SpacecraftState

Element	Missed Instructions	Cov.	Missed Branches	Cov.	Missed	Cxty	Missed	Lines	Missed	Methods
Total	1 of 639	100%	2 of 32	94%	2	54	1	103	0	38
ensureCompatibleAdditionalStates(SpacecraftState)		99%		83%	2	7	1	13	0	1
interpolate(AbsoluteDate, Collection)		100%		100%	0	6	0	26	0	1
SpacecraftState(Orbit, Attitude, double, Map)		100%		100%	0	3	0	12	0	1
checkConsistency(Orbit, Attitude)		100%		100%	0	3	0	5	0	1
addAdditionalState(String, double[])		100%		n/a	0	1	0	4	0	1
getAdditionalState(String)		100%		100%	0	2	0	3	0	1
toTransform()		100%		n/a	0	1	0	2	0	1
SpacecraftState(Orbit)		100%		n/a	0	1	0	2	0	1
SpacecraftState(Orbit, double)		100%		n/a	0	1	0	2	0	1
SpacecraftState(Orbit, Map)		100%		n/a	0	1	0	2	0	1
SpacecraftState(Orbit, double, Map)		100%		n/a	0	1	0	2	0	1
shiftedBy(double)		100%		n/a	0	1	0	1	0	1
SpacecraftState(Orbit, Attitude)		100%		n/a	0	1	0	2	0	1
SpacecraftState(Orbit, Attitude, double)		100%		n/a	0	1	0	2	0	1
SpacecraftState(Orbit, Attitude, Map)		100%		n/a	0	1	0	2	0	1
writeReplace()		100%		n/a	0	1	0	1	0	1
hasAdditionalState(String)		100%		n/a	0	1	0	1	0	1
getPVCoordinates(Frame)		100%		n/a	0	1	0	1	0	1
getDate()		100%		n/a	0	1	0	1	0	1
getFrame()		100%		n/a	0	1	0	1	0	1
getAdditionalStates()		100%		n/a	0	1	0	1	0	1
getMu()		100%		n/a	0	1	0	1	0	1
getKeplerianPeriod()		100%		n/a	0	1	0	1	0	1
getKeplerianMeanMotion()		100%		n/a	0	1	0	1	0	1
getA()		100%		n/a	0	1	0	1	0	1
getEquinoctialEx()		100%		n/a	0	1	0	1	0	1
getEquinoctialEy()		100%		n/a	0	1	0	1	0	1
getHx()		100%		n/a	0	1	0	1	0	1
getHy()		100%		n/a	0	1	0	1	0	1
getLv()		100%		n/a	0	1	0	1	0	1
getLE()		100%		n/a	0	1	0	1	0	1
getLM()		100%		n/a	0	1	0	1	0	1
getE()		100%		n/a	0	1	0	1	0	1
getI()		100%		n/a	0	1	0	1	0	1
getPVCoordinates()		100%		n/a	0	1	0	1	0	1
getOrbit()		100%		n/a	0	1	0	1	0	1
getAttitude()		100%		n/a	0	1	0	1	0	1
getMass()		100%		n/a	0	1	0	1	0	1