EcksteinHechlerPropagator

Element	Missed Instructions	Cov.	Missed Branches	Cov.	Missed	Cxty	Missed	Lines	Missed	Methods
Total	12 of 1,668	99%	6 of 22	73%	6	24	1	152	0	13
computeMeanParameters(CircularOrbit)		97%		73%	6	12	1	43	0	1
propagateOrbit(AbsoluteDate)		100%		n/a	0	1	0	74	0	1
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double)		100%		n/a	0	1	0	14	0	1
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics)		100%		n/a	0	1	0	2	0	1
resetInitialState(SpacecraftState)		100%		n/a	0	1	0	4	0	1
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double)		100%		n/a	0	1	0	2	0	1
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double, double)		100%		n/a	0	1	0	2	0	1
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double)		100%		n/a	0	1	0	2	0	1
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider)		100%		n/a	0	1	0	2	0	1
EcksteinHechlerPropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider)		100%		n/a	0	1	0	2	0	1
EcksteinHechlerPropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider)		100%		n/a	0	1	0	2	0	1
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider)		100%		n/a	0	1	0	2	0	1
getMass(AbsoluteDate)		100%		n/a	0	1	0	1	0	1