CartesianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 1,317100%2 of 4295%2600240039
shiftPVHyperbolic(double)259100%2100%0204001
shiftPVElliptic(double)252100%2100%0204101
getPVDerivatives()77100%n/a0101101
addKeplerContribution(PositionAngleType, double, double[])75100%n/a0101201
getEDot()64100%2100%0201301
getHxDot()61100%1583%1401201
getHyDot()60100%1583%1401201
getE()57100%2100%0201001
toString()48100%n/a0101101
initEquinoctial()40100%4100%030701
getHx()36100%4100%030401
getHy()35100%4100%030401
getADot()34100%2100%020701
CartesianOrbit(Orbit)33100%4100%030801
shiftedBy(double)24100%2100%020201
getIDot()23100%2100%020701
getA()20100%n/a010301
CartesianOrbit(TimeStampedPVCoordinates, Frame, double)14100%n/a010401
CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double)10100%n/a010201
getI()6100%n/a010101
getEquinoctialEx()6100%n/a010201
getEquinoctialExDot()6100%n/a010201
getEquinoctialEy()6100%n/a010201
getEquinoctialEyDot()6100%n/a010201
getLv()6100%n/a010201
getLvDot()6100%n/a010201
getLE()6100%n/a010201
getLEDot()6100%n/a010201
getLM()6100%n/a010201
getLMDot()6100%n/a010201
writeReplace()6100%n/a010101
static {...}5100%n/a010101
initPosition()4100%n/a010101
hasDerivatives()3100%n/a010101
initPVCoordinates()3100%n/a010101
getType()100%n/a010101
computeJacobianMeanWrtCartesian()100%n/a010101
computeJacobianEccentricWrtCartesian()100%n/a010101
computeJacobianTrueWrtCartesian()100%n/a010101