| hasManeuvers() |   | 87% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| validate(double) | | 100% | | 100% | 0 | 5 | 0 | 14 | 0 | 1 |
| OpmData(StateVector, KeplerianElements, SpacecraftParameters, CartesianCovariance, List, UserDefined, double) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| getManeuver(int) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getKeplerianElementsBlock() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSpacecraftParametersBlock() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCovarianceBlock() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getNbManeuvers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getManeuvers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getUserDefinedBlock() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$validate$0(double, Maneuver) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getStateVectorBlock() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMass() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |