IntegratedEphemeris

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total77 of 32977%9 of 2462%9251760313
writeReplace()406562%6225%4591701
basicPropagate(AbsoluteDate)205071%3350%2451401
resetIntermediateState(SpacecraftState, boolean)70%n/a111111
propagateOrbit(AbsoluteDate)50%n/a111111
getMass(AbsoluteDate)50%n/a111111
IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, boolean, ContinuousOutputModel, Map, List, String[])58100%4100%0301401
setInterpolationDate(AbsoluteDate)49100%6100%040601
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