| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 7 of 139 | 94% | 0 of 2 | 100% | 1 | 11 | 1 | 32 | 1 | 10 |
| resetIntermediateState(SpacecraftState, boolean) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| EphemerisSegmentPropagator(EphemerisFile.EphemerisSegment) | | 100% | | 100% | 0 | 2 | 0 | 19 | 0 | 1 |
| getPVCoordinates(AbsoluteDate, Frame) | | 100% | n/a | 0 | 1 | 0 | 4 | 0 | 1 | |
| propagateOrbit(AbsoluteDate) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| resetInitialState(SpacecraftState) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getInitialState() | | 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 | |
| static {...} | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getMass(AbsoluteDate) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |