Orbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total42 of 74994%12 of 3667%104010112020
getJacobianWrtParameters(PositionAngle, double[][])324659%8433%6891901
getJacobianWrtCartesian(PositionAngle, double[][])86789%3975%3811901
getKeplerianPeriod()21789%1150%120201
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int)101100%n/a010401
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int)86100%n/a010401
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int)71100%n/a010401
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int)56100%n/a010401
Orbit(TimeStampedPVCoordinates, Frame, double)54100%2100%0201201
Orbit(Frame, AbsoluteDate, double)41100%n/a0101301
fillHalfRow(double, Vector3D, double, Vector3D, double[], int)41100%n/a010401
getPVCoordinates(Frame)26100%4100%030601
fillHalfRow(double, Vector3D, double[], int)26100%n/a010401
createInverseJacobian(PositionAngle)21100%n/a010501
ensurePseudoInertialFrame(Frame)14100%2100%020301
getKeplerianMeanMotion()12100%n/a010201
getPVCoordinates()10100%2100%020301
getPVCoordinates(AbsoluteDate, Frame)9100%n/a010101
getFrame()3100%n/a010101
getMu()3100%n/a010101
getDate()3100%n/a010101