This C-kernels was produced using the SPICE program "prediCkt" on
   2014-DEC-30 09:19:26.  The following files were provided in support
   of the construction of the attitude given in this kernel.
 
File
Type  Name
----  ------------------------------------------
SPK   /ftp/pub/naif/CASSINI/kernels/spk/140114AP_SCPSE_13290_17265.bsp
SPK   /ftp/pub/naif/CASSINI/kernels/spk/140114AP_SK_13290_17265.bsp
TEXT  /ftp/pub/naif/CASSINI/kernels/lsk/naif0010.tls
TEXT  /ftp/pub/naif/generic_kernels/pck/pck00010.tpc
 
 
 
   This C-kernel matches the specification given below to 0.05730 degrees.
 
 
   The text kernel used to specify the orientation of structures
   included in this file is given below.
 
   =============================================================
 
Predicted CASSINI Spacecraft Orientation CK File, Case 1
=========================================================================
 
   Created by Boris Semenov, December 30, 2014.
 
 
Abstract
--------------------------------------------------------
 
   This CK contains sample CASSINI spacecraft orientation. This file
   was generated by running prediCkt program with the set of setups
   provided in the sections below.
 
 
CASSINI SPICE Kernels Used in the prediCkt Run Generated This File
--------------------------------------------------------
 
   The kernels provided in support of the construction of the attitude
   given in this kernel are listed in the small comment block preceding
   this description. The SPK kernel providing the spacecraft trajectory
   (140114AP_SK_13290_17265.bsp) was suggested by Julie Bellerose, JPL
   on December 29, 2014.
 
   Note that since this CK contains predicted data it must be used
   with the SCLK kernel with which it was generated.
 
 
Orientation Mode Definition
--------------------------------------------------------
 
   This section defines CASSINI s/c orientation mode simulated in this
   file. The "Case 1"  mode is based on the following description
   provided by Jose Rodriguez, JPL in the e-mail from December 19, 2014
   with the subject "RE: Deliveries Round 3":
 
      Case 1.
      +Y  axis, sun-pointing
      +Z axis, Saturn north pointing (parallel to Saturn longitude lines)
 
   The following keywords define the this attitude:
 
      \begindata
 
         DIRECTION_SPECS  += ( 'ToSun       = POSITION OF SUN   -' )
         DIRECTION_SPECS  += (               'FROM CASSINI      -' )
         DIRECTION_SPECS  += (               'CORRECTION LT+S'     )
 
         DIRECTION_SPECS  += ( 'SaturnNorth = FIXED IAU_SATURN  -' )
         DIRECTION_SPECS  += (               'XYZ 0 0 1'           )
 
         ORIENTATION_NAME += 'Case1'
         PRIMARY          += '+Y = ToSun'
         SECONDARY        += '+Z = SaturnNorth'
         BASE_FRAME       += 'J2000'
 
      \begintext
 
 
Orientation Schedule
--------------------------------------------------------
 
   This section defines the CASSINI orientation schedule implemented by
   this CK file. The schedule below was provided by Susan Linick, JPL
   in the e-mail from December 29, 2014 with the subject "FW: Start and
   end times of F ring and proximal orbits data":
 
      F ring orbits
 
         FringPeriapse_1_states_Sat.txt
         Start time: 29-NOV-2016 13:30:41.0276 UTC
         End time: 09-DEC-2016 13:30:41.0274 UTC
 
         FringPeriapse_10_states_Sat.txt
         Start time: 02-FEB-2017 01:46:32.6451 UTC
         End time: 12-FEB-2017 01:46:32.6448 UTC
 
         FringPeriapse_20_states_Sat.txt
         Start time: 14-APR-2017 18:05:19.4006 UTC
         End time: 24-APR-2017 18:05:19.4006 UTC
 
      Proximal orbits
 
         Periapse_1_states_Sat.txt
         Start time: 21-APR-2017 09:03:34.8144 UTC
         End time: 01-MAY-2017 09:03:34.8145 UTC
 
         Periapse_11_states_Sat.txt
         Start time: 24-JUN-2017 22:16:07.5157 UTC
         End time: 04-JUL-2017 22:16:07.5160 UTC
 
         Periapse_22_states_Sat.txt
         Start time: 04-SEP-2017 00:25:05.2774 UTC
         End time: 14-SEP-2017 00:25:05.2775 UTC
 
   In the keyword assignments below the times are given as ETs:
 
      \begindata
 
          CK-SCLK               =  82
          CK-SPK                = -82
          CK-FRAMES             = -82000
 
          CK-82000ORIENTATION  += 'Case1'
          CK-82000START        += @2016-11-29-13:31:48.211
          CK-82000STOP         += @2016-12-09-13:31:48.211
 
          CK-82000ORIENTATION  += 'GOTO Case1'
          CK-82000START        += @2017-02-02-01:47:39.830
          CK-82000STOP         += @2017-02-12-01:47:39.830
 
          CK-82000ORIENTATION  += 'GOTO Case1'
          CK-82000START        += @2017-04-14-18:06:26.586
          CK-82000STOP         += @2017-04-24-18:06:26.586
 
          CK-82000ORIENTATION  += 'GOTO Case1'
          CK-82000START        += @2017-04-21-09:04:42.000
          CK-82000STOP         += @2017-05-01-09:04:42.000
 
          CK-82000ORIENTATION  += 'GOTO Case1'
          CK-82000START        += @2017-06-24-22:17:14.700
          CK-82000STOP         += @2017-07-04-22:17:14.700
 
          CK-82000ORIENTATION  += 'GOTO Case1'
          CK-82000START        += @2017-09-04-00:26:12.460
          CK-82000STOP         += @2017-09-14-00:26:12.460
 
      \begintext
 
End of prediCkt setup.