| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 26 of 1,265 | 98% | 2 of 20 | 90% | 3 | 22 | 4 | 166 | 1 | 12 |
| computePVCoordinates() | | 98% | | 86% | 2 | 8 | 1 | 85 | 0 | 1 |
| resetInitialState(SpacecraftState) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| propagateOrbit(AbsoluteDate) | | 65% | n/a | 0 | 1 | 2 | 3 | 0 | 1 | |
| initializeCommons() | | 100% | | 100% | 0 | 3 | 0 | 51 | 0 | 1 |
| selectExtrapolator(TLE, AttitudeProvider, double) | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| TLEPropagator(TLE, AttitudeProvider, double) | | 100% | n/a | 0 | 1 | 0 | 9 | 0 | 1 | |
| getPVCoordinates(AbsoluteDate) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| selectExtrapolator(TLE) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getMass(AbsoluteDate) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
| getTLE() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
| getFrame() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
| getMU() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |