| createFromDrivers() |  | 100% | | n/a | 0 | 1 | 0 | 21 | 0 | 1 |
| createOrbitalParametersDrivers(TLE) | | 100% | | n/a | 0 | 1 | 0 | 14 | 0 | 1 |
| toGradient(TLE) | | 100% | | n/a | 0 | 1 | 0 | 16 | 0 | 1 |
| getJacobianWrtParameters(TLE) | | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
| toArray(Orbit) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| TleGenerationAlgorithm(TLE, Frame, OsculatingToMeanConverter) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| clone() | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| generate(SpacecraftState, TLE) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| generate(FieldSpacecraftState, FieldTLE) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getBStar() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getJacobianWrtParameters() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTemplateTLE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getConverter() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getNonKeplerianParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |