| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 0 of 156 | 100% | 0 of 0 | n/a | 0 | 8 | 0 | 33 | 0 | 8 |
| acceleration(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | n/a | 0 | 1 | 0 | 10 | 0 | 1 | |
| acceleration(SpacecraftState, double[]) | | 100% | n/a | 0 | 1 | 0 | 10 | 0 | 1 | |
| DeSitterRelativity(CelestialBody, CelestialBody) | | 100% | n/a | 0 | 1 | 0 | 6 | 0 | 1 | |
| DeSitterRelativity() | | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | |
| static {...} | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getParametersDrivers() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getSun() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getEarth() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |