EphemerisSegmentPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 133100%0 of 0n/a0902909
EphemerisSegmentPropagator(EphemerisFile.EphemerisSegment)68100%n/a0101701
getPVCoordinates(AbsoluteDate, Frame)20100%n/a010401
propagateOrbit(AbsoluteDate)16100%n/a010201
resetIntermediateState(SpacecraftState, boolean)7100%n/a010101
resetInitialState(SpacecraftState)7100%n/a010101
getInitialState()5100%n/a010101
getMinDate()4100%n/a010101
getMaxDate()4100%n/a010101
getMass(AbsoluteDate)2100%n/a010101