📄 geo.sa
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RangeConstraint 5000.000 ApoPeriPad 30000.000 OrbitPathPad 30000.000 TimeDistPad 30000.000 OutOfDate 2592000.000 UseApogeePerigeeFilter Yes UsePathFilter Yes UseTimeFilter Yes UseOutOfDate Yes CreateSats No MaxSatsToCreate 500 UseLaunchWindow Yes LaunchWindowStart 0.000 LaunchWindowStop 0.000 ShowLine Yes AnimHighlight Yes StaticHighlight Yes UseCrossRefDb Yes CollisionDB STKData\Databases\Satellite\stkAllTLE.tce CollisionCrossRefDB STKData\Databases\Satellite\stkAllTLE.sd END ClsApp BEGIN ExternData END ExternData BEGIN Lifetime Semi_parameter 6.678137000000e+006 Eccentricity 0.000000000000e+000 Argument_Perigee 0.000000000000e+000 RA_Asc_Node 0.000000000000e+000 Inclination 4.974188368180e-001 UTC_Year 1997 UTC_Month 1 UTC_Day 1 UTC_Hour 0 UTC_Minute 0 UTC_Second 0.000000000000e+000 Rev_Count_Limit 99999 Revs_Calculation 10 Gaussian_Quadratures 1 Solar_Flux_Flag 0 Gravity_Model_Flag 1 Reflection_Coef 1.000000000000e+000 Sun_Area 1.543000000000e+001 Mass 1.000000000000e+003 Drag_Coef 2.000000000000e+000 Drag_Area 1.365000000000e+001 Rotating_Atm_Flag 0 Compute_Gamma_Flag 0 Initial_Time 0.000000000000e+000 Decay_Alt 6.500000000000e+004 Solar_Flux_Filename SolFlx0900_Schatten.dat END Lifetime BEGIN AccessConstraints LineOfSight IncludeIntervals END AccessConstraints BEGIN AttitudeSimulator UseReferenceForAttitude No UseForAttitude No UsePctCmplt Yes PctCmpltDivisor 24 PctCmpltTitle Attitude Simulation UseAnimate No AnimateSampling 1.0000000000000000e+000 StartTime 20 Sep 2002 15:00:00.000000000 StopTime 20 Sep 2002 16:00:00.000000000 Step 0.0000000000000000e+000 InitialTime 20 Sep 2002 15:00:00.000000000 BEGIN InitialAttitude 0.0000000000000000e+000 0.0000000000000000e+000 0.0000000000000000e+000 1.0000000000000000e+000 END InitialAttitude Representation 0 Sequence 0 BEGIN InitialAngVel 0.0000000000000000e+000 0.0000000000000000e+000 0.0000000000000000e+000 END InitialAngVel BEGIN InitialMomentumBias 0.0000000000000000e+000 0.0000000000000000e+000 0.0000000000000000e+000 END InitialMomentumBias UseMomentumBias No BEGIN IntegratedSimulation BEGIN Integrator Type RK78 RelTol 1.0000000000000000e-003 AbsTol 9.9999999999999995e-007 MinStep 9.9999999999999995e-007 UseMinStep No MaxStep 1.0000000000000000e+001 UseMaxStep No NumIter 10 UseIter No UseStat No END Integrator BEGIN Formulation BEGIN EnvironmentData UseApproxAlt No MeanFlux 100 DailyFlux 150 GeoMagIndex 3.0000000000000000 RefAlt 0.0000000000000000 ScaleAlt 8500.0000000000000000 RefDensity 1.2170000000000001 DensityModel Exponential END EnvironmentData BEGIN InitList END InitList BEGIN UpdateList END UpdateList BEGIN PostList END PostList UseInitialUpdateStep No UseUpdateStep No END Formulation END IntegratedSimulation END AttitudeSimulator BEGIN ObjectCoverage END ObjectCoverage BEGIN Desc ShortText 0 LongText 0 END Desc BEGIN RCS Inherited True ClutterCoef 0.000000e+000 BEGIN RCSBAND ConstantValue 0.000000e+000 Swerling 0 BandData 3.000000e+006 3.000000e+011 END RCSBAND END RCS BEGIN Reference END Reference BEGIN AcquisitionData DataType IIRV9 MessageID 0 MessageClass 10 MessageOrigin A MessageDestination GSVL VectorType 1 VectorSource 1 CoordinateSystem 1 SupportID 0 VehicleIdentificationCode 1 CounterStart 1 Area 0.000000 SolarReflectivity 0.000000 OriginRouteMsg HJSC IRON 1 PerturbationCoeffType 0 DragCoefficient 2.000000 SRPCoefficient 1.000000 END AcquisitionData BEGIN Identification END Identification BEGIN Crdn BEGIN ANGLE Type ANGLE_BETWEEN Name SunMoon Description Angle between the sun and moon vectors Origin BEGIN VECTOR Type VECTOR_LINKTO Name Sun END VECTOR Destination BEGIN VECTOR Type VECTOR_LINKTO Name Moon END VECTOR END ANGLE END Crdn BEGIN DIS Begin Input End Input Begin Output Enable Off ForceID 1 EntityID 0:0:0 PriEntityType 0:0:0:0:0:0:0 AltEntityType 0:0:0:0:0:0:0 DistanceThresh 1.000000 End Output END DIS BEGIN VO END VO BEGIN PODS VehicleID 0 ODStartTime 1 Jun 2003 12:00:00.000000000 ODStopTime 1 Jun 2003 16:00:00.000000000 GenerateEphem On EstimateDrag Off EstimateSRP Off EstimateOrb On UpdateCovariance On DragSigma 0.500000 SRPSigma 0.500000 BEGIN State StartTime 1 Jun 2003 12:00:00.000000000 StopTime 1 Jun 2003 16:00:00.000000000 Epoch 1 Jun 2003 12:00:00.000000000 TimeStep 60.000000 X -2.301084801966e+006 Y 6.254942499445e+006 Z -2.277820636920e+003 VX -5.929257428679e+003 VY -2.179925885720e+003 VZ 3.693481262710e+003 Area 1.0000 DragCoefficient 2.300000 SRPCoefficient 1.500000 UseDrag On UseSRP On MaxDegree 36 DisplayCoordType 0 DisplayCoordSys J2000 END State BEGIN Covariance Covar1_1 1.000000000000e+014 Covar2_2 1.000000000000e+014 Covar3_3 1.000000000000e+014 Covar4_4 1.000000000000e+014 Covar5_5 1.000000000000e+014 Covar6_6 1.000000000000e+014 END Covariance UseTransponderDelay No TransponderDelay 0.000000000000e+000 END PODSEND ExtensionsBEGIN SubObjectsClass Transmitter GEOTransEND ClassEND SubObjectsEND Satellite
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