KeplerianPropagator

Element	Missed Instructions	Cov.	Missed Branches	Cov.	Missed	Cxty	Missed	Lines	Missed	Methods
Total	3 of 195	98%	1 of 8	87%	1	14	0	47	0	10
resetInitialState(SpacecraftState)		90%		50%	1	2	0	9	0	1
fixState(Orbit, Attitude, double, double, Map)		100%		100%	0	2	0	10	0	1
KeplerianPropagator(Orbit, AttitudeProvider, double, double)		100%		n/a	0	1	0	9	0	1
propagateOrbit(AbsoluteDate)		100%		100%	0	2	0	4	0	1
resetIntermediateState(SpacecraftState, boolean)		100%		100%	0	2	0	5	0	1
KeplerianPropagator(Orbit)		100%		n/a	0	1	0	3	0	1
KeplerianPropagator(Orbit, double)		100%		n/a	0	1	0	2	0	1
KeplerianPropagator(Orbit, AttitudeProvider)		100%		n/a	0	1	0	2	0	1
KeplerianPropagator(Orbit, AttitudeProvider, double)		100%		n/a	0	1	0	2	0	1
getMass(AbsoluteDate)		100%		n/a	0	1	0	1	0	1