| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 41 of 171 | 76% | 1 of 8 | 87% | 5 | 16 | 7 | 33 | 4 | 12 |
| basicPropagate(AbsoluteDate) | | 69% | | 50% | 1 | 2 | 3 | 10 | 0 | 1 |
| propagateOrbit(AbsoluteDate) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| getMass(AbsoluteDate) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| getInitialState() | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| resetIntermediateState(SpacecraftState, boolean) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| AggregateBoundedPropagator(Collection) | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
| defaultAttitude(Collection) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getPropagator(AbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| getPVCoordinates(AbsoluteDate, Frame) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getMinDate() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getMaxDate() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| resetInitialState(SpacecraftState) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |