KPL/PCK \begintext P_constants (PcK) SPICE kernel file from the JUP365 Jupiter solution, contains GM values used in the satellite orbit integration, gravity field for Jupiter from Juno, satellite gravity fields, Jupiter and satellite orientation angles found as part of the solution. The Europa orientation has been extended to include Prime Meridian librations. BODYnnn_GM is the GM in km^3/s^2 BODYnnn_RADII are the triaxial radii in km, the largest is also the reference radius for the gravity field Gravity coefficients are un-normalized BODYnnn_JCOEF = J1, J2, J3, J4, etc BODYnnn_CCOEF = C11, C12, C22, C13, C23, C33, C14, C24, C34, C44, etc BODYnnn_SCOEF = S11, S12, S22, S13, S23, S33, S14, S24, S34, S44, etc BODY599_K2 is the k2 love number of Jupiter BODY599_MOI is the normalized axial moment of inertia of Jupiter =========================================================================== Saturn [3] \begindata BODY6_GM = ( 3.794058484180000E+07 ) \begintext Uranus [2] \begindata BODY7_GM = ( 5.794556465800000E+06 ) \begintext Neptune [1] \begindata BODY8_GM = ( 6.836527100600000E+06 ) \begintext Sun including the moon and inner planets [5] \begindata BODY10_GM = ( 1.327132332633514E+11 ) \begintext Jupiter [6,7,8] \begindata BODY5_CONSTANTS_JED_EPOCH = ( 2451545.0 ) BODY5_GM = ( 1.267127618414429E+08 ) BODY599_GM = ( 1.266865319003704E+08 ) BODY599_RADII = ( 71492.000, 71492.000, 66854.0 ) BODY599_JCOEF = ( 0.000000000000000E+00, 1.469650630000000E-02, -4.500000000000000E-08, -5.866085000000000E-04, -7.230000000000001E-08, 3.420070000000000E-05, 1.200000000000000E-07, -2.422000000000000E-06, -1.130000000000000E-07, 1.810000000000000E-07, 1.600000000000000E-08, 6.200000000000000E-08 ) BODY599_K2 = ( 5.897600000000000E-01 ) BODY599_MOI = ( 0.26708 ) BODY5_NUT_PREC_ANGLES = ( 99.3909037703700, 4850.57301032, 175.8927987627000, 1191.97138452, 300.1651705594000, 262.06085820, 50.1093240381100, 65.42434388, 244.7419890000000, 529.31728280, 108.3935660000000, 6076.59757260, 351.8043720000000, 2383.99260780, 216.9946890000000, 268.33760340, 200.0000000000000, 3034.73731920, 290.0000000000000, 3034.73731920, 313.2711570000000, 9109.85172630, 77.1462660000000, 91490.36580150, 154.2925320000000, 182980.73160300, 19.6057090000000, 45156.62937940, 39.2114180000000, 90313.25875880, 142.2243610000000, 415038.45222100, 350.1464370000000, 304950.80483400, 161.7871940000000, 313497.78806080, 266.6345470000000, 52830.42724960, 111.0225270000000, 1521.72145910, 248.3754170000000, 6393.69174410, 279.1075400000000, 28429.18670390, 205.1627760000000, 27277.12954930, 124.2953050000000, 27077.85793460 ) BODY599_POLE_RA = ( 268.0566974810512, -0.0064194664432, 0.0000000000000 ) BODY599_POLE_DEC = ( 64.4953388143978, 0.0024115863921, 0.0000000000000 ) BODY599_PM = ( 284.9505007299769, 870.5360000000001, 0.0000000000000 ) BODY599_NUT_PREC_RA = ( 0.0001158005, 0.0009311395, 0.0014259335, 0.0020940352, 0.0000000000, 0.0000000000 ) BODY599_NUT_PREC_DEC = ( 0.0000498082, 0.0004008882, 0.0006143954, 0.0009056974, 0.0000000000, 0.0000000000 ) BODY599_NUT_PREC_PM = ( -0.0001045158, -0.0008404002, -0.0012869767, -0.0018899720, 0.0000000000, 0.0000000000 ) \begintext Io [4,8] \begindata BODY501_GM = ( 5.959915466180539E+03 ) BODY501_RADII = ( 1829.400, 1819.400, 1815.700 ) BODY501_JCOEF = ( 0.000000000000000E+00, 1.823646136416393E-03, 0.000000000000000E+00 ) BODY501_CCOEF = ( 0.000000000000000E+00, 1.781457455378686E-06, 5.497270485195980E-04, 0.000000000000000E+00, 0.000000000000000E+00, 0.000000000000000E+00 ) BODY501_SCOEF = ( 0.000000000000000E+00, 3.996129695703687E-06, 1.283513055290983E-06, 0.000000000000000E+00, 0.000000000000000E+00, 0.000000000000000E+00 ) BODY501_POLE_RA = ( 268.0599860000000, -0.0060862679000, 0.0000000000000 ) BODY501_POLE_DEC = ( 64.4969780000000, 0.0022125612000, 0.0000000000000 ) BODY501_PM = ( 199.9439480000000, 203.4889584539000, 0.0000000000000 ) BODY501_NUT_PREC_RA = ( -0.08322700000, -0.02296900000, -0.00301200000, 0.00000000000, 0.00000000000, 0.00059300000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000 ) BODY501_NUT_PREC_DEC = ( -0.03583400000, -0.00988400000, -0.00125100000, 0.00000000000, 0.00000000000, -0.00029500000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000 ) BODY501_NUT_PREC_PM = ( 0.07494800000, 0.02080600000, 0.00211400000, 0.00000000000, 0.00000000000, 0.00011700000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000 ) \begintext Europa [4,8] \begindata BODY502_GM = ( 3.202712099607295E+03 ) BODY502_RADII = ( 1562.600, 1562.600, 1562.600 ) BODY502_JCOEF = ( 0.000000000000000E+00, 4.388708176988398E-04, 0.000000000000000E+00 ) BODY502_CCOEF = ( 0.000000000000000E+00, 1.120555546446984E-08, 1.323965822019810E-04, 0.000000000000000E+00, 0.000000000000000E+00, 0.000000000000000E+00 ) BODY502_SCOEF = ( 0.000000000000000E+00, 8.171607866380926E-07, -3.533408417230239E-06, 0.000000000000000E+00, 0.000000000000000E+00, 0.000000000000000E+00 ) BODY502_POLE_RA = ( 268.0530110000000, -0.0376557572000, 0.0000000000000 ) BODY502_POLE_DEC = ( 64.5142040000000, -0.0073180344000, 0.0000000000000 ) BODY502_PM = ( 34.3741010000000, 101.3747217722000, 0.0000000000000 ) BODY502_NUT_PREC_RA = ( 0.0027470000, -1.0805610000, -0.0561040000, 0.0325460000, 0.0000000000, 0.0019780000, 0.0091540000, 0.0018430000, 0.0006050000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, -0.0027870000, 0.0009200000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000 ) BODY502_NUT_PREC_DEC = ( 0.0011800000, -0.4651610000, -0.0246800000, -0.0169920000, 0.0000000000, -0.0008490000, 0.0019640000, -0.0004850000, 0.0000810000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, -0.0012000000, 0.0001750000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000 ) BODY502_NUT_PREC_PM = ( -0.0024660000, 0.9752040000, 0.0611580000, 0.1644270000, -0.0021770000, -0.0024600000, -0.0091790000, 0.0106660000, 0.0099910000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0000000000, 0.0025890000, -0.0014790000, -0.0083620000, 0.0155990000, 0.0485680000, -0.0259750000 ) \begintext Ganymede [4,8] \begindata BODY503_GM = ( 9.887832752719638E+03 ) BODY503_RADII = ( 2631.200, 2631.200, 2631.200 ) BODY503_JCOEF = ( 0.000000000000000E+00, 1.335434133821036E-04, -1.179470540188439E-05, 2.388685790723879E-05 ) BODY503_CCOEF = ( 0.000000000000000E+00, -7.010041812041256E-10, 4.005827956855108E-05, -3.677219166637273E-06, -2.296827018181999E-06, -1.674453595247786E-07, 1.027129517979281E-06, -1.576607674391440E-06, -2.188764830124715E-07, -5.727924115642320E-08 ) BODY503_SCOEF = ( 0.000000000000000E+00, -1.385547808427734E-07, -6.269370591849706E-07, 2.724699810044038E-06, 1.485991540186672E-06, -1.696195511310734E-07, 4.552812279631407E-07, -1.379268772864875E-06, 2.875422798309351E-07, 1.878523550529800E-08 ) BODY503_POLE_RA = ( 268.2027720000000, -0.0076801817000, 0.0000000000000 ) BODY503_POLE_DEC = ( 64.5671820000000, 0.0028243105000, 0.0000000000000 ) BODY503_PM = ( 41.6532810000000, 50.3176074735000, 0.0000000000000 ) BODY503_NUT_PREC_RA = ( 0.00000000000, 0.03841400000, -0.43294600000, -0.08667300000, 0.00140300000, 0.00422600000, 0.00000000000, 0.00083400000, 0.00100300000, 0.00024600000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000 ) BODY503_NUT_PREC_DEC = ( 0.00000000000, 0.01650600000, -0.18606700000, -0.03715300000, 0.00030600000, -0.00182500000, 0.00000000000, 0.00038200000, 0.00000300000, 0.00028700000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000 ) BODY503_NUT_PREC_PM = ( 0.00000000000, -0.03401000000, 0.39268300000, 0.07920300000, -0.00149300000, -0.00398300000, 0.00000000000, 0.00093100000, 0.01235400000, -0.00028700000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000 ) \begintext Callisto [4,8] \begindata BODY504_GM = ( 7.179283402579837E+03 ) BODY504_RADII = ( 2410.300, 2410.300, 2410.300 ) BODY504_JCOEF = ( 0.000000000000000E+00, 3.657037635982658E-05, 0.000000000000000E+00 ) BODY504_CCOEF = ( 0.000000000000000E+00, -7.383688948884316E-11, 1.002453170298303E-05, 0.000000000000000E+00, 0.000000000000000E+00, 0.000000000000000E+00 ) BODY504_SCOEF = ( 0.000000000000000E+00, 2.291937903493773E-08, -8.757010248194102E-07, 0.000000000000000E+00, 0.000000000000000E+00, 0.000000000000000E+00 ) BODY504_POLE_RA = ( 268.7106500000000, -0.0183058264000, 0.0000000000000 ) BODY504_POLE_DEC = ( 64.8174840000000, 0.0085641373000, 0.0000000000000 ) BODY504_PM = ( 260.3743280000000, 21.5710730689000, 0.0000000000000 ) BODY504_NUT_PREC_RA = ( 0.00000000000, 0.00135800000, 0.07051500000, -0.56007800000, 0.00000000000, 0.00949100000, 0.00000000000, 0.00000000000, 0.00226300000, 0.00044700000, -0.00108900000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000 ) BODY504_NUT_PREC_DEC = ( 0.00000000000, 0.00053200000, 0.02991200000, -0.23958700000, 0.00000000000, -0.00409700000, 0.00000000000, 0.00000000000, -0.00004100000, 0.00062400000, 0.00047000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000 ) BODY504_NUT_PREC_PM = ( 0.00000000000, -0.00183800000, -0.06392600000, 0.51205000000, 0.00000000000, -0.00931600000, 0.00000000000, 0.00000000000, 0.02999200000, -0.00061300000, 0.00100900000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000 ) \begintext Amalthea [4,8] \begindata BODY505_GM = ( 1.645634534798259E-01 ) BODY505_RADII = ( 138.000, 75.000, 64.000 ) BODY505_JCOEF = ( 0.000000000000000E+00, 6.900777672565674E-02, -1.795225686177211E-03, -1.471584466885456E-02 ) BODY505_CCOEF = ( 0.000000000000000E+00, 9.813893822384191E-04, 2.761142140044916E-02, -8.971365498427236E-04, -7.669341328578119E-05, 9.824080610742884E-05, -3.545183156668532E-04, -1.633988102810438E-03, 3.619591145527105E-05, 1.723038414990577E-04 ) BODY505_SCOEF = ( 0.000000000000000E+00, -3.684607143791918E-03, 2.864870091916350E-03, -1.266189958046020E-03, -5.352750110024392E-04, 2.101246514377142E-04, -1.576088151410741E-04, -6.762387574949739E-05, 3.149843954973100E-05, -4.838009999456752E-06 ) BODY505_POLE_RA = ( 268.0565310000000, -0.0066061122000, 0.0000000000000 ) BODY505_POLE_DEC = ( 64.4940730000000, 0.0024707399000, 0.0000000000000 ) BODY505_PM = ( 233.5727750000000, 722.6317219443000, 0.0000000000000 ) BODY505_NUT_PREC_RA = ( 0.00000000000, 0.00080400000, 0.00141600000, 0.00217500000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, -0.87574700000, 0.00604000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000 ) BODY505_NUT_PREC_DEC = ( 0.00000000000, 0.00034600000, 0.00060800000, 0.00091700000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, -0.37706200000, 0.00130000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000 ) BODY505_NUT_PREC_PM = ( 0.00000000000, -0.00072600000, -0.00126000000, -0.00041600000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.79041200000, -0.00607200000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000 ) \begintext Thebe [4,8] \begindata BODY514_GM = ( 0.030148) BODY514_RADII = ( 58.0, 49.0, 42.0 ) BODY514_POLE_RA = ( 268.05631100000, -0.00710230040, 0.0000000000000 ) BODY514_POLE_DEC = ( 64.48587500000, 0.00119807760, 0.0000000000000 ) BODY514_PM = ( 9.08295600000, 533.70027256860, 0.0000000000000 ) BODY514_NUT_PREC_RA = ( 0.00000000000, 0.00000000000, 0.00137200000, 0.00256700000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, -2.48017900000, 0.04845300000, -0.00286600000, 0.00000000000, 0.00000000000 ) BODY514_NUT_PREC_DEC = ( 0.00000000000, 0.00000000000, 0.00058400000, -0.00055200000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, -1.06764800000, 0.01042600000, -0.00123300000, 0.00000000000, 0.00000000000 ) BODY514_NUT_PREC_PM = ( 0.00000000000, 0.00000000000, -0.00118600000, 0.00002200000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 2.23850400000, -0.04871000000, 0.00258800000, 0.00000000000, 0.00000000000 ) \begintext Adrastea [4,8] \begindata BODY515_GM = ( 0.000139 ) BODY515_RADII = ( 10.0, 8.0, 7.0 ) BODY515_POLE_RA = ( 268.05653600000, -0.00656938840, 0.0000000000000 ) BODY515_POLE_DEC = ( 64.49535500000, 0.00246905120, 0.0000000000000 ) BODY515_PM = ( 34.44365600000,1206.99888267290, 0.0000000000000 ) BODY515_NUT_PREC_RA = ( 0.00000000000, 0.00093000000, 0.00145300000, 0.00213900000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.01604000000, 0.00000000000 ) BODY515_NUT_PREC_DEC = ( 0.00000000000, 0.00040000000, 0.00062600000, 0.00092600000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00690600000, 0.00000000000 ) BODY515_NUT_PREC_PM = ( 0.00000000000, -0.00106200000, -0.00002200000, 0.01534300000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, -0.01447500000, 0.00000000000 ) \begintext Metis [4,8] \begindata BODY516_GM = ( 0.002501 ) BODY516_RADII = ( 30.0, 20.0, 17.0 ) BODY516_POLE_RA = ( 268.05653900000, -0.00656615750, 0.0000000000000 ) BODY516_POLE_DEC = ( 64.49535600000, 0.00246773150, 0.0000000000000 ) BODY516_PM = ( 345.97243900000,1221.25468423971, 0.0000000000000 ) BODY516_NUT_PREC_RA = ( 0.00010600000, 0.00093100000, 0.00145300000, 0.00213500000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, -0.00542000000 ) BODY516_NUT_PREC_DEC = ( 0.00004600000, 0.00040100000, 0.00062600000, 0.00092500000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, -0.00233300000 ) BODY516_NUT_PREC_PM = ( -0.00009500000, -0.00082800000, -0.00136100000, 0.00175500000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00000000000, 0.00489200000 ) \begintext REFERENCES 1. Jacobson, R. A., 2009. "The orbits of the {Neptunian} satellites and the orientation of the pole of Neptune", AJ, 137, 4322--4329 2. Jacobson, R. A., 2014. "The Orbits of the Uranian Satellites and Rings, the Gravity Field of the Uranian System, and the Orientation of the Pole of Uranus", AJ, 148, 76--88 3. Jacobson, R. A., 2019. "Saturnian} Satellite Ephemeris -- SAT427", private communication 4. Archinal, B. A., Acton, C. H., A'Hearn, M. F., et al., 2018. "Report of the IAU Working Group on Cartographic Coordinates and Rotational Elements: 2015", Celest. Mech. 130, 22 5. Park, R. S., Folkner, W. M., Williams, J. G., Boggs, D.~H., 2021. "The JPL Planetary and Lunar Ephemerides DE440 and DE441", AJ, 161, 105-119 6. Durante, D., Parisi, M., Serra, D., Zannoni, M., Notaro, V., Racioppa, P., Buccino, D. R., Lari, G., Gomez Casajus, L., Iess, L., Folkner, W. M., Tommei, G., Tortora, P., Bolton, S. J., Feb. 2020. "Jupiter's Gravity Field Halfway Through the Juno Mission", Geophys. Res. Lett. 47 (4), e86572. 7. Wahl, S. M., Parisi, M., Folkner, W. M., Hubbard, W. B., Militzer, B., Mar. 2020. "Equilibrium Tidal Response of Jupiter: Detectability by the Juno Spacecraft", Astrophys J. 891 (1), 42. 8. Jacobson, R. A., 2021 "The Orbits of the Regular Jovian Satellites and the Orientation of the Pole of Jupiter", submitted to AJ =========================================================================== End of file pck_jup365.tpc ===========================================================================