| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 0 of 189 | 100% | 0 of 0 | n/a | 0 | 7 | 0 | 31 | 0 | 7 |
| accelerationDerivatives(SpacecraftState, String) | | 100% | n/a | 0 | 1 | 0 | 7 | 0 | 1 | |
| addContribution(SpacecraftState, TimeDerivativesEquations) | | 100% | n/a | 0 | 1 | 0 | 7 | 0 | 1 | |
| accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D, FieldVector3D, FieldRotation, DerivativeStructure) | | 100% | n/a | 0 | 1 | 0 | 7 | 0 | 1 | |
| ThirdBodyAttraction(CelestialBody) | | 100% | n/a | 0 | 1 | 0 | 4 | 0 | 1 | |
| setParameter(String, double) | | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | |
| getParameter(String) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| getEventsDetectors() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |