| hashCode() |  | 0% | | n/a | 1 | 1 | 16 | 16 | 1 | 1 |
| TLE(String, String, TimeScale) |  | 100% | | 100% | 0 | 2 | 0 | 36 | 0 | 1 |
| buildLine1() | | 100% | | n/a | 0 | 1 | 0 | 33 | 0 | 1 |
| stateToTLE(SpacecraftState, TLE, TimeScale, Frame, double, int) | | 100% | | 92% | 1 | 8 | 0 | 43 | 0 | 1 |
| buildLine2() | | 100% | | n/a | 0 | 1 | 0 | 22 | 0 | 1 |
| equals(Object) | | 100% | | 57% | 17 | 21 | 0 | 9 | 0 | 1 |
| isFormatOK(String, String) | | 100% | | 81% | 3 | 9 | 0 | 15 | 0 | 1 |
| newTLE(KeplerianOrbit, TLE, TimeScale) | | 100% | | n/a | 0 | 1 | 0 | 21 | 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 |
| stateToTLE(SpacecraftState, TLE) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| convert(Orbit, Frame) | | 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 |
| stateToTLE(SpacecraftState, TLE, TimeScale, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getBStar() | | 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 |