| updateAdditionalStates(FieldSpacecraftState) |   | 78% | | 50% | 2 | 4 | 3 | 13 | 0 | 1 |
| stateChanged(FieldSpacecraftState) | | 90% | | 87% | 1 | 5 | 1 | 10 | 0 | 1 |
| propagate(FieldAbsoluteDate) | | 64% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
| initializePropagation() | | 100% | | 83% | 1 | 4 | 0 | 9 | 0 | 1 |
| updateUnmanagedStates(FieldSpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| getManagedAdditionalStates() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| addAdditionalStateProvider(FieldAdditionalStateProvider) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| FieldAbstractPropagator(Field) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| isAdditionalStateManaged(String) | | 100% | | 100% | 0 | 3 | 0 | 5 | 0 | 1 |
| initializeAdditionalStates(FieldAbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| resetInitialState(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getPVCoordinates(FieldAbsoluteDate, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setStartDate(FieldAbsoluteDate) | | 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 |
| getField() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getInitialState() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMultiplexer() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |