| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 22 of 299 | 93% | 2 of 30 | 93% | 3 | 28 | 4 | 64 | 1 | 13 |
| setParameters(double[]) | | 73% | | 90% | 1 | 6 | 3 | 14 | 0 | 1 |
| getInitialOrbitDate() | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| AbstractPropagatorBuilder(Orbit, PositionAngle, double) | | 100% | | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
| getSelectedNormalizedParameters() | | 100% | | 88% | 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 | |
| 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 |