| StateMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) |  | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| mapDoubleToDate(double, AbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| mapArrayToState(double, double[], double[], PropagationType) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| mapDoubleToDate(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| mapDateToDouble(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setAttitudeProvider(AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getReferenceDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getOrbitType() | | 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 |
| getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAttitudeProvider() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |