TLE

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total122 of 1,38991%21 of 8073%227818218138
hashCode()1100%n/a11161611
buildLine1()1223595%1150%1223601
TLE(String, String, TimeScale)268100%2100%0203601
buildLine2()171100%n/a0102201
equals(Object)118100%172357%17210901
isFormatOK(String, String)108100%31381%3901501
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
writeReplace()10100%n/a010101
TLE(String, String)8100%n/a010201
getLine1()8100%2100%020301
getLine2()8100%2100%020301
getBStar()6100%n/a010101
getBStar(AbsoluteDate)5100%n/a010101
stateToTLE(SpacecraftState, TLE, TleGenerationAlgorithm)5100%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