, 0.991452, 0.990964, 0.990231, 0.989743, 0.98901, 
+                                   0.988277, 0.987789, 0.987056, 0.986324, 0.985591, 0.984614, 0.983882, 0.983149, 0.982172, 0.98144, 0.980463, 
+                                   0.97973, 0.978754, 0.977777, 0.9768, 0.975823]}
 
 @pytest.fixture(scope="module", autouse=True)
-def test_kernels():
+def fc_kernels():
     kernels = get_image_kernels('FC21A0038582_15170161546F6F')
     updated_kernels, binary_kernels = convert_kernels(kernels)
     yield updated_kernels
@@ -23,7 +51,7 @@ def test_kernels():
         os.remove(kern)
 
 @pytest.mark.parametrize("label_type", ['pds3', 'isis3'])
-def test_load(test_kernels, label_type):
+def test_fc_load(fc_kernels, label_type):
     if label_type == 'isis3':
         label_prefix_file = "FC21A0038582_15170161546F6G"
         compare_dict = get_isd("dawnfc_isis")
@@ -33,13 +61,33 @@ def test_load(test_kernels, label_type):
 
     label_file = get_image_label(label_prefix_file, label_type=label_type)
 
-    isd_str = ale.loads(label_file, props={'kernels': test_kernels})
+    isd_str = ale.loads(label_file, props={'kernels': fc_kernels})
     isd_obj = json.loads(isd_str)
     # print(json.dumps(isd_obj, indent=2))
     assert compare_dicts(isd_obj, compare_dict) == []
 
-# ========= Test pds3label and naifspice driver =========
-class test_pds3_naif(unittest.TestCase):
+@pytest.fixture(scope="module", autouse=True)
+def vir_kernels():
+    kernels = get_image_kernels('VIR_IR_1A_1_362681634_1')
+    updated_kernels, binary_kernels = convert_kernels(kernels)
+    yield updated_kernels
+    for kern in binary_kernels:
+        os.remove(kern)
+
+def test_vir_load(vir_kernels):
+    label_file = get_image_label("VIR_IR_1A_1_362681634_1", label_type="isis3")
+    with patch('ale.drivers.dawn_drivers.read_table_data', return_value=12345) as read_table_data, \
+        patch('ale.drivers.dawn_drivers.parse_table', return_value=housekeeping_dict) as parse_table:
+
+        compare_dict = get_isd("dawnvir")
+
+        isd_str = ale.loads(label_file, props={"kernels": vir_kernels, "nadir": False}, verbose=False)
+        isd_obj = json.loads(isd_str)
+        x = compare_dicts(isd_obj, compare_dict)
+        assert x == []
+
+# ========= Test dawn fc pds3label and naifspice driver =========
+class test_dawn_fc_pds3_naif(unittest.TestCase):
 
     def setUp(self):
         label = get_image_label("FC21A0038582_15170161546F6F", "pds3")
@@ -101,12 +149,12 @@ class test_pds3_naif(unittest.TestCase):
             bods2c.assert_called_with('DAWN_FC2_FILTER_6')
             gdpool.assert_called_with('INS54321_CCD_CENTER', 0, 2)
 
-# ========= Test isis3label and naifspice driver =========
-class test_isis3_naif(unittest.TestCase):
+# ========= Test dawn fc isis3label and naifspice driver =========
+class test_dawn_fc_isis3_naif(unittest.TestCase):
 
     def setUp(self):
         label = get_image_label("FC21A0038582_15170161546F6G", "isis3");
-        self.driver = DawnFcIsisLabelNaifSpiceDriver(label);
+        self.driver = DawnFcIsisLabelNaifSpiceDriver(label)
 
     def test_short_mission_name(self):
         assert self.driver.short_mission_name == 'dawn'
@@ -125,3 +173,89 @@ class test_isis3_naif(unittest.TestCase):
             assert self.driver.ephemeris_start_time == 12345.193
             scs2e.assert_called_with(-203, '488002612:246')
 
+
+# ========= Test dawn vir isis3label and naifspice driver =========
+class test_dawn_vir_isis3_naif(unittest.TestCase):
+    def setUp(self):
+        label = get_image_label("VIR_IR_1A_1_362681634_1", "isis3")
+        self.driver = DawnVirIsisLabelNaifSpiceDriver(label)
+
+    def test_instrument_id(self):
+        assert self.driver.instrument_id == "Visual and Infrared Spectrometer"
+
+    def test_sensor_name(self):
+         assert self.driver.sensor_name == "VIR"
+
+    def test_line_exposure_duration(self):
+        np.testing.assert_array_equal(self.driver.line_exposure_duration, [0.5])
+
+    def test_focal_length(self):
+        with patch('ale.drivers.dawn_drivers.spice.gdpool', return_value=[152.0]) as gdpool:
+             assert self.driver.focal_length == 152.0
+
+    def test_ikid(self):
+        assert self.driver.ikid == -203213
+
+    def test_sensor_frame_id(self):
+        ale.spice_root = "/foo/bar"
+        assert self.driver.sensor_frame_id == -203223
+
+    def test_line_scan_rate(self):
+        with patch('ale.drivers.dawn_drivers.read_table_data', return_value=12345) as read_table_data, \
+             patch('ale.drivers.dawn_drivers.spice.scs2e', return_value=362681649.6134113) as scs2e, \
+             patch('ale.drivers.dawn_drivers.parse_table', return_value={'ScetTimeClock': ['362681634.09', '362681650.09', '362681666.09'], \
+                                                                'ShutterStatus': ['closed', 'open', 'open'], \
+                                                                'MirrorSin': [0.066178, -0.037118, -0.037118], \
+                                                                'MirrorCos': [0.997557, 0.999266, 0.999266]}) as parse_table:
+            
+            assert self.driver.line_scan_rate == ([0.5, 1.5, 2.5, 3.5], [-0.25, -0.25, -0.25, 15.75], [16, 16, 16, 16])
+
+    def test_sensor_model_version(self):
+        assert self.driver.sensor_model_version == 1
+
+    def test_optical_angles(self):
+        with patch('ale.drivers.dawn_drivers.read_table_data', return_value=12345) as read_table_data, \
+             patch('ale.drivers.dawn_drivers.parse_table', return_value={'ScetTimeClock': ['362681634.09', '362681650.09', '362681666.09'], \
+                                                                'ShutterStatus': ['closed', 'open', 'open'], \
+                                                                'MirrorSin': [0.066178, -0.037118, -0.037118], \
+                                                                'MirrorCos': [0.997557, 0.999266, 0.999266]}) as parse_table:
+            
+            assert self.driver.optical_angles == [-0.005747392247876606, -0.005747392247876606, -0.005747392247876606]
+
+    def test_hk_ephemeris_time(self):
+        with patch('ale.drivers.dawn_drivers.read_table_data', return_value=12345) as read_table_data, \
+             patch('ale.drivers.dawn_drivers.spice.scs2e', return_value=362681633.8634121) as scs2e, \
+             patch('ale.drivers.dawn_drivers.parse_table', return_value={'ScetTimeClock': ['362681634.09', '362681650.09', '362681666.09'], \
+                                                                'ShutterStatus': ['closed', 'open', 'open'], \
+                                                                'MirrorSin': [0.066178, -0.037118, -0.037118], \
+                                                                'MirrorCos': [0.997557, 0.999266, 0.999266]}) as parse_table:
+            
+            assert self.driver.hk_ephemeris_time == [362681633.8634121, 362681633.8634121, 362681633.8634121]
+
+    def test_ephemeris_start_time(self):
+        with patch('ale.drivers.dawn_drivers.read_table_data', return_value=12345) as read_table_data, \
+             patch('ale.drivers.dawn_drivers.spice.scs2e', return_value=362681633.8634121) as scs2e, \
+             patch('ale.drivers.dawn_drivers.parse_table', return_value={'ScetTimeClock': ['362681634.09', '362681650.09', '362681666.09'], \
+                                                                'ShutterStatus': ['closed', 'open', 'open'], \
+                                                                'MirrorSin': [0.066178, -0.037118, -0.037118], \
+                                                                'MirrorCos': [0.997557, 0.999266, 0.999266]}) as parse_table:
+
+             assert self.driver.ephemeris_start_time == 362681633.8634121 - (0.5 / 2)
+
+    def test_ephemeris_stop_time(self):
+        with patch('ale.drivers.dawn_drivers.read_table_data', return_value=12345) as read_table_data, \
+             patch('ale.drivers.dawn_drivers.spice.scs2e', return_value=362682578.1133645) as scs2e, \
+             patch('ale.drivers.dawn_drivers.parse_table', return_value={'ScetTimeClock': ['362681634.09', '362681650.09', '362681666.09'], \
+                                                                'ShutterStatus': ['closed', 'open', 'open'], \
+                                                                'MirrorSin': [0.066178, -0.037118, -0.037118], \
+                                                                'MirrorCos': [0.997557, 0.999266, 0.999266]}) as parse_table:
+
+             assert self.driver.ephemeris_stop_time == 362682578.1133645 + (0.5 / 2)
+ 
+    def test_is_calibrated(self):
+        assert self.driver.is_calibrated == False
+
+    def test_has_articulation_kernel(self):
+        ale.spice_root = "/foo/bar"
+        assert self.driver.has_articulation_kernel == False
+
-- 
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