| setParameters(double[]) |   | 73% | | 90% | 1 | 6 | 3 | 14 | 0 | 1 |
| AbstractPropagatorBuilder(Orbit, PositionAngle, double, boolean) | | 100% | | 100% | 0 | 3 | 0 | 16 | 0 | 1 |
| getSelectedNormalizedParameters() | | 100% | | 87% | 1 | 5 | 0 | 11 | 0 | 1 |
| getNbSelected() | | 100% | | 100% | 0 | 5 | 0 | 10 | 0 | 1 |
| createInitialOrbit() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| addSupportedParameter(ParameterDriver) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getOrbitType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPositionAngle() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getInitialOrbitDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getOrbitalParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPropagationParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |