CartesianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total19 of 1,66198%5 of 6492%5763278044
meanToHyperbolicEccentric(double, double)1211590%21487%2922301
meanToEccentric(double, double, double)76990%1375%1311601
shiftPVElliptic(double)307100%2100%0203901
shiftPVHyperbolic(double)258100%2100%0204001
addKeplerContribution(PositionAngle, double, double[])75100%n/a0101201
getEDot()68100%2100%0201201
getHxDot()63100%1583%1401101
getHyDot()62100%1583%1401101
getE()59100%2100%0201001
getPositionDS()54100%n/a010501
getVelocityDS()54100%n/a010501
toString()48100%n/a0101101
initEquinoctial()41100%4100%030701
getADot()36100%2100%020601
getHx()35100%4100%030401
getHy()34100%4100%030401
CartesianOrbit(Orbit)33100%4100%030801
shiftedBy(double)26100%2100%020201
getIDot()25100%2100%020601
getA()21100%n/a010301
create6x6Identity()19100%2100%020401
interpolate(AbsoluteDate, Stream)17100%n/a010401
CartesianOrbit(TimeStampedPVCoordinates, Frame, double)14100%n/a010401
CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double)10100%n/a010201
static {...}7100%n/a010101
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
hasDerivatives()3100%n/a010101
initPVCoordinates()3100%n/a010101
computeJacobianMeanWrtCartesian()3100%n/a010101
computeJacobianEccentricWrtCartesian()3100%n/a010101
computeJacobianTrueWrtCartesian()3100%n/a010101
lambda$interpolate$0(Orbit)3100%n/a010101
getType()100%n/a010101