| clone() |   | 86% | | 100% | 0 | 2 | 2 | 15 | 0 | 1 |
| setPositionAngleType(PositionAngleType) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| reset(Orbit) | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
| AbstractOrbitalStateFactory(OrbitParamsType, ParameterDriversList, Frame, PositionAngleType, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| getJacobianWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getNonKeplerianParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setDate(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setFrame(Frame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setMu(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getOrbitParamsType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getOrbitalParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMu() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |