| getEclipseAngles(Vector3D, Frame, AbsoluteDate) |   | 79% | | 50% | 1 | 2 | 1 | 9 | 0 | 1 |
| getLightingRatio(Vector3D, Frame, AbsoluteDate) | | 100% | | 100% | 0 | 3 | 0 | 23 | 0 | 1 |
| addContribution(SpacecraftState, TimeDerivativesEquations) | | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
| accelerationDerivatives(SpacecraftState, String) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D, FieldVector3D, FieldRotation, DerivativeStructure) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| SolarRadiationPressure(double, double, PVCoordinatesProvider, double, RadiationSensitive) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| getEventsDetectors() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| SolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |