| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 48 of 124 | 61% | 2 of 8 | 75% | 7 | 14 | 12 | 29 | 6 | 10 |
| resetIntermediateState(SpacecraftState, boolean) | 0% | 0% | 2 | 2 | 4 | 4 | 1 | 1 | ||
| basicPropagate(AbsoluteDate) | 88% | 100% | 0 | 4 | 2 | 12 | 0 | 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 |