KPL/PCK \begindata CASSINI_PCK_VERSION = ( '2005-JUL-11' ) \begintext P_constants (PcK) SPICE kernel file Refer to the notes at the bottom of the file for help, contacts, version history, references, and Cassini-specific parameter descriptions. -------- SUN BODY10_GM from [3]. \begindata BODY10_GM = ( 132712440017.9870 ) \begintext -------- VENUS BODY2_GM, BODY299_GM from [4]. \begindata BODY2_GM = ( 324858.598826460 ) BODY299_GM = ( 324858.598826460 ) \begintext -------- EARTH BODY3_GM, BODY399_GM from [3]. \begindata BODY3_GM = ( 403503.233479087 ) BODY399_GM = ( 398600.4328969392 ) \begintext -------- JUPITER BODY5_GM, BODY599_GM from [3]. \begindata BODY5_GM = ( 126712767.8577960 ) BODY599_GM = ( 126686536.9610660 ) \begintext -------- SATURN BODY6_GM, BODY699_GM from [13]. Nonzero gravitational harmonics listed below are J2, J4, and J6 from [13] C22 and S22 from [1]. RA and DEC pole vectors from [13]. \begindata BODY6_GM = ( 37940584.32393724 ) BODY699_GM = ( 37931206.6260 ) BODY699_POLE_RA = ( 40.582524 -0.042290 0. ) BODY699_POLE_DEC = ( 83.537645 -0.004440 0. ) BODY699_JCOEF = ( 0.0, 0.016290795528, 0.0, -0.000932738706, 0.0, 0.000092477088) BODY699_CCOEF = ( 0.0, 0.0, 0.0000000000000 ) BODY699_SCOEF = ( 0.0, 0.0, 0.00000000 ) \begintext -------- URANUS BODY7_GM value from [3]. \begindata BODY7_GM = ( 5794549.007071874 ) \begintext -------- MOON BODY301_GM from [3]. \begindata BODY301_GM = ( 4902.800582147764 ) \begintext -------- MIMAS BODY601_GM from [13]. \begindata BODY601_GM = ( 2.530120927277264 ) \begintext -------- ENCELADUS BODY602_GM from [13]. \begindata BODY602_GM = ( 7.210665451438561 ) \begintext -------- TETHYS BODY603_GM from [13]. \begindata BODY603_GM = ( 41.20659404333172 ) \begintext -------- DIONE BODY604_GM from [13]. \begindata BODY604_GM = ( 73.11260446242133 ) \begintext -------- RHEA BODY605_GM from [13]. \begindata BODY605_GM = ( 154.0186476847478 ) \begintext -------- TITAN BODY606_GM from [13]. \begindata BODY606_GM = ( 8978.179855914042 ) \begintext -------- HYPERION BODY607_GM from [13]. \begindata BODY607_GM = ( 0.378215663233720 ) \begintext -------- IAPETUS BODY608_GM from [13]. \begindata BODY608_GM = ( 120.5079215829297 ) \begintext -------- PHOEBE BODY609_GM from [13]. \begindata BODY609_GM = ( 0.5532635543008535 ) \begintext Note that GM values >= 1.0 are packaged as is into 7CONIC_VEC commands for AACS to propagate the body's ephemeris. For GM values < 1.0, the value in the G_MASS parameter of the 7CONIC_VEC command is set to 1.0. One is the minimum value for the G_MASS parameter. The resetting of the G_MASS parameter to the minimum acceptable where the actual GM is < 1.0 is acceptable since Cassini will not pass close enough to any of the affected bodies for the gravitational mass to have an effect. -------- CONSTANTS AND NOTES FOR CASPER USERS \begindata BODY601_GM/PRIMARY = ( 6.59087D-08 ) BODY602_GM/PRIMARY = ( 1.29181D-07 ) BODY603_GM/PRIMARY = ( 1.1022D-06 ) BODY604_GM/PRIMARY = ( 1.92865D-06 ) BODY605_GM/PRIMARY = ( 4.05998D-06 ) BODY606_GM/PRIMARY = ( 2.36697D-04 ) BODY607_GM/PRIMARY = ( 2.60998D-08 ) BODY608_GM/PRIMARY = ( 2.79453D-06 ) BODY609_GM/PRIMARY = ( 1.26545D-08 ) BODY610_GM/PRIMARY = ( 3.38507D-09 ) BODY611_GM/PRIMARY = ( 9.41176D-10 ) BODY612_GM/PRIMARY = ( 4.48179D-11 ) BODY613_GM/PRIMARY = ( 1.26545D-11 ) BODY614_GM/PRIMARY = ( 6.32723D-12 ) BODY615_GM/PRIMARY = ( 1.89817D-11 ) BODY616_GM/PRIMARY = ( 5.79996D-10 ) BODY617_GM/PRIMARY = ( 3.42725D-10 ) BODY618_GM/PRIMARY = ( 4.74543D-12 ) \begintext -------- URLS AND CONTACTS Description of PCK format and contents can be found in NAIF's PCK "required reading" document, at: ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/C/ascii/individual_docs/pck.req NAIF tutorial on PCK formatting and use at: ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/Tutorials/office/individual_docs/16_pck.ppt ftp://naif.jpl.nasa.gov/pub/naif/toolkit_docs/Tutorials/office/packages/ SPICE_Tutorials_Office.zip The Cassini PCK & ephemeris files can be found on the DOM, and at: ftp://naif.jpl.nasa.gov/pub/naif/CASSINI/kernels/ Questions regarding this file can be directed to: Diane Conner (818)354-8586 Diane.Conner@jpl.nasa.gov Adrian Tinio (818)354-7511 Adrian.Tinio@jpl.nasa.gov David Seal (818)354-2707 David.Seal@jpl.nasa.gov -------- VERSION HISTORY 2005 Jul 11 ( published ) A. Tinio Applicable current Ephemeris = 050708R_SCPSE_05150_05169.XSP Restrictions/Limitations = Use for period of file. Reference/Source of new values = 050707_010Sa Parameter Superceded Value New Value BODY6_GM 37940571.43290575 37940584.32393724 BODY699_GM 37931193.7263 37931206.6260 BODY699_POLE_RA(1) 40.58051 40.582524 BODY699_POLE_DEC(1) 83.537912 83.537645 BODY699_JCOEF(2) 0.016290989185 0.016290795528 BODY699_JCOEF(4) -0.000931564786 -0.000932738706 BODY601_GM 2.538987472063466 2.530120927277264 BODY602_GM 7.209467692177664 7.210665451438561 BODY603_GM 41.20833951087783 41.20659404333172 BODY604_GM 73.11259945289306 73.11260446242133 BODY605_GM 154.0294413273712 154.0186476847478 BODY606_GM 8978.160024110673 8978.179855914042 BODY607_GM 0.379051300989386 0.378215663233720 BODY608_GM 120.5154106017876 120.5079215829297 BODY609_GM 0.5532537713007321 0.5532635543008535 2005 Jul 05 ( published ) A. Tinio Applicable current Ephemeris = 050623R_SCPSE_05132_05150 Restrictions/Limitations = Use for tour analysis for period of file. Reference/Source of new values = 050613_009Sa Parameter Superceded Value New Value BODY6_GM 37940570.36454137 37940571.43290575 BODY699_GM 37931192.6617 37931193.7263 BODY699_POLE_RA(1) 40.581077 40.580518 BODY699_POLE_DEC(1) 83.538043 83.537912 BODY699_JCOEF(2) 0.016290903873 0.016290989185 BODY699_JCOEF(4) -0.000933053169 -0.000931564786 BODY601_GM 2.539649757406880 2.538987472063466 BODY602_GM 7.207150581927309 7.209467692177664 BODY603_GM 41.20796800520257 41.20833951087783 BODY604_GM 73.11254942698964 73.11259945289306 BODY605_GM 154.0258089104270 154.0294413273712 BODY606_GM 8978.156565061139 8978.160024110673 BODY607_GM 0.379403816124753 0.379051300989386 BODY608_GM 120.5204864031117 120.5154106017876 BODY609_GM 0.5532476180130315 0.5532537713007321 2005 Jun 09 ( published ) D. Conner Applicable Ephemeris SPK File: 050606R_SCPSE_05114_05132 Restrictions/Limitations = Use for timespan of file. Reference/Source of new values = 050606_008Sa Parameter Superceded Value New Value BODY6_GM 37940560.63663255 37940570.36454137 BODY699_GM 37931182.9332 37931192.6617 BODY699_POLE_RA(1) 40.580644 40.581077 BODY699_POLE_DEC(1) 83.538056 83.538043 BODY699_JCOEF(2) 0.016291055854 0.016290903873 BODY699_JCOEF(4) -0.000931733527 -0.000933053169 BODY601_GM 2.540653252053214 2.539649757406880 BODY602_GM 7.205425461485284 7.207150581927309 BODY603_GM 41.20782889316963 41.20796800520257 BODY604_GM 73.11252681773537 73.11254942698964 BODY605_GM 154.0324679857708 154.0258089104270 BODY606_GM 8978.152308074805 8978.156565061139 BODY607_GM 0.379158979334525 0.379403816124753 BODY608_GM 120.5197925170135 120.5204864031117 BODY609_GM 0.5532510109715066 0.5532476180130315 2005 May 19 ( published ) A. Tinio Applicable Ephemeris SPK File: 050513R_SCPSE_05097_05114 Restrictions/Limitations = Use for timespan of file. Reference/Source of new values = 050513_007Sa Parameter Superceded Value New Value BODY6_GM 37940486.41643649 37940560.63663255 BODY699_GM 37931108.7402 37931182.9332 BODY699_POLE_RA(1) 40.578897 40.580644 BODY699_POLE_DEC(1) 83.537936 83.538056 BODY699_JCOEF(2) 0.016291230650 0.016291055854 BODY699_JCOEF(4) -0.000931186978 -0.000931733527 BODY699_JCOEF(6) 0.000091862764 0.000092477088 BODY601_GM 2.541872652365942 2.540653252053214 BODY602_GM 7.203042868002126 7.205425461485284 BODY603_GM 41.20826146236565 41.20782889316963 BODY604_GM 73.11229775557260 73.11252681773537 BODY605_GM 154.0200209194596 154.0324679857708 BODY606_GM 8978.142297854909 8978.152308074805 BODY607_GM 0.374580947348313 0.379158979334525 BODY608_GM 120.5206235708291 120.5197925170135 BODY609_GM 0.5532316617014716 0.5532510109715066 2005 May 05 ( published ) D. Conner Applicable Ephemeris SPK File: 050506R_SCPSE_05081_05097 Restrictions/Limitations = Use for period of this file. Reference/Source of new values = 050502_006T5 Parameter Superceded Value New Value BODY6_GM 37940491.60216828 37940486.41643649 BODY699_GM 37931113.8322 37931108.7402 BODY699_POLE_RA(1) 40.577216 40.578897 BODY699_POLE_DEC(1) 83.537833 83.537936 BODY699_JCOEF(2) 0.016291419485 0.016291230650 BODY699_JCOEF(4) -0.000930059692 -0.000931186978 BODY699_JCOEF(6) 0.000092794848 0.000091862764 BODY601_GM 2.541204859609778 2.541872652365942 BODY602_GM 7.208563270001138 7.203042868002126 BODY603_GM 41.20878136449268 41.20826146236565 BODY604_GM 73.11206772081295 73.11229775557260 BODY605_GM 154.1075398995426 154.0200209194596 BODY606_GM 8978.138361913190 8978.142297854909 BODY607_GM 0.372850585561523 0.374580947348313 BODY608_GM 120.5278582301508 120.5206235708291 BODY609_GM 0.5526937087918932 0.5532316617014716 2005 Apr 29 ( published ) D. Conner Applicable Ephemeris SPK File: 050426AP_SCPSE_05116_05216 Restrictions/Limitations = Use for period of this file. Reference/Source of new values = 050425_007Sa Parameter Superceded Value New Value BODY6_GM 37940502.18556380 37940491.60216828 BODY699_GM 37931124.7142 37931113.8322 BODY699_POLE_RA(1) 40.576012 40.577216 BODY699_POLE_DEC(1) 83.537850 83.537833 BODY699_JCOEF(2) 0.016291065583 0.016291419485 BODY699_JCOEF(4) -0.000932322006 -0.000930059692 BODY699_JCOEF(6) 0.000091137816 0.000092794848 BODY601_GM 2.540934363643657 2.541204859609778 BODY602_GM 7.205763658107196 7.208563270001138 BODY603_GM 41.20992788910005 41.20878136449268 BODY604_GM 73.11190061154372 73.11206772081295 BODY605_GM 153.8210020695582 154.1075398995426 BODY606_GM 8978.126641404288 8978.138361913190 BODY607_GM 0.379166152072442 0.372850585561523 BODY608_GM 120.5233558989635 120.5278582301508 BODY609_GM 0.5526908562645090 0.5526937087918932 2005 Apr 21 ( published ) D. Conner Applicable Ephemeris SPK File: 050414R_SCPSE_05034_05060 (s/c=-82, planets, satellites) Restrictions/Limitations = Use for tour analysis for period of this file. Reference/Source of new values = 050312_004E1 Parameter Superceded Value New Value BODY6_GM 37940496.33673127 37940502.18556380 BODY699_GM 37931118.8405 37931124.7142 BODY699_POLE_RA(1) 40.576463 40.576012 BODY699_POLE_DEC(1) 83.537851 83.537850 BODY699_JCOEF(2) 0.016290828142 0.016291065583 BODY699_JCOEF(4) -0.000933491306 -0.000932322006 BODY699_JCOEF(6) 0.000090898497 0.000091137816 BODY601_GM 2.541473321497260 2.540934363643657 BODY602_GM 7.209619039344632 7.205763658107196 BODY603_GM 41.21072942926893 41.20992788910005 BODY604_GM 73.11206095252155 73.11190061154372 BODY605_GM 153.8604802758120 153.8210020695582 BODY606_GM 8978.112734019802 8978.126641404288 BODY607_GM 0.379253012301593 0.379166152072442 BODY608_GM 120.5170740119231 120.5233558989635 BODY609_GM 0.5528058513249935 0.5526908562645090 2005 Apr 12 ( published ) D. Conner Applicable Ephemeris SPK File: 050411R_SCPSE_05015_05034 (s/c=-82, planets, satellites) Restrictions/Limitations = Use for Tour analysis for period of SPK file. Reference/Source of new values = 050218_003T3 5rameter Superceded Value New Value BODY6_GM 37940515.88181417 37940496.33673127 BODY699_GM 37931137.6508 37931118.8405 BODY699_POLE_RA(1) 40.575513 40.576463 BODY699_POLE_DEC(1) 83.537853 83.537851 BODY699_JCOEF(2) 0.016290958191 0.016290828142 BODY699_JCOEF(4) -0.000932286762 -0.000933491306 BODY601_GM 2.543473865943931 2.541473321497260 BODY602_GM 7.689375056656368 7.209619039344632 BODY603_GM 41.21109406519917 41.21072942926893 BODY604_GM 73.11102520071464 73.11206095252155 BODY605_GM 154.0395402008101 153.8604802758120 BODY606_GM 8978.169116863904 8978.112734019802 BODY607_GM 0.372672948245801 0.379253012301593 BODY608_GM 120.5420141732170 120.5170740119231 BODY609_GM 0.5526971060144958 0.5528058513249935 2005 Mar 01 ( published ) A. Tinio Applicable Ephemeris SPK File: 050214R_SCPSE_04336_05015 (s/c=-82, planets, satellites) Restrictions/Limitations = Use only for timespan of current Ephemeris Reference/Source of new values = 050214_00cTc Parameter Superceded Value New Value BODY6_GM 37940575.96714743 37940515.88181417 BODY699_GM 37931197.4166 37931137.6508 BODY699_POLE_RA(1) 40.584988 40.575513 BODY699_POLE_DEC(1) 83.537357 83.537853 BODY699_JCOEF(2) 0.016291386368 0.016290958191 BODY699_JCOEF(4) -0.000930863753 -0.000932286762 BODY699_JCOEF(6) 0.000089007261 0.000090898497 BODY601_GM 2.543221623761831 2.543473865943931 BODY602_GM 7.680749472948529 7.689375056656368 BODY603_GM 41.20953772443173 41.21109406519917 BODY604_GM 73.11013294006862 73.11102520071464 BODY605_GM 154.0976429614129 154.0395402008101 BODY606_GM 8978.252049389006 8978.169116863904 BODY607_GM 0.379196699024020 0.372672948245801 BODY608_GM 120.7250175986224 120.5420141732170 BODY609_GM 0.5529492368788559 0.5526971060144958 2005 Feb 28 ( published ) A. Tinio Applicable Ephemeris SPK File: 050105R_SCPSE_04247_04336 (s/c=-82, planets, satellites) Restrictions/Limitations = Use for Tour Analysis for period of SPK file. Reference/Source of new values = 050105_00bTb Parameter Superceded Value New Value BODY2_GM 324858.598826460 324858.598826460 BODY6_GM 37940594.58466490 37940575.96714743 BODY699_GM 37931216.9052 37931197.4166 BODY699_POLE_RA(1) 40.585770 40.584988 BODY699_POLE_DEC(1) 83.537290 83.537357 BODY699_JCOEF(2) 0.016290382080 0.016291386368 BODY699_JCOEF(4) -0.000934342762 -0.000930863753 BODY601_GM 2.543886999046834 2.543221623761831 BODY602_GM 7.896235619817622 7.680749472948529 BODY603_GM 41.21020363352076 41.20953772443173 BODY604_GM 73.10970856734933 73.11013294006862 BODY605_GM 153.4403813617471 154.0976429614129 BODY606_GM 8978.060680624023 8978.252049389006 BODY607_GM 0.521670363874684 0.379196699024020 BODY608_GM 120.3437832637150 120.7250175986224 BODY609_GM* 120.7250175986224 0.5529492368788559 *BODY609_GM value was inadvertently updated with the value for BODY608_GM in the "2005 Jan 10" pck file. This delivery corrects this error. The new value for BODY609_GM is the previous correct value which appears in the "2004 Dec 9" pck file. BODY608_GM is also correctly updated in this delivery. 2005 Jan 10 ( published ) D. Conner Applicable Ephemeris SPK File: 050105R_SCPSE_04247_04336 (s/c=-82, planets, satellites) Restrictions/Limitations = Use for Tour Analysis for period of SPK file. Reference/Source of new values = 050105_00bTb Parameter Superceded Value New Value BODY2_GM 324858.598826460 324858.598826460 BODY6_GM 37940594.58466490 37940575.96714743 BODY699_GM 37931216.9052 37931197.4166 BODY699_POLE_RA(1) 40.585770 40.584988 BODY699_POLE_DEC(1) 83.537290 83.537357 BODY699_JCOEF(2) 0.016290382080 0.016291386368 BODY699_JCOEF(4) -0.000934342762 -0.000930863753 BODY601_GM 2.543886999046834 2.543221623761831 BODY602_GM 7.896235619817622 7.680749472948529 BODY603_GM 41.21020363352076 41.20953772443173 BODY604_GM 73.10970856734933 73.11013294006862 BODY605_GM 153.4403813617471 154.0976429614129 BODY606_GM 8978.060680624023 8978.252049389006 BODY607_GM 0.521670363874684 0.379196699024020 BODY608_GM 120.3437832637150 120.7250175986224 2004 Dec 9 ( published ) D. Conner This file was created from cpck29Sep2004.tpc. Removed keywords controlled by PSG, including Jupiter satellites, to a separate file which is concatenated to this file. Only NAVT affected keywords appear above. Minor satellites and rocks keywords have been moved to the rocks PCK in a separate file cpck_rock.... BODY799_GM keyword removed. NAVT only provides a System GM. Applicable current Ephemeris = 041210AP_SCPSE_04329_08189 Restrictions/Limitations = None Reference/Source of new values = 041207_00cTc (OD Solution) Parameter Superceded Value New Value BODY10_GM 132712440035.0199 132712440017.9870 BODY2_GM 324858.592000000 324858.598826460 BODY3_GM 403503.241738000 403503.233479087 BODY399_GM 398600.4415000001 398600.4328969392 BODY5_GM 126712765.4543717 126712767.8577960 BODY599_GM 126686534.5576417 126686536.9610660 BODY6_GM 37940630.56986377 37940594.58466490 BODY699_GM 37931248.2650 37931216.9052 BODY699_POLE_RA(1) 40.578921 40.585770 BODY699_POLE_DEC(1) 83.537507 83.537290 BODY699_JCOEF(2) 0.016292234642 0.016290382080 BODY699_JCOEF(4) -0.000927651602 -0.000934342762 BODY699_JCOEF(6) 0.000096989418 0.000089007261 BODY7_GM 5794549.007815570 5794549.007071874 BODY301_GM 4902.800238000001 4902.800582147764 BODY601_GM 2.520135918453203 2.543886999046834 BODY602_GM 7.266915346837596 7.896235619817622 BODY603_GM 41.21004576075436 41.21020363352076 BODY604_GM 73.11466506841310 73.10970856734933 BODY605_GM 155.8320579960241 153.4403813617471 BODY606_GM 8977.930889955829 8978.060680624023 BODY607_GM 0.720000000000000 0.521670363874684 BODY608_GM 123.1583788283249 120.3437832637150 BODY609_GM 0.5517732425959611 0.5529492368788559 2004 Sep 29 (published) Applicable current Ephemeris: 041001AP_SCPSE_04275_08222.XSP (s/c=-82, planets, satellites) Restrictions/Limitations = None Reference/Source of new values = 040927_00aTa (OD solution) Parameter Superceded Value New Value BODY6_GM 37940690.7690100 37940630.56986377 BODY699_GM 37931300.4040 37931248.2650 BODY699_POLE_RA(1) 40.584666 40.578921 BODY699_POLE_DEC(1) 83.537319 83.537507 BODY699_JCOEF(2) 0.016293483929 0.016292234642 BODY699_JCOEF(4) -0.000921635401 -0.000927651602 BODY699_JCOEF(6) 0.000088726120 0.000096989418 BODY601_GM 2.521560245529253 2.520135918453203 BODY602_GM 7.127481554948487 7.266915346837596 BODY603_GM 41.20541310412448 41.21004576075436 BODY604_GM 73.11977199413563 73.11466506841310 BODY605_GM 154.4787324900041 155.8320579960241 BODY606_GM 8977.981454369899 8977.930889955829 BODY608_GM 132.6589941798197 123.1583788283249 BODY609_GM 0.5515856703994798 0.5517732425959611 2004 Jun 21 (published) Applicable current Ephemeris: 040622AP_SCPSE_04002_09011.BSP (s/c=-82, planets, satellites) 040622AP_SK_04122_08222.BSP (spacecraft ephemeris, scid=-82) 040622AP_PE_04002_09011.BSP (planetary ephemeris) 040622AP_SE_04002_09011.BSP (satellite ephemeris) Reference/Source of new values = 040615_00Sa (OD solution) Parameter Superceded Value New Value BODY6_GM 37940679.45741954 37940690.76901004 BODY699_GM 37931289.4836 37931300.4040 BODY699_POLE_RA(1) 40.586420 40.584666 BODY699_POLE_DEC(1) 83.537291 83.537319 BODY699_JCOEF(2) 0.016292243237 0.016293483929 BODY699_JCOEF(4) -0.000928716077 -0.000921635401 BODY699_JCOEF(6) 0.000088845313 0.000088726120 BODY601_GM 2.539908238874431 2.521560245529253 BODY602_GM 6.980134096218938 7.127481554948487 BODY603_GM 41.21066708236702 41.20541310412448 BODY604_GM 73.12382308588424 73.11977199413563 BODY605_GM 154.6927779454911 154.4787324900041 BODY606_GM 8978.009444641593 8977.981454369899 BODY608_GM 132.2117925658847 132.6589941798197 BODY609_GM 0.4852416379406062 0.5515856703994798 * * Reference for new Phoebe GM: IOM 312.0-024-04 "Navigation Results from the Phoebe flyby", J.B. Jones, 16 June 2004. 2004 May 05 (published) BODY299_GM was set equal to the BODY2_GM. BODY799_GM was calculated based on the new BODY7_GM. Applicable Ephemeris Files: 040506AP_SCPSE_04122_08222.XSP (s/c=-82, planets, satellites) 040506AP_SK_04122_08222.XSP (spacecraft ephemeris, scid=-82) 040506AP_OPK_04122_08222.XSP (s/c & probe, scids=-82,-150) 040506AP_PE_94328_16357.XSP (planetary ephemeris) 040506AP_SE_04002_09011.XSP (satellite ephemeris) Reference/Source of new values is NAV OD Solution: 040409_00Sa Parameter Superceded Value New Value BODY10_GM 132712440017.9870 132712440035.0199 BODY2_GM 324858.5988264598 324858.592000000 BODY3_GM 403503.2334790870 403503.241738000 BODY399_GM 398600.4328969392 398600.4415000001 BODY5_GM 126712767.8577960 126712765.4543717 BODY599_GM 126686536.9637693 126686534.5576417 BODY6_GM 37940629.764 37940679.45741954 BODY699_GM 37931267.73 37931289.4836 BODY699_POLE_RA(1) 40.589 40.586420 BODY699_POLE_RA(2) -0.036 -0.042290 BODY699_POLE_DEC(1) 83.537 83.537291 BODY699_POLE_DEC(2) -0.004 -0.004440 BODY699_JCOEF(2) 0.016298 0.016292243237 BODY699_JCOEF(4) -0.000915 -0.000928716077 BODY699_JCOEF(6) 0.000103 0.000088845313 BODY699_CCOEF(3) 0.00000070 0.0000000000000 BODY699_SCOEF(3) -0.00000020 0.00000000 BODY7_GM 5794549.007071874 5794549.007815570 BODY301_GM 4902.800582147764 4902.800238000001 BODY601_GM 2.5 2.539908238874431 BODY602_GM 4.9 6.980134096218938 BODY603_GM 41.808 41.21066708236702 BODY604_GM 73.156 73.12382308588424 BODY605_GM 154.000 154.6927779454911 BODY606_GM 8978.2 8978.009444641593 BODY607_GM 0.99 0.720000000000000 BODY608_GM 106.0 132.2117925658847 BODY609_GM 0.48 0.4852416379406062 -------- FORMATTING FOR SPECIAL PARAMETERS BODYNNN_GM GM in km^3/s^2 BODYNNN_*COEF Where * = J, C, or S. These coefficients are the normalized gravity field coefficients. J's are 1 to N, C's and S's have two indexes. Index 1 goes from 1 to N, and Index 2 goes from 1 to (Index 1). E.g. C11, C21, C22, C31, C32, C33, C41, etc. -------- REFERENCES 1. Cassini NAV OD solution 040615_00Sa. 2. Cassini NAV OD solution 040927_00aTa. 3. Cassini NAV OD solution 041207_00cTc. 4. Cassini NAV OD solution 050105_00bTb. 5. Cassini Nav OD solution 050214_00cTc. 6. Cassini Nav OD solution 050218_003T3. 7. Cassini Nav OD solution 050312_004E1. 8. Cassini Nav OD solution 050425_007Sa. 9. Cassini Nav OD solution 050502_006T5. 10. Cassini Nav OD solution 050513_007Sa. 11. Cassini Nav OD solution 050606_008Sa. 12. Cassini Nav OD solution 050613_009Sa. 13. Cassini Nav OD solution 050707_010Sa.