| acceleration(FieldSpacecraftState, CalculusFieldElement[]) |  | 100% | | n/a | 0 | 1 | 0 | 17 | 0 | 1 |
| acceleration(SpacecraftState, double[]) | | 100% | | n/a | 0 | 1 | 0 | 17 | 0 | 1 |
| J2OnlyPerturbation(UnnormalizedSphericalHarmonicsProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| J2OnlyPerturbation(double, double, double, Frame) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| J2OnlyPerturbation(double, double, TimeScalarFunction, Frame) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| getJ2(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getJ2(FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMu() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getrEq() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| dependsOnPositionOnly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |