Orbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total12 of 84898%5 of 4488%5462136022
getJacobianWrtParameters(PositionAngle, double[][])57093%21083%2811901
getJacobianWrtCartesian(PositionAngle, double[][])56793%11191%1811901
getKeplerianPeriod()21789%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
hasNonKeplerianAcceleration(PVCoordinates, double)51100%1583%1401101
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int)44100%n/a010401
Orbit(Frame, AbsoluteDate, double)41100%n/a0101301
fillHalfRow(double, Vector3D, double, Vector3D, double[], int)35100%n/a010401
getPVCoordinates(Frame)26100%4100%030601
fillHalfRow(double, Vector3D, double[], int)26100%n/a010401
createInverseJacobian(PositionAngle)21100%n/a010501
ensurePseudoInertialFrame(Frame)16100%2100%020401
getKeplerianMeanMotion()12100%n/a010201
getPVCoordinates()10100%2100%020301
getPVCoordinates(AbsoluteDate, Frame)9100%n/a010101
hasDerivatives()8100%2100%020101
getFrame()3100%n/a010101
getMu()3100%n/a010101
getDate()3100%n/a010101