****** Changes made to the mission will not be reflected ****** ****** in the data displayed until the mission is rerun ****** ====== Propagate Command: Wait for 1 hour (initial operations) Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 01 Jun 2022 12:59:28.000 29732.0412962963 TAI Epoch: 01 Jun 2022 13:00:05.000 29732.0417245370 TT Epoch: 01 Jun 2022 13:00:37.184 29732.0420970370 TDB Epoch: 01 Jun 2022 13:00:37.185 29732.0420970474 Cartesian State Keplerian State --------------------------- -------------------------------- X = -50079072.006907 km SMA = 254977944.75223 km Y = -143200663.71900 km ECC = 0.4290262806265 Z = 7142.2622528002 km INC = 0.0080865576945 deg VX = 30.904201180264 km/sec RAAN = 231.23862807353 deg VY = -16.554719044629 km/sec AOP = 349.44280049926 deg VZ = 0.0048639241085 km/sec TA = 30.043198040332 deg MA = 11.148445220792 deg EA = 19.254540186221 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 151704790.93834 km Mean Motion = 8.947503826e-08 deg/sec RA = -109.27537356634 deg Orbit Energy = -260.24297934269 km^2/s^2 DEC = 0.0026974855631 deg C3 = -520.48595868537 km^2/s^2 VMAG = 35.058927492075 km/s Semilatus Rectum = 2726471858.2790 km AZI = 89.992376615767 deg Angular Momentum = 5254547140.1437 km^2/s VFPA = 81.098372153627 deg Beta Angle = 0.0000000000000 deg RAV = -28.177001130217 deg Periapsis Altitude = 144889715.47340 km DECV = 0.0079489688966 deg VelPeriapsis = 36.092466104812 km/s VelApoapsis = 14.420903165051 km/s Orbit Period = 70222773.068406 s Planetodetic Properties --------------------------- LST = 236.09917868472 deg MHA = 292.37992135966 deg Latitude = -0.6328603283819 deg Longitude = -56.280742674943 deg Altitude = 151008800.93834 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 ====== Propagate Command: Free flight to next terminator Command summary is not supported for Propagate (in Single Step Mode) or when the command did not execute due to control logic statements. Please see the next valid command. ====== Maneuver Command: Apply ToDepartureOrbit Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 01 Jun 2022 12:59:28.000 29732.0412962963 TAI Epoch: 01 Jun 2022 13:00:05.000 29732.0417245370 TT Epoch: 01 Jun 2022 13:00:37.184 29732.0420970370 TDB Epoch: 01 Jun 2022 13:00:37.185 29732.0420970474 Cartesian State Keplerian State --------------------------- -------------------------------- X = -50079072.006907 km SMA = 412926912.56423 km Y = -143200663.71900 km ECC = 0.6521808071830 Z = 7142.2622528002 km INC = 0.0109998025187 deg VX = 32.363375090957 km/sec RAAN = 236.52917877295 deg VY = -19.514911025130 km/sec AOP = 344.08470306344 deg VZ = 0.0072491092917 km/sec TA = 30.110744848299 deg MA = 4.9862930637669 deg EA = 14.071438840275 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 151704790.93834 km Mean Motion = 4.341562262e-08 deg/sec RA = -109.27537356634 deg Orbit Energy = -160.69725171685 km^2/s^2 DEC = 0.0026974855631 deg C3 = -321.39450343369 km^2/s^2 VMAG = 37.791796095797 km/s Semilatus Rectum = 2931945337.7313 km AZI = 89.989336078220 deg Angular Momentum = 5611745531.0648 km^2/s VFPA = 78.185661308655 deg Beta Angle = 0.0000000000000 deg RAV = -31.089711962821 deg Periapsis Altitude = 142927915.42052 km DECV = 0.0109903051218 deg VelPeriapsis = 39.072503387469 km/s VelApoapsis = 8.2255928228231 km/s Orbit Period = 144721759.78589 s Planetodetic Properties --------------------------- LST = 236.09917868472 deg MHA = 292.37992135966 deg Latitude = -0.6328603283819 deg Longitude = -56.280742674943 deg Altitude = 151008800.93834 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 Maneuver Summary ----------------- Impulsive Burn: ToDepartureOrbit Spacecraft: Spacecraft Origin: Earth Axes: VNB Delta V Vector: Element 1: 3.3002925252433 km/s Element 2: 0.0000000000000 km/s Element 3: 0.0000000000000 km/s No mass depletion ====== Propagate Command: Free flight until leave Earth SOI Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 05 Jun 2022 08:17:32.967 29735.8455204490 TAI Epoch: 05 Jun 2022 08:18:09.967 29735.8459486897 TT Epoch: 05 Jun 2022 08:18:42.151 29735.8463211897 TDB Epoch: 05 Jun 2022 08:18:42.152 29735.8463211991 Cartesian State Keplerian State --------------------------- -------------------------------- X = -39959550.049394 km SMA = 178506727.53067 km Y = -146174905.23415 km ECC = 0.1514076982849 Z = 8758.7468891591 km INC = 0.0084046274861 deg VX = 30.709539400743 km/sec RAAN = 231.50554412225 deg VY = -8.0623367361461 km/sec AOP = 27.611760451997 deg VZ = 0.0042618411204 km/sec TA = 355.59340994642 deg MA = 356.78893342959 deg EA = 356.21649839506 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 151538340.48543 km Mean Motion = 1.527474379e-07 deg/sec RA = -105.28928570258 deg Orbit Energy = -371.72951925631 km^2/s^2 DEC = 0.0033116320876 deg C3 = -743.45903851262 km^2/s^2 VMAG = 31.750229952177 km/s Semilatus Rectum = 2481537218.5838 km AZI = 89.992275308660 deg Angular Momentum = 4811131411.7729 km^2/s VFPA = 90.579091658506 deg Beta Angle = 0.0000000000000 deg RAV = -14.710193593344 deg Periapsis Altitude = 150783444.78689 km DECV = 0.0076908264997 deg VelPeriapsis = 31.760954340379 km/s VelApoapsis = 23.407956528795 km/s Orbit Period = 41134472.642306 s Planetodetic Properties --------------------------- LST = 240.05350711374 deg MHA = 346.34055841637 deg Latitude = -0.1298921754190 deg Longitude = -106.28705130263 deg Altitude = 150842350.48543 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 ====== Maneuver Command: Apply ToJupiter1 Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 05 Jun 2022 08:17:32.967 29735.8455204490 TAI Epoch: 05 Jun 2022 08:18:09.967 29735.8459486897 TT Epoch: 05 Jun 2022 08:18:42.151 29735.8463211897 TDB Epoch: 05 Jun 2022 08:18:42.152 29735.8463211991 Cartesian State Keplerian State --------------------------- -------------------------------- X = -39959550.049394 km SMA = 452771700.94833 km Y = -146174905.23415 km ECC = 0.6653540473529 Z = 8758.7468891591 km INC = 0.0049243920236 deg VX = 36.939464034668 km/sec RAAN = 212.45074266226 deg VY = -9.6902511924725 km/sec AOP = 43.737258399030 deg VZ = 0.0024063328802 km/sec TA = 358.52271334146 deg MA = 359.77837012379 deg EA = 359.33774766072 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 151538340.48543 km Mean Motion = 3.781263171e-08 deg/sec RA = -105.28928570258 deg Orbit Energy = -146.55558169826 km^2/s^2 DEC = 0.0033116320876 deg C3 = -293.11116339653 km^2/s^2 VMAG = 38.189330671435 km/s Semilatus Rectum = 3032120156.9090 km AZI = 89.996355452053 deg Angular Momentum = 5786840753.5580 km^2/s VFPA = 90.590208140585 deg Beta Angle = 0.0000000000000 deg RAV = -14.699077351158 deg Periapsis Altitude = 150822227.19550 km DECV = 0.0036102418086 deg VelPeriapsis = 38.192376208408 km/s VelApoapsis = 7.6745987680127 km/s Orbit Period = 166166305.34510 s Planetodetic Properties --------------------------- LST = 240.05350711374 deg MHA = 346.34055841637 deg Latitude = -0.1298921754190 deg Longitude = -106.28705130263 deg Altitude = 150842350.48543 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 Maneuver Summary ----------------- Impulsive Burn: ToJupiter Spacecraft: Spacecraft Origin: Sun Axes: VNB Delta V Vector: Element 1: 6.4390999036473 km/s Element 2: -0.0027193918888 km/s Element 3: -0.0074094648333 km/s No mass depletion ====== Propagate Command: Free flight to MA=45 Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 28 Jan 2023 19:15:20.185 29973.3023169516 TAI Epoch: 28 Jan 2023 19:15:57.185 29973.3027451923 TT Epoch: 28 Jan 2023 19:16:29.369 29973.3031176923 TDB Epoch: 28 Jan 2023 19:16:29.369 29973.3031177004 Cartesian State Keplerian State --------------------------- -------------------------------- X = 380138219.18761 km SMA = 447539236.67783 km Y = 151802539.11246 km ECC = 0.6614970637897 Z = 4333.5960712060 km INC = 0.0059626749535 deg VX = 6.2331839072282 km/sec RAAN = 207.60749459336 deg VY = 17.693233722218 km/sec AOP = 48.560809669205 deg VZ = -0.0013310548009 km/sec TA = 125.60025701051 deg MA = 45.000000000001 deg EA = 82.583949807388 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 409327590.79605 km Mean Motion = 3.847770333e-08 deg/sec RA = 21.768561304476 deg Orbit Energy = -148.26905569570 km^2/s^2 DEC = 0.0006065966981 deg C3 = -296.53811139140 km^2/s^2 VMAG = 18.759080546287 km/s Semilatus Rectum = 210315819.22397 km AZI = 90.005931739497 deg Angular Momentum = 5779661246.2594 km^2/s VFPA = 48.824488060210 deg Beta Angle = 0.0000000000000 deg RAV = 70.593049178537 deg Periapsis Altitude = 150797355.68478 km DECV = -0.0040654349911 deg VelPeriapsis = 38.151254895944 km/s VelApoapsis = 7.7726961328060 km/s Orbit Period = 163294187.62843 s Planetodetic Properties --------------------------- LST = 7.3224673189729 deg MHA = 114.52274270938 deg Latitude = 5.8617378010478 deg Longitude = -107.20027539040 deg Altitude = 408631600.79605 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 ====== Maneuver Command: Apply ToJupiter_Correction1 Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 28 Jan 2023 19:15:20.185 29973.3023169516 TAI Epoch: 28 Jan 2023 19:15:57.185 29973.3027451923 TT Epoch: 28 Jan 2023 19:16:29.369 29973.3031176923 TDB Epoch: 28 Jan 2023 19:16:29.369 29973.3031177004 Cartesian State Keplerian State --------------------------- -------------------------------- X = 380138219.18761 km SMA = 457672420.10803 km Y = 151802539.11246 km ECC = 0.6648994055515 Z = 4333.5960712060 km INC = 0.4647922837710 deg VX = 6.3335043722203 km/sec RAAN = 201.84333594975 deg VY = 17.842144076630 km/sec AOP = 55.467600943162 deg VZ = -0.1152328974901 km/sec TA = 124.45762195115 deg MA = 43.246642584425 deg EA = 80.858741081943 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 409327590.79605 km Mean Motion = 3.720691858e-08 deg/sec RA = 21.768561304476 deg Orbit Energy = -144.98627641432 km^2/s^2 DEC = 0.0006065966981 deg C3 = -289.97255282864 km^2/s^2 VMAG = 18.933268642916 km/s Semilatus Rectum = 213366952.46444 km AZI = 90.464791887947 deg Angular Momentum = 5821230368.6026 km^2/s VFPA = 48.688816634405 deg Beta Angle = 0.0000000000000 deg RAV = 70.456440340256 deg Periapsis Altitude = 152670310.04090 km DECV = -0.3487194722632 deg VelPeriapsis = 37.956385249237 km/s VelApoapsis = 7.6396250834891 km/s Orbit Period = 168871423.57894 s Planetodetic Properties --------------------------- LST = 7.3224673189729 deg MHA = 114.52274270938 deg Latitude = 5.8617378010478 deg Longitude = -107.20027539040 deg Altitude = 408631600.79605 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 Maneuver Summary ----------------- Impulsive Burn: ToJupiter_Correction1 Spacecraft: Spacecraft Origin: Sun Axes: VNB Delta V Vector: Element 1: 0.1737917385543 km/s Element 2: -0.1138929477534 km/s Element 3: 0.0451325511983 km/s No mass depletion ====== Propagate Command: Free flight to MA=90 Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 10 Oct 2023 12:36:23.683 30228.0252741129 TAI Epoch: 10 Oct 2023 12:37:00.683 30228.0257023536 TT Epoch: 10 Oct 2023 12:37:32.867 30228.0260748536 TDB Epoch: 10 Oct 2023 12:37:32.866 30228.0260748345 Cartesian State Keplerian State --------------------------- -------------------------------- X = 402762705.56308 km SMA = 457571732.09304 km Y = 472325118.61156 km ECC = 0.6671765357222 Z = -2364726.1414787 km INC = 0.4798782853451 deg VX = -2.5224254510658 km/sec RAAN = 202.49041456131 deg VY = 11.453733937223 km/sec AOP = 54.706627272535 deg VZ = -0.0967178745636 km/sec TA = 152.34876669991 deg MA = 90.000000000003 deg EA = 122.30834225813 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 620736986.64865 km Mean Motion = 3.721920025e-08 deg/sec RA = 49.544994491947 deg Orbit Energy = -145.01818044018 km^2/s^2 DEC = -0.2182714390219 deg C3 = -290.03636088037 km^2/s^2 VMAG = 11.728597768196 km/s Semilatus Rectum = 5750400950.3801 km AZI = 90.427365921897 deg Angular Momentum = 5804745364.9360 km^2/s VFPA = 52.874380116580 deg Beta Angle = 0.0000000000000 deg RAV = 102.41984266526 deg Periapsis Altitude = 151594619.03079 km DECV = -0.4724851967108 deg VelPeriapsis = 38.116239746354 km/s VelApoapsis = 7.6092595389898 km/s Orbit Period = 168815699.02859 s Planetodetic Properties --------------------------- LST = 35.036917014415 deg MHA = 127.61505588438 deg Latitude = 2.9802926826665 deg Longitude = -92.578138869965 deg Altitude = 620040996.64865 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 ====== Maneuver Command: Apply ToJupiter_Correction2 Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 10 Oct 2023 12:36:23.683 30228.0252741129 TAI Epoch: 10 Oct 2023 12:37:00.683 30228.0257023536 TT Epoch: 10 Oct 2023 12:37:32.867 30228.0260748536 TDB Epoch: 10 Oct 2023 12:37:32.866 30228.0260748345 Cartesian State Keplerian State --------------------------- -------------------------------- X = 402762705.56308 km SMA = 458053777.12568 km Y = 472325118.61156 km ECC = 0.6693979949546 Z = -2364726.1414787 km INC = 0.9784436959512 deg VX = -2.4753962858744 km/sec RAAN = 216.65619161225 deg VY = 11.476251497896 km/sec AOP = 40.580126593766 deg VZ = -0.1824769699660 km/sec TA = 152.31049308663 deg MA = 89.533725825383 deg EA = 122.04390664890 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 620736986.64865 km Mean Motion = 3.716046279e-08 deg/sec RA = 49.544994491947 deg Orbit Energy = -144.86556671443 km^2/s^2 DEC = -0.2182714390219 deg C3 = -289.73113342885 km^2/s^2 VMAG = 11.741602661462 km/s Semilatus Rectum = 5737794256.8578 km AZI = 90.953789308991 deg Angular Momentum = 5792242511.4200 km^2/s VFPA = 52.628400790124 deg Beta Angle = 0.0000000000000 deg RAV = 102.17206099867 deg Periapsis Altitude = 150737507.13637 km DECV = -0.8904730851191 deg VelPeriapsis = 38.249413907439 km/s VelApoapsis = 7.5747862210382 km/s Orbit Period = 169082536.52745 s Planetodetic Properties --------------------------- LST = 35.036917014415 deg MHA = 127.61505588438 deg Latitude = 2.9802926826665 deg Longitude = -92.578138869965 deg Altitude = 620040996.64865 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 Maneuver Summary ----------------- Impulsive Burn: ToJupiter_Correction2 Spacecraft: Spacecraft Origin: Sun Axes: VNB Delta V Vector: Element 1: 0.0125826655490 km/s Element 2: -0.0857325113499 km/s Element 3: 0.0506460105716 km/s No mass depletion ====== Propagate Command: Free flight to Jupiter periapsis Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 26 Sep 2024 08:40:23.959 30579.8613884136 TAI Epoch: 26 Sep 2024 08:41:00.959 30579.8618166543 TT Epoch: 26 Sep 2024 08:41:33.143 30579.8621891543 TDB Epoch: 26 Sep 2024 08:41:33.141 30579.8621891354 Cartesian State Keplerian State --------------------------- -------------------------------- X = 264148250.21065 km SMA = -99495521.819394 km Y = 708099533.66565 km ECC = 8.4754534690441 Z = -8817077.6958602 km INC = 81.686796127858 deg VX = -3.2298124379844 km/sec RAAN = 249.44488602459 deg VY = 8.0816473483235 km/sec AOP = 169.84542405608 deg VZ = -40.115901178636 km/sec TA = 10.830081761239 deg MA = 72.685599781379 deg HA = 9.6710957722565 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 755815446.07526 km Mean Motion = 3.670713727e-07 deg/sec RA = 69.542557946915 deg Orbit Energy = 666.92669977093 km^2/s^2 DEC = -0.6684076133530 deg C3 = 1333.8533995419 km^2/s^2 VMAG = 41.049119839789 km/s Semilatus Rectum = 6671806971.8962 km AZI = 171.68622640515 deg Angular Momentum = 30582737494.926 km^2/s VFPA = 80.308076101696 deg Beta Angle = 0.0000000000000 deg RAV = 111.78401030248 deg Periapsis Altitude = 743078153.73914 km DECV = -77.759373636291 deg VelPeriapsis = 41.118312262347 km/s Planetodetic Properties Hyperbolic Parameters --------------------------- -------------------------------- LST = 54.842842673468 deg BdotT = 375542544.97770 km MHA = 78.199235573789 deg BdotR = -748446502.36390 km Latitude = 0.1209122249466 deg B Vector Angle = -63.354209150561 deg Longitude = -23.356392900321 deg B Vector Mag = 837379465.94664 km Altitude = 755119456.07526 km DLA = -81.030942401730 deg RLA = 137.23394055743 deg Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 ====== Maneuver Command: Apply ToJupiterOrbit Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 26 Sep 2024 08:40:23.959 30579.8613884136 TAI Epoch: 26 Sep 2024 08:41:00.959 30579.8618166543 TT Epoch: 26 Sep 2024 08:41:33.143 30579.8621891543 TDB Epoch: 26 Sep 2024 08:41:33.141 30579.8621891354 Cartesian State Keplerian State --------------------------- -------------------------------- X = 264148250.21065 km SMA = -108429382.98256 km Y = 708099533.66565 km ECC = 7.8583711926452 Z = -8817077.6958602 km INC = 81.009214394999 deg VX = -3.5482415476977 km/sec RAAN = 249.43679791141 deg VY = 7.9811014070940 km/sec AOP = 169.74516706806 deg VZ = -38.714875420484 km/sec TA = 10.931555486077 deg MA = 66.687715780459 deg HA = 9.6708599924785 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 755815446.07526 km Mean Motion = 3.226527250e-07 deg/sec RA = 69.542557946915 deg Orbit Energy = 611.97636824762 km^2/s^2 DEC = -0.6684076133530 deg C3 = 1223.9527364952 km^2/s^2 VMAG = 39.687902143786 km/s Semilatus Rectum = 6327846956.6759 km AZI = 171.00859749411 deg Angular Momentum = 29567645377.655 km^2/s VFPA = 80.297337265827 deg Beta Angle = 0.0000000000000 deg RAV = 113.96899517874 deg Periapsis Altitude = 742952966.68385 km DECV = -77.286584045648 deg VelPeriapsis = 39.760219001053 km/s Planetodetic Properties Hyperbolic Parameters --------------------------- -------------------------------- LST = 54.842842673468 deg BdotT = 392417304.60397 km MHA = 78.199235573789 deg BdotR = -748524698.91250 km Latitude = 0.1209122249466 deg B Vector Angle = -62.334030465873 deg Longitude = -23.356392900321 deg B Vector Mag = 845151208.85833 km Altitude = 755119456.07526 km DLA = -80.543263705995 deg RLA = 141.22149548291 deg Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 Maneuver Summary ----------------- Impulsive Burn: ToJupiterOrbit Spacecraft: Spacecraft Origin: Jupiter Axes: VNB Delta V Vector: Element 1: -1.4402707242797 km/s Element 2: 0.0000000000000 km/s Element 3: 0.0000000000000 km/s No mass depletion ====== Propagate Command: Free flight to Jupiter apoapsis Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 02 Oct 2024 06:58:42.029 30585.7907642222 TAI Epoch: 02 Oct 2024 06:59:19.029 30585.7911924629 TT Epoch: 02 Oct 2024 06:59:51.213 30585.7915649629 TDB Epoch: 02 Oct 2024 06:59:51.211 30585.7915649437 Cartesian State Keplerian State --------------------------- -------------------------------- X = 254893131.46700 km SMA = 856321189.67212 km Y = 711233649.13424 km ECC = 0.1189785079456 Z = -9305874.2339819 km INC = 9.5330867124298 deg VX = -12.911750099002 km/sec RAAN = 74.489297864127 deg VY = 4.9246092724208 km/sec AOP = 346.03448568468 deg VZ = 2.3105419506672 km/sec TA = 9.7007830280450 deg MA = 7.5913089081148 deg EA = 8.6121110432442 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 755586137.66077 km Mean Motion = 1.453787000e-08 deg/sec RA = 70.283249143045 deg Orbit Energy = -77.489872736189 km^2/s^2 DEC = -0.7056783762524 deg C3 = -154.97974547238 km^2/s^2 VMAG = 14.010841202829 km/s Semilatus Rectum = 6176309215.4776 km AZI = 80.492826965510 deg Angular Momentum = 10584693494.296 km^2/s VFPA = 88.972005382462 deg Beta Angle = 0.0000000000000 deg RAV = 159.12288629175 deg Periapsis Altitude = 753741382.20277 km DECV = 9.4920648036846 deg VelPeriapsis = 14.029916709178 km/s VelApoapsis = 11.046376730875 km/s Orbit Period = 432194352.33923 s Planetodetic Properties --------------------------- LST = 55.572938688849 deg MHA = 162.30387378791 deg Latitude = -0.0090654669032 deg Longitude = -106.73093509906 deg Altitude = 754890147.66077 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 ====== Propagate Command: Free flight to periapsis Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 08 Oct 2024 05:13:27.215 30591.7176761009 TAI Epoch: 08 Oct 2024 05:14:04.215 30591.7181043416 TT Epoch: 08 Oct 2024 05:14:36.399 30591.7184768416 TDB Epoch: 08 Oct 2024 05:14:36.397 30591.7184768224 Cartesian State Keplerian State --------------------------- -------------------------------- X = 251398319.84393 km SMA = -108733954.45385 km Y = 713295271.51528 km ECC = 7.8485714449290 Z = -8553395.0079997 km INC = 81.179009807845 deg VX = -3.6253686765770 km/sec RAAN = 250.48462286144 deg VY = 7.7517820104255 km/sec AOP = 169.94994283865 deg VZ = -38.706845094713 km/sec TA = 10.705772753205 deg MA = 65.177279141039 deg HA = 9.4674747460139 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 756349403.48530 km Mean Motion = 3.212980153e-07 deg/sec RA = 70.585179732100 deg Orbit Energy = 610.26217930075 km^2/s^2 DEC = -0.6479596316429 deg C3 = 1220.5243586015 km^2/s^2 VMAG = 39.641560004172 km/s Semilatus Rectum = 7860572217.5530 km AZI = 171.17844120136 deg Angular Momentum = 29571611005.179 km^2/s VFPA = 80.499279547580 deg Beta Angle = 0.0000000000000 deg RAV = 115.06464432503 deg Periapsis Altitude = 743976265.56685 km DECV = -77.533087296962 deg VelPeriapsis = 39.710907428221 km/s Planetodetic Properties Hyperbolic Parameters --------------------------- -------------------------------- LST = 55.879708452643 deg BdotT = 390395613.14459 km MHA = 246.37356264249 deg BdotR = -751046171.47561 km Latitude = 0.0102508234543 deg B Vector Angle = -62.534480326853 deg Longitude = 169.50614581015 deg B Vector Mag = 846450876.57271 km Altitude = 755653413.48530 km DLA = -80.769408724566 deg RLA = 143.21148402362 deg Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 ====== Maneuver Command: Apply ToIntersectingOrbit Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 08 Oct 2024 05:13:27.215 30591.7176761009 TAI Epoch: 08 Oct 2024 05:14:04.215 30591.7181043416 TT Epoch: 08 Oct 2024 05:14:36.399 30591.7184768416 TDB Epoch: 08 Oct 2024 05:14:36.397 30591.7184768224 Cartesian State Keplerian State --------------------------- -------------------------------- X = 251398319.84393 km SMA = -108864622.23389 km Y = 713295271.51528 km ECC = 7.8384015989329 Z = -8553395.0079997 km INC = 81.591493452410 deg VX = -3.3406758884344 km/sec RAAN = 250.48939494954 deg VY = 7.7099314494041 km/sec AOP = 169.85128884681 deg VZ = -38.721895008248 km/sec TA = 10.803711930035 deg MA = 65.677367458215 deg HA = 9.5533882868536 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 756349403.48530 km Mean Motion = 3.207197186e-07 deg/sec RA = 70.585179732100 deg Orbit Energy = 609.52969520651 km^2/s^2 DEC = -0.6479596316429 deg C3 = 1219.0593904130 km^2/s^2 VMAG = 39.623078014913 km/s Semilatus Rectum = 7788235776.8418 km AZI = 171.59095183007 deg Angular Momentum = 29550400313.604 km^2/s VFPA = 80.413676347223 deg Beta Angle = 0.0000000000000 deg RAV = 113.42685080682 deg Periapsis Altitude = 743764016.75146 km DECV = -77.756753170950 deg VelPeriapsis = 39.693737804063 km/s Planetodetic Properties Hyperbolic Parameters --------------------------- -------------------------------- LST = 55.879708452643 deg BdotT = 373732210.05526 km MHA = 246.37356264249 deg BdotR = -759365295.24734 km Latitude = 0.0102508234543 deg B Vector Angle = -63.795252301250 deg Longitude = 169.50614581015 deg B Vector Mag = 846351827.82272 km Altitude = 755653413.48530 km DLA = -81.134718241281 deg RLA = 141.87858791755 deg Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 Maneuver Summary ----------------- Impulsive Burn: ToIntersectingOrbit Spacecraft: Spacecraft Origin: Jupiter Axes: VNB Delta V Vector: Element 1: 0.0746966736063 km/s Element 2: 0.0000000000000 km/s Element 3: 0.2782954543786 km/s No mass depletion ====== Propagate Command: Free flight to apoapsis Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 14 Oct 2024 20:16:26.166 30598.3447472937 TAI Epoch: 14 Oct 2024 20:17:03.166 30598.3451755345 TT Epoch: 14 Oct 2024 20:17:35.350 30598.3455480345 TDB Epoch: 14 Oct 2024 20:17:35.349 30598.3455480155 Cartesian State Keplerian State --------------------------- -------------------------------- X = 241134530.11415 km SMA = 853545441.69593 km Y = 716648834.03248 km ECC = 0.1159047082154 Z = -9117352.2069858 km INC = 8.9153615219303 deg VX = -12.990266552679 km/sec RAAN = 75.811608455765 deg VY = 4.7036571273274 km/sec AOP = 344.06742527417 deg VZ = 2.1564859378749 km/sec TA = 11.470462570475 deg MA = 9.0389530248331 deg EA = 10.216870777571 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 756184196.50555 km Mean Motion = 1.460884381e-08 deg/sec RA = 71.403192171275 deg Orbit Energy = -77.741871454612 km^2/s^2 DEC = -0.6908349338588 deg C3 = -155.48374290922 km^2/s^2 VMAG = 13.982912682319 km/s Semilatus Rectum = 7770022933.8963 km AZI = 81.111228814939 deg Angular Momentum = 10571393394.467 km^2/s VFPA = 88.814258919830 deg Beta Angle = 0.0000000000000 deg RAV = 160.09514007686 deg Periapsis Altitude = 753919516.32758 km DECV = 8.8717322548611 deg VelPeriapsis = 14.008979812665 km/s VelApoapsis = 11.098862657269 km/s Orbit Period = 430094632.19298 s Planetodetic Properties --------------------------- LST = 56.685775276170 deg MHA = 340.37459127183 deg Latitude = -0.1351750151386 deg Longitude = 76.311184004340 deg Altitude = 755488206.50555 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 ====== Maneuver Command: Apply ToIntersectingOrbit_Correction Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 14 Oct 2024 20:16:26.166 30598.3447472937 TAI Epoch: 14 Oct 2024 20:17:03.166 30598.3451755345 TT Epoch: 14 Oct 2024 20:17:35.350 30598.3455480345 TDB Epoch: 14 Oct 2024 20:17:35.349 30598.3455480155 Cartesian State Keplerian State --------------------------- -------------------------------- X = 241134530.11415 km SMA = 897429850.22546 km Y = 716648834.03248 km ECC = 0.1575103047656 Z = -9117352.2069858 km INC = 16.645247384918 deg VX = -12.898568621560 km/sec RAAN = 73.714624079049 deg VY = 4.4860146379599 km/sec AOP = 354.95262320915 deg VZ = 4.0776975962911 km/sec TA = 2.6349689828240 deg MA = 1.8940944560570 deg EA = 2.2481029930746 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 756184196.50555 km Mean Motion = 1.355049158e-08 deg/sec RA = 71.403192171275 deg Orbit Energy = -73.940286243347 km^2/s^2 DEC = -0.6908349338588 deg C3 = -147.88057248669 km^2/s^2 VMAG = 14.252193427816 km/s Semilatus Rectum = 7994644716.6025 km AZI = 73.368689539100 deg Angular Momentum = 10777072495.480 km^2/s VFPA = 89.641521316028 deg Beta Angle = 0.0000000000000 deg RAV = 160.82275144649 deg Periapsis Altitude = 755379411.01071 km DECV = 16.625220677379 deg VelPeriapsis = 14.253965254092 km/s VelApoapsis = 10.374697135188 km/s Orbit Period = 463686890.61395 s Planetodetic Properties --------------------------- LST = 56.685775276170 deg MHA = 340.37459127183 deg Latitude = -0.1351750151386 deg Longitude = 76.311184004340 deg Altitude = 755488206.50555 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 Maneuver Summary ----------------- Impulsive Burn: ToIntersectingOrbit_Correction Spacecraft: Spacecraft Origin: Jupiter Axes: VNB Delta V Vector: Element 1: 1.8558239861743 km/s Element 2: 0.0000000000000 km/s Element 3: -0.5502257105260 km/s No mass depletion ====== Propagate Command: Free flight to periapsis Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 22 Oct 2024 10:01:14.692 30605.9175311561 TAI Epoch: 22 Oct 2024 10:01:51.692 30605.9179593968 TT Epoch: 22 Oct 2024 10:02:23.876 30605.9183318968 TDB Epoch: 22 Oct 2024 10:02:23.874 30605.9183318785 Cartesian State Keplerian State --------------------------- -------------------------------- X = 236496398.36613 km SMA = -17023301370.217 km Y = 719125906.15238 km ECC = 1.0431244106212 Z = -8069276.4695938 km INC = 62.988735415487 deg VX = -7.0557999803078 km/sec RAAN = 251.48436065435 deg VY = 5.6393003650340 km/sec AOP = 160.84698867946 deg VZ = -16.637610502262 km/sec TA = 19.838500685736 deg MA = 0.1268845546262 deg HA = 2.9119636890704 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 757058603.12288 km Mean Motion = 1.640174802e-10 deg/sec RA = 71.795698179523 deg Orbit Energy = 3.8979642412421 km^2/s^2 DEC = -0.6107112952239 deg C3 = 7.7959284824842 km^2/s^2 VMAG = 18.931352439648 km/s Semilatus Rectum = 6208523476.7436 km AZI = 152.98707613436 deg Angular Momentum = 14108690402.835 km^2/s VFPA = 79.869267028922 deg Beta Angle = 0.0000000000000 deg RAV = 141.36664037291 deg Periapsis Altitude = 733423848.41759 km DECV = -61.502626091402 deg VelPeriapsis = 19.218511289991 km/s Planetodetic Properties Hyperbolic Parameters --------------------------- -------------------------------- LST = 57.085221248106 deg BdotT = 2296823732.0497 km MHA = 87.789986693999 deg BdotR = -4500868714.3181 km Latitude = -0.1051003526138 deg B Vector Angle = -62.964471986208 deg Longitude = -30.704765445893 deg B Vector Mag = 5053040514.3472 km Altitude = 756362613.12288 km DLA = -31.312405607134 deg RLA = -126.58078271534 deg Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 ====== Propagate Command: Free flight to Europa orbit plane Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 22 Oct 2024 12:59:52.270 30606.0415772032 TAI Epoch: 22 Oct 2024 13:00:29.270 30606.0420054440 TT Epoch: 22 Oct 2024 13:01:01.454 30606.0423779440 TDB Epoch: 22 Oct 2024 13:01:01.453 30606.0423779256 Cartesian State Keplerian State --------------------------- -------------------------------- X = 236404753.64594 km SMA = -1626447397.0349 km Y = 719189139.92648 km ECC = 1.4579242247449 Z = -8250995.5526961 km INC = 56.138911614506 deg VX = -10.055219720000 km/sec RAAN = 251.38477251835 deg VY = 6.1465214450855 km/sec AOP = 167.30978362715 deg VZ = -17.125830027727 km/sec TA = 13.442203183480 deg MA = 2.6861725691682 deg HA = 5.8338661964690 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 757092005.94261 km Mean Motion = 5.553870951e-09 deg/sec RA = 71.803782088902 deg Orbit Energy = 40.798257681107 km^2/s^2 DEC = -0.6244374223441 deg C3 = 81.596515362214 km^2/s^2 VMAG = 20.788968796719 km/s Semilatus Rectum = 7388023489.9319 km AZI = 146.13662829613 deg Angular Momentum = 15586797109.294 km^2/s VFPA = 82.021148527086 deg Beta Angle = 0.0000000000000 deg RAV = 148.56352745376 deg Periapsis Altitude = 744093673.37555 km DECV = -55.466422242798 deg VelPeriapsis = 20.927783877466 km/s Planetodetic Properties Hyperbolic Parameters --------------------------- -------------------------------- LST = 57.091511864634 deg BdotT = 1085582908.1536 km MHA = 89.549505446150 deg BdotR = -1341247110.2922 km Latitude = -0.1197351351783 deg B Vector Angle = -51.013872424559 deg Longitude = -32.457993581516 deg B Vector Mag = 1725524285.9324 km Altitude = 756396015.94261 km DLA = -45.612786151619 deg RLA = -151.88978201226 deg Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 ====== Maneuver Command: Apply ToInterceptEuropa Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 22 Oct 2024 12:59:52.270 30606.0415772032 TAI Epoch: 22 Oct 2024 13:00:29.270 30606.0420054440 TT Epoch: 22 Oct 2024 13:01:01.454 30606.0423779440 TDB Epoch: 22 Oct 2024 13:01:01.453 30606.0423779256 Cartesian State Keplerian State --------------------------- -------------------------------- X = 236404753.64594 km SMA = -1990021911.0067 km Y = 719189139.92648 km ECC = 1.3734339665099 Z = -8250995.5526961 km INC = 57.499026649334 deg VX = -9.4425932832664 km/sec RAAN = 251.40593771522 deg VY = 6.0475970351068 km/sec AOP = 166.24274408793 deg VZ = -17.074473477241 km/sec TA = 14.497658487257 deg MA = 2.1743672641319 deg HA = 5.7864332552309 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 757092005.94261 km Mean Motion = 4.103637877e-09 deg/sec RA = 71.803782088902 deg Orbit Energy = 33.344467034249 km^2/s^2 DEC = -0.6244374223441 deg C3 = 66.688934068497 km^2/s^2 VMAG = 20.427276919287 km/s Semilatus Rectum = 7146742406.2303 km AZI = 147.49685866790 deg Angular Momentum = 15299605462.066 km^2/s VFPA = 81.604675126388 deg Beta Angle = 0.0000000000000 deg RAV = 147.36209022113 deg Periapsis Altitude = 742445785.66887 km DECV = -56.706156931156 deg VelPeriapsis = 20.587734350280 km/s Planetodetic Properties Hyperbolic Parameters --------------------------- -------------------------------- LST = 57.091511864634 deg BdotT = 1106709098.3721 km MHA = 89.549505446150 deg BdotR = -1511684988.1690 km Latitude = -0.1197351351783 deg B Vector Angle = -53.792030335386 deg Longitude = -32.457993581516 deg B Vector Mag = 1873498473.9453 km Altitude = 756396015.94261 km DLA = -45.036596615461 deg RLA = -148.23010222149 deg Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 Maneuver Summary ----------------- Impulsive Burn: ToInterceptEuropa Spacecraft: Spacecraft Origin: Jupiter Axes: VNB Delta V Vector: Element 1: 0.0288466790700 km/s Element 2: 0.0000000000000 km/s Element 3: 0.6220149148199 km/s No mass depletion ====== Propagate Command: Free flight to Europa orbital plane Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 03 Nov 2024 09:27:08.233 30617.8938452844 TAI Epoch: 03 Nov 2024 09:27:45.233 30617.8942735252 TT Epoch: 03 Nov 2024 09:28:17.417 30617.8946460252 TDB Epoch: 03 Nov 2024 09:28:17.415 30617.8946460084 Cartesian State Keplerian State --------------------------- -------------------------------- X = 220049795.19668 km SMA = 622663228.56520 km Y = 724405428.52095 km ECC = 0.2195255911847 Z = -8039720.4980640 km INC = 22.389010244047 deg VX = -10.212211338867 km/sec RAAN = 74.580146133801 deg VY = 3.6461580440305 km/sec AOP = 186.68485733187 deg VZ = 4.4548170902532 km/sec TA = 171.71762791451 deg MA = 167.39876159762 deg EA = 169.65700247974 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 757132600.23751 km Mean Motion = 2.344639020e-08 deg/sec RA = 73.102997939798 deg Orbit Energy = -106.56839357914 km^2/s^2 DEC = -0.6084148403573 deg C3 = -213.13678715828 km^2/s^2 VMAG = 11.723016856567 km/s Semilatus Rectum = 9029258839.7169 km AZI = 67.618833065850 deg Angular Momentum = 8868643946.9791 km^2/s VFPA = 87.686553985695 deg Beta Angle = 0.0000000000000 deg RAV = 160.35145195798 deg Periapsis Altitude = 485276725.20546 km DECV = 22.334056143705 deg VelPeriapsis = 18.249263115995 km/s VelApoapsis = 11.679199636914 km/s Orbit Period = 267980923.90729 s Planetodetic Properties --------------------------- LST = 58.382322867228 deg MHA = 257.66681684296 deg Latitude = -0.2675528318402 deg Longitude = 160.71550602427 deg Altitude = 756436610.23751 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 ====== Propagate Command: Free flight to P line Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 07 Nov 2024 13:32:56.527 30622.0645431407 TAI Epoch: 07 Nov 2024 13:33:33.527 30622.0649713815 TT Epoch: 07 Nov 2024 13:34:05.711 30622.0653438815 TDB Epoch: 07 Nov 2024 13:34:05.710 30622.0653438654 Cartesian State Keplerian State --------------------------- -------------------------------- X = 217838810.42886 km SMA = 392554655.71851 km Y = 725529592.30083 km ECC = 0.9692699735663 Z = -6902143.9581110 km INC = 69.167566584610 deg VX = -0.0541712618427 km/sec RAAN = 253.08907522450 deg VY = 2.7183267987996 km/sec AOP = 2.6215845656500 deg VZ = -2.2142473929251 km/sec TA = 177.93696317264 deg MA = 147.91282458758 deg EA = 163.59620670921 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 757558298.89487 km Mean Motion = 4.683878472e-08 deg/sec RA = 73.287720450615 deg Orbit Energy = -169.03689471607 km^2/s^2 DEC = -0.5220313611276 deg C3 = -338.07378943215 km^2/s^2 VMAG = 3.5064407349558 km/s Semilatus Rectum = 4859863136.1046 km AZI = 159.16666163262 deg Angular Momentum = 1775578917.3849 km^2/s VFPA = 41.946182656136 deg Beta Angle = 0.0000000000000 deg RAV = 91.141648569732 deg Periapsis Altitude = 11367224.946888 km DECV = -39.159403017599 deg VelPeriapsis = 147.18952826443 km/s VelApoapsis = 2.2968603365913 km/s Orbit Period = 134144925.94077 s Planetodetic Properties --------------------------- LST = 58.576456702528 deg MHA = 316.82566352145 deg Latitude = -0.2051518428108 deg Longitude = 101.75079318108 deg Altitude = 756862308.89487 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 ====== Maneuver Command: Apply ToInterceptEuropa_Correction Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 07 Nov 2024 13:32:56.527 30622.0645431407 TAI Epoch: 07 Nov 2024 13:33:33.527 30622.0649713815 TT Epoch: 07 Nov 2024 13:34:05.711 30622.0653438815 TDB Epoch: 07 Nov 2024 13:34:05.710 30622.0653438654 Cartesian State Keplerian State --------------------------- -------------------------------- X = 217838810.42886 km SMA = 393137000.72081 km Y = 725529592.30083 km ECC = 0.9680690332320 Z = -6902143.9581110 km INC = 69.150201938488 deg VX = -0.0553978964523 km/sec RAAN = 253.08889407786 deg VY = 2.7739840904505 km/sec AOP = 2.7082319523077 deg VZ = -2.2578421273141 km/sec TA = 177.85038023392 deg MA = 147.24992634161 deg EA = 163.24226681157 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 757558298.89487 km Mean Motion = 4.673475141e-08 deg/sec RA = 73.287720450615 deg Orbit Energy = -168.78650416351 km^2/s^2 DEC = -0.5220313611276 deg C3 = -337.57300832703 km^2/s^2 VMAG = 3.5771368065644 km/s Semilatus Rectum = 4864000521.4802 km AZI = 159.14929616126 deg Angular Momentum = 1810731158.8461 km^2/s VFPA = 41.927804924141 deg Beta Angle = 0.0000000000000 deg RAV = 91.144074261479 deg Periapsis Altitude = 11857254.505274 km DECV = -39.137749113720 deg VelPeriapsis = 144.24407634898 km/s VelApoapsis = 2.3402902696005 km/s Orbit Period = 134443537.57611 s Planetodetic Properties --------------------------- LST = 58.576456702528 deg MHA = 316.82566352145 deg Latitude = -0.2051518428108 deg Longitude = 101.75079318108 deg Altitude = 756862308.89487 km Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000 Maneuver Summary ----------------- Impulsive Burn: ToInterceptEuropa_Correction Spacecraft: Spacecraft Origin: Jupiter Axes: VNB Delta V Vector: Element 1: 0.0000000000000 km/s Element 2: 0.0499991290552 km/s Element 3: -0.0499982670354 km/s No mass depletion ====== Propagate Command: Free flight to Europa orbital plane Spacecraft : Spacecraft Coordinate System: SunMJ2000Ec Time System Gregorian Modified Julian ---------------------------------------------------------------------- UTC Epoch: 08 Nov 2024 16:26:41.549 30623.1852031087 TAI Epoch: 08 Nov 2024 16:27:18.549 30623.1856313494 TT Epoch: 08 Nov 2024 16:27:50.733 30623.1860038494 TDB Epoch: 08 Nov 2024 16:27:50.731 30623.1860038335 Cartesian State Keplerian State --------------------------- -------------------------------- X = 217691115.65597 km SMA = -1913672492.8372 km Y = 725895094.47076 km ECC = 1.3895152295189 Z = -7860251.6022142 km INC = 57.818367018638 deg VX = -9.5873055639421 km/sec RAAN = 252.93239245505 deg VY = 5.6468343327788 km/sec AOP = 167.03943194869 deg VZ = -17.197931039479 km/sec TA = 13.662694078263 deg MA = 2.1726328762524 deg HA = 5.5468632527640 deg Spherical State Other Orbit Data --------------------------- -------------------------------- RMAG = 757875249.34352 km Mean Motion = 4.351654383e-09 deg/sec RA = 73.306361689306 deg Orbit Energy = 34.674804731407 km^2/s^2 DEC = -0.5942499341868 deg C3 = 69.349609462814 km^2/s^2 VMAG = 20.483456690630 km/s Semilatus Rectum = 9206265914.9816 km AZI = 147.81642766136 deg Angular Momentum = 15374703421.248 km^2/s VFPA = 82.049909334575 deg Beta Angle = 0.0000000000000 deg RAV = 149.50230819772 deg Periapsis Altitude = 744708590.27147 km DECV = -57.098011802382 deg VelPeriapsis = 20.625984637294 km/s Planetodetic Properties Hyperbolic Parameters --------------------------- -------------------------------- LST = 58.585840624166 deg BdotT = 1092664485.4587 km MHA = 332.72155277652 deg BdotR = -1488164235.9322 km Latitude = -0.2791446036303 deg B Vector Angle = -53.712526197021 deg Longitude = 85.864287847644 deg B Vector Mag = 1846225465.8872 km Altitude = 757179259.34352 km DLA = -45.176365308298 deg RLA = -146.35214885826 deg Spacecraft Properties ------------------------------ Cd = 2.200000 Drag area = 15.00000 m^2 Cr = 1.800000 Reflective (SRP) area = 1.000000 m^2 Dry mass = 850.00000000000 kg Total mass = 850.00000000000 kg SPADDragScaleFactor = 1.000000 SPADSRPScaleFactor = 1.000000