| setInitialState(SpacecraftState) |  | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| setSatelliteRevolution(int) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| initialIsOsculating() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| removeForceModels() | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| getSatelliteRevolution() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) |  | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| beforeIntegration(SpacecraftState, AbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| DSSTPropagator(AbstractIntegrator) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| setInitialState(SpacecraftState, boolean) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| resetInitialState(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getMainStateEquations(AbstractIntegrator) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| addForceModel(DSSTForceModel) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| tolerances(double, Orbit) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |