FieldKeplerianPropagator

Element	Missed Instructions	Cov.	Missed Branches	Cov.	Missed	Cxty	Missed	Lines	Missed	Methods
Total	33 of 208	84%	3 of 6	50%	4	13	6	39	2	10
resetIntermediateState(FieldSpacecraftState, boolean)		0%		0%	2	2	4	4	1	1
FieldKeplerianPropagator(FieldOrbit, AttitudeProvider, double)		0%		n/a	1	1	2	2	1	1
resetInitialState(FieldSpacecraftState)		91%		50%	1	2	0	8	0	1
FieldKeplerianPropagator(FieldOrbit, AttitudeProvider, double, RealFieldElement)		100%		n/a	0	1	0	8	0	1
fixState(FieldOrbit, FieldAttitude, RealFieldElement, double)		100%		n/a	0	1	0	6	0	1
propagateOrbit(FieldAbsoluteDate)		100%		100%	0	2	0	4	0	1
FieldKeplerianPropagator(FieldOrbit)		100%		n/a	0	1	0	2	0	1
FieldKeplerianPropagator(FieldOrbit, AttitudeProvider)		100%		n/a	0	1	0	2	0	1
FieldKeplerianPropagator(FieldOrbit, double)		100%		n/a	0	1	0	2	0	1
getMass(FieldAbsoluteDate)		100%		n/a	0	1	0	1	0	1