Ephemeris

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total13 of 25495%0 of 12100%120347114
resetIntermediateState(SpacecraftState, boolean)70%n/a111111
basicPropagate(AbsoluteDate)64187%2100%0221001
Ephemeris(List, int)91100%4100%0301601
isAdditionalStateManaged(String)31100%6100%040601
getManagedAdditionalStates()30100%n/a010501
writeReplace()11100%n/a010101
resetInitialState(SpacecraftState)7100%n/a010101
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
getFrame()3100%n/a010101