toString() | | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
buildLine1() | | 95% | | 50% | 1 | 2 | 2 | 36 | 0 | 1 |
equals(Object) | | 98% | | 55% | 18 | 21 | 1 | 17 | 0 | 1 |
FieldTLE(Field, String, String, TimeScale) | | 100% | | 100% | 0 | 2 | 0 | 38 | 0 | 1 |
buildLine2() | | 100% | | n/a | 0 | 1 | 0 | 22 | 0 | 1 |
hashCode() | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
formatExponentMarkerFree(String, double, int, char, int, boolean) | | 100% | | 100% | 0 | 6 | 0 | 12 | 0 | 1 |
FieldTLE(int, char, int, int, String, int, int, FieldAbsoluteDate, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, int, double, TimeScale) | | 100% | | n/a | 0 | 1 | 0 | 24 | 0 | 1 |
toTLE() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
checksum(CharSequence) | | 100% | | 100% | 0 | 4 | 0 | 8 | 0 | 1 |
FieldTLE(int, char, int, int, String, int, int, FieldAbsoluteDate, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, int, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
static {...} | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldTLE(Field, 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 |
stateToTLE(FieldSpacecraftState, FieldTLE, TleGenerationAlgorithm) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
isFormatOK(String, String) | | 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 |