| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 14 of 85 | 84% | 0 of 2 | 100% | 2 | 9 | 4 | 22 | 2 | 8 |
| KeplerianPropagator(Orbit, double) | | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 1 | |
| KeplerianPropagator(Orbit, AttitudeProvider, double) | | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 1 | |
| KeplerianPropagator(Orbit, AttitudeProvider, double, double) | | 100% | n/a | 0 | 1 | 0 | 6 | 0 | 1 | |
| propagateOrbit(AbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| KeplerianPropagator(Orbit) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| KeplerianPropagator(Orbit, AttitudeProvider) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| resetInitialState(SpacecraftState) | | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | |
| getMass(AbsoluteDate) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |