| updateAdditionalStates(SpacecraftState) |  | 100% | | 100% | 0 | 5 | 0 | 8 | 0 | 1 |
| getManagedAdditionalStates() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| addAdditionalStateProvider(AdditionalStateProvider) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| isAdditionalStateManaged(String) | | 100% | | 100% | 0 | 3 | 0 | 4 | 0 | 1 |
| AbstractPropagator() | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| propagate(AbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| setMasterMode(double, OrekitFixedStepHandler) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setSlaveMode() | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| setMasterMode(OrekitStepHandler) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| setEphemerisMode() | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| resetInitialState(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getPVCoordinates(AbsoluteDate, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setStartDate(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setAttitudeProvider(AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAdditionalStateProviders() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getStartDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAttitudeProvider() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getInitialState() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMode() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFixedStepSize() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getStepHandler() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |