| getMeanElementRate(FieldSpacecraftState, FieldAuxiliaryElements, CalculusFieldElement[]) |  | 100% | | n/a | 0 | 1 | 0 | 19 | 0 | 1 |
| getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) | | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
| DSSTJ2SquaredClosedForm(J2SquaredModel, UnnormalizedSphericalHarmonicsProvider) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| initializeShortPeriodTerms(FieldAuxiliaryElements, PropagationType, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| updateShortPeriodTerms(double[], SpacecraftState[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| updateShortPeriodTerms(CalculusFieldElement[], FieldSpacecraftState[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| registerAttitudeProvider(AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |