TLE

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total122 of 1,69892%22 of 9276%238617281140
hashCode()1100%n/a11161611
stateToTLE(SpacecraftState, TLE, TimeScale, Frame, double, int)1220794%21285%2814301
TLE(String, String, TimeScale)268100%2100%0203601
buildLine1()233100%n/a0103301
buildLine2()172100%n/a0102201
equals(Object)118100%172357%17210901
isFormatOK(String, String)108100%31381%3901501
newTLE(KeplerianOrbit, TLE, TimeScale)97100%n/a0102101
formatExponentMarkerFree(String, double, int, char, int, boolean)95100%10100%0601201
TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double, TimeScale)79100%n/a0102301
checksum(CharSequence)31100%6100%040801
TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double)24100%n/a010301
static {...}16100%n/a010601
toString()14100%n/a010101
stateToTLE(SpacecraftState, TLE)10100%n/a010301
convert(Orbit, Frame)10100%n/a010101
TLE(String, String)8100%n/a010201
getLine1()8100%2100%020301
getLine2()8100%2100%020301
stateToTLE(SpacecraftState, TLE, TimeScale, Frame)8100%n/a010101
getBStar()4100%n/a010101
getParametersDrivers()4100%n/a010101
getUtc()3100%n/a010101
getSatelliteNumber()3100%n/a010101
getClassification()3100%n/a010101
getLaunchYear()3100%n/a010101
getLaunchNumber()3100%n/a010101
getLaunchPiece()3100%n/a010101
getEphemerisType()3100%n/a010101
getElementNumber()3100%n/a010101
getDate()3100%n/a010101
getMeanMotion()3100%n/a010101
getMeanMotionFirstDerivative()3100%n/a010101
getMeanMotionSecondDerivative()3100%n/a010101
getE()3100%n/a010101
getI()3100%n/a010101
getPerigeeArgument()3100%n/a010101
getRaan()3100%n/a010101
getMeanAnomaly()3100%n/a010101
getRevolutionNumberAtEpoch()3100%n/a010101