KeplerianPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total6 of 26498%1 of 1694%118254010
writeReplace()611995%11192%1722201
KeplerianPropagator(Orbit, AttitudeProvider, double, double)47100%n/a0101001
propagateOrbit(AbsoluteDate)21100%2100%020401
resetIntermediateState(SpacecraftState, boolean)20100%2100%020501
resetInitialState(SpacecraftState)14100%n/a010401
KeplerianPropagator(Orbit)8100%n/a010201
KeplerianPropagator(Orbit, AttitudeProvider)8100%n/a010201
KeplerianPropagator(Orbit, double)7100%n/a010201
KeplerianPropagator(Orbit, AttitudeProvider, double)7100%n/a010201
getMass(AbsoluteDate)7100%n/a010101