KeplerianElements

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 178100%0 of 0n/a023058023
validate(double)40100%n/a010801
KeplerianElements()27100%n/a0101001
generateKeplerianOrbit(Frame)23100%n/a010101
setEpoch(AbsoluteDate)6100%n/a010301
setA(double)6100%n/a010301
setE(double)6100%n/a010301
setI(double)6100%n/a010301
setRaan(double)6100%n/a010301
setPa(double)6100%n/a010301
setAnomaly(double)6100%n/a010301
setAnomalyType(PositionAngleType)6100%n/a010301
setMu(double)6100%n/a010301
setMeanMotion(double)4100%n/a010201
getEpoch()3100%n/a010101
getA()3100%n/a010101
getMeanMotion()3100%n/a010101
getE()3100%n/a010101
getI()3100%n/a010101
getRaan()3100%n/a010101
getPa()3100%n/a010101
getAnomaly()3100%n/a010101
getAnomalyType()3100%n/a010101
getMu()3100%n/a010101