| getHasManeuver() |   | 88% |   | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| generateKeplerianOrbit() |  | 100% |  | 100% | 0 | 2 | 0 | 4 | 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 |
| getMetaDataComment() |  | 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 |