?? satellite111.sa
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stk.v.4.3BEGIN SatelliteName Satellite111BEGIN VehiclePath CentralBody Earth BEGIN Interval StartTime 1 Jun 2002 12:00:00.000000000 StopTime 2 Jun 2002 12:00:00.000000000 END Interval StoreEphemeris Yes SmoothInterp No BEGIN TwoBody EphemEpoch 1 Jun 2002 12:00:00.000000000 StartTime 1 Jun 2002 12:00:00.000000000 StopTime 2 Jun 2002 12:00:00.000000000 SemiMajorAxis 0.000000000000e+000 AltitudeOfApogee 0.000000000000e+000 AltitudeOfPerigee 0.000000000000e+000 RadiusOfApogee 0.000000000000e+000 RadiusOfPerigee 4.216416963714e+007 PeriodOfOrbit 0.000000000000e+000 MeanMotion 0.000000000000e+000 Inclination 0.000000000000e+000 Eccentricity 0.000000000000e+000 ArgOfPerigee 0.000000000000e+000 LongAscenNode 1.000000000000e+002 RightAscension 1.697696437620e+002 TrueAnomaly 0.000000000000e+000 MeanAnomaly 0.000000000000e+000 TimePastAscenNode 0.000000000000e+000 TimePastPerigee 0.000000000000e+000 TimeStep 60.000000 OrbitGranularity 0.000000000000e+000 NumberOfPasses 0 DisplayCoordType 4 DisplayCoordSys J2000 EllipseType Osculating BEGIN DisplayFlags SizeShapeType PeriodEcc AscenNodeType RightAscension AnomalyType TrueAnomaly DelLType L DelGType G DelHType H EquiOrbType SMA FPAType HorizontalFPA MixFPAType HorizontalFPA END DisplayFlags END TwoBodyBEGIN PassDefn Break Ascending CoordSystem Inertial BreakType Latitude BreakAngle 0.000000000000e+000 PartialPassMethod ByMeanArgLatitude DisplayFlag Both FirstPass 1 FirstPath 1 RepeatCycle 1 MaintainPassNum No RangeFirstPass 1 RangeLastPass 2147483647 DisplayScheme AllEphemeris ScenarioEpoch 1 Jun 2002 12:00:00.000000000 Passes END PassesEND PassDefnEND VehiclePathBEGIN EphemerisNumberOfEphemerisPoints 1441ScenarioEpoch 1 Jun 2002 12:00:00.000000000InterpolationMethod LagrangeInterpolationOrder 5CentralBody EarthCoordinateSystem Fixed BlockingFactor 20EphemerisTimePosVel
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