buildLine1() |   | 95% |   | 50% | 1 | 2 | 2 | 36 | 0 | 1 |
TLE(String, String, TimeScale) |  | 100% |  | 100% | 0 | 2 | 0 | 36 | 0 | 1 |
buildLine2() |  | 100% | | n/a | 0 | 1 | 0 | 22 | 0 | 1 |
equals(Object) |  | 100% |   | 60% | 16 | 21 | 0 | 9 | 0 | 1 |
hashCode() |  | 100% | | n/a | 0 | 1 | 0 | 16 | 0 | 1 |
isFormatOK(String, String) |  | 100% |   | 81% | 3 | 9 | 0 | 15 | 0 | 1 |
formatExponentMarkerFree(String, double, int, char, int, boolean) |  | 100% |  | 100% | 0 | 6 | 0 | 12 | 0 | 1 |
TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double, TimeScale) |  | 100% | | n/a | 0 | 1 | 0 | 23 | 0 | 1 |
checksum(CharSequence) |  | 100% |  | 100% | 0 | 4 | 0 | 8 | 0 | 1 |
TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
static {...} |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
toString() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
writeReplace() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
TLE(String, String) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getLine1() |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getLine2() |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getBStar() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getBStar(AbsoluteDate) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
stateToTLE(SpacecraftState, TLE, TleGenerationAlgorithm) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getParametersDrivers() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getUtc() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getSatelliteNumber() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getClassification() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLaunchYear() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLaunchNumber() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLaunchPiece() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEphemerisType() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getElementNumber() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDate() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMeanMotion() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMeanMotionFirstDerivative() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMeanMotionSecondDerivative() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getE() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPerigeeArgument() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRaan() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMeanAnomaly() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRevolutionNumberAtEpoch() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |