| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 68 of 144 | 53% | 6 of 12 | 50% | 9 | 16 | 18 | 35 | 6 | 10 |
| basicPropagate(AbsoluteDate) | | 66% | | 60% | 2 | 6 | 8 | 18 | 0 | 1 |
| resetIntermediateState(SpacecraftState, boolean) | | 0% | | 0% | 2 | 2 | 4 | 4 | 1 | 1 |
| resetInitialState(SpacecraftState) | | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 1 | |
| propagateOrbit(AbsoluteDate) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| getMass(AbsoluteDate) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| getEffects() | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| getPropagator() | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| AdapterPropagator(Propagator) | | 100% | n/a | 0 | 1 | 0 | 4 | 0 | 1 | |
| addEffect(AdapterPropagator.DifferentialEffect) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| getInitialState() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |