Ephemeris

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total7 of 30497%0 of 20100%126156116
resetIntermediateState(SpacecraftState, boolean)70%n/a111111
Ephemeris(List, int, double)94100%4100%0301801
basicPropagate(AbsoluteDate)83100%10100%0601401
isAdditionalStateManaged(String)31100%6100%040601
getManagedAdditionalStates()30100%n/a010501
writeReplace()13100%n/a010101
resetInitialState(SpacecraftState)7100%n/a010101
Ephemeris(List, int)6100%n/a010201
getPVCoordinates(AbsoluteDate, Frame)6100%n/a010101
propagateOrbit(AbsoluteDate)5100%n/a010101
getMass(AbsoluteDate)5100%n/a010101
getInitialState()5100%n/a010101
getMinDate()3100%n/a010101
getMaxDate()3100%n/a010101
getExtrapolationThreshold()3100%n/a010101
getFrame()3100%n/a010101