| setParameters(double[]) |   | 73% | | 90% | 1 | 6 | 3 | 14 | 0 | 1 |
| clone() | | 33% | | n/a | 0 | 1 | 2 | 3 | 0 | 1 |
| AbstractPropagatorBuilder(OrbitalStateFactory, boolean, AttitudeProvider, double) | | 100% | | 100% | 0 | 3 | 0 | 18 | 0 | 1 |
| getSelectedNormalizedParameters() | | 100% | | 100% | 0 | 5 | 0 | 11 | 0 | 1 |
| getNbValuesForSelected() | | 100% | | 100% | 0 | 5 | 0 | 10 | 0 | 1 |
| deselectDynamicParameters() | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| addPropagationParameters(List) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| AbstractPropagatorBuilder(OrbitalStateFactory, boolean) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| AbstractPropagatorBuilder(OrbitalStateFactory, boolean, AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| addAdditionalDerivativesProvider(AdditionalDerivativesProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| buildPropagator() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| resetOrbit(Orbit) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setMass(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setAttitudeProvider(AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getMass() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getOrbitalStateFactory() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPropagationParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAttitudeProvider() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAdditionalDerivativesProviders() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |