Orbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total13 of 90098%5 of 5290%5553150027
getJacobianWrtParameters(PositionAngleType, double[][])57093%21083%2811901
getJacobianWrtCartesian(PositionAngleType, double[][])56793%11191%1811901
hasNonKeplerianAcceleration(PVCoordinates, double)24195%1583%1411201
getKeplerianPeriod()1794%1150%120201
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int)143100%n/a010801
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int)124100%n/a010801
Orbit(TimeStampedPVCoordinates, Frame, double)54100%2100%0201501
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int)53100%n/a010401
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int)44100%n/a010401
Orbit(Frame, AbsoluteDate, double)35100%n/a0101301
fillHalfRow(double, Vector3D, double, Vector3D, double[], int)35100%n/a010401
getPVCoordinates(Frame)26100%4100%030601
getPosition(Frame)26100%4100%030601
fillHalfRow(double, Vector3D, double[], int)26100%n/a010401
createInverseJacobian(PositionAngleType)21100%n/a010501
ensurePseudoInertialFrame(Frame)16100%2100%020401
getPVCoordinates()15100%2100%020401
getKeplerianMeanMotion()12100%n/a010201
getPosition()10100%2100%020301
isElliptical()9100%2100%020101
getPVCoordinates(AbsoluteDate, Frame)9100%n/a010101
getPosition(AbsoluteDate, Frame)9100%n/a010101
hasDerivatives()8100%2100%020101
getMeanAnomalyDotWrtA()8100%n/a010101
getFrame()3100%n/a010101
getMu()3100%n/a010101
getDate()3100%n/a010101