| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 0 of 165 | 100% | 0 of 0 | n/a | 0 | 11 | 0 | 34 | 0 | 11 |
| EphemerisSegmentPropagator(EphemerisFile.EphemerisSegment, AttitudeProvider) | | 100% | n/a | 0 | 1 | 0 | 17 | 0 | 1 | |
| interpolate(AbsoluteDate) | | 100% | n/a | 0 | 1 | 0 | 5 | 0 | 1 | |
| propagateOrbit(AbsoluteDate) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| getPosition(AbsoluteDate, Frame) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| getPVCoordinates(AbsoluteDate, Frame) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| resetIntermediateState(SpacecraftState, boolean) | | 100% | n/a | 0 | 1 | 0 | 1 | 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 | |
| getMass(AbsoluteDate) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |