IntegratedEphemeris

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total61 of 29980%6 of 1867%7221455313
writeReplace()406562%6225%4591901
resetIntermediateState(SpacecraftState, boolean)70%n/a111111
propagateOrbit(AbsoluteDate)50%n/a111111
getMass(AbsoluteDate)50%n/a111111
basicPropagate(AbsoluteDate)44291%2100%022901
IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, boolean, DenseOutputModel, Map, List, String[])58100%4100%0301401
getInterpolatedState(AbsoluteDate)43100%4100%030401
resetInitialState(SpacecraftState)7100%n/a010101
getInitialState()7100%n/a010101
getPVCoordinates(AbsoluteDate, Frame)6100%n/a010101
getFrame()4100%n/a010101
getMinDate()3100%n/a010101
getMaxDate()3100%n/a010101