CartesianOrbit

Element	Missed Instructions	Cov.	Missed Branches	Cov.	Missed	Cxty	Missed	Lines	Missed	Methods
Total	18 of 940	98%	0 of 40	100%	1	59	2	181	1	39
shiftedBy(TimeOffset)		0%		n/a	1	1	2	2	1	1
shiftPV(double)		100%		100%	0	2	0	17	0	1
getPVDerivatives()		100%		n/a	0	1	0	11	0	1
addKeplerContribution(PositionAngleType, double, double[])		100%		n/a	0	1	0	12	0	1
getEDot()		100%		100%	0	2	0	13	0	1
getHxDot()		100%		100%	0	4	0	12	0	1
getHyDot()		100%		100%	0	4	0	12	0	1
getE()		100%		100%	0	2	0	10	0	1
toString()		100%		n/a	0	1	0	11	0	1
initEquinoctial()		100%		100%	0	3	0	7	0	1
getHx()		100%		100%	0	3	0	4	0	1
getADot()		100%		100%	0	2	0	7	0	1
getHy()		100%		100%	0	3	0	4	0	1
CartesianOrbit(Orbit)		100%		100%	0	3	0	8	0	1
inFrame(Frame)		100%		100%	0	2	0	4	0	1
getIDot()		100%		100%	0	2	0	7	0	1
getA()		100%		n/a	0	1	0	3	0	1
shiftedBy(double)		100%		n/a	0	1	0	2	0	1
CartesianOrbit(TimeStampedPVCoordinates, Frame, double)		100%		n/a	0	1	0	4	0	1
CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double)		100%		n/a	0	1	0	2	0	1
getI()		100%		n/a	0	1	0	1	0	1
getEquinoctialEx()		100%		n/a	0	1	0	2	0	1
getEquinoctialExDot()		100%		n/a	0	1	0	2	0	1
getEquinoctialEy()		100%		n/a	0	1	0	2	0	1
getEquinoctialEyDot()		100%		n/a	0	1	0	2	0	1
getLv()		100%		n/a	0	1	0	2	0	1
getLvDot()		100%		n/a	0	1	0	2	0	1
getLE()		100%		n/a	0	1	0	2	0	1
getLEDot()		100%		n/a	0	1	0	2	0	1
getLM()		100%		n/a	0	1	0	2	0	1
getLMDot()		100%		n/a	0	1	0	2	0	1
static {...}		100%		n/a	0	1	0	1	0	1
initPosition()		100%		n/a	0	1	0	1	0	1
hasNonKeplerianAcceleration()		100%		n/a	0	1	0	1	0	1
initPVCoordinates()		100%		n/a	0	1	0	1	0	1
getType()		100%		n/a	0	1	0	1	0	1
computeJacobianMeanWrtCartesian()		100%		n/a	0	1	0	1	0	1
computeJacobianEccentricWrtCartesian()		100%		n/a	0	1	0	1	0	1
computeJacobianTrueWrtCartesian()		100%		n/a	0	1	0	1	0	1