| generateKeplerianOrbit() |   | 70% | | 50% | 1 | 2 | 1 | 4 | 0 | 1 |
| getMetaDataComment() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getHasManeuver() | | 88% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| getSatelliteCoordinates(String) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| generateCartesianOrbit() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| OPMFile() | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getSatelliteCoordinatesOPM() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPVCoordinates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| generateSpacecraftState() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getManeuver(int) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| addManeuver(OPMFile.Maneuver) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getCoordinateSystem() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setPosition(Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setVelocity(Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getNbManeuvers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getManeuvers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTimeSystem() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMetaData() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPosition() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getVelocity() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |