| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 1 of 125 | 99% | 1 of 12 | 91% | 1 | 18 | 0 | 34 | 0 | 12 |
| hasManeuvers() | 87% | 50% | 1 | 2 | 0 | 1 | 0 | 1 | ||
| validate(double) | 100% | 100% | 0 | 6 | 0 | 15 | 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 | ||
| getNbManeuvers() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
| getManeuvers() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
| getStateVectorBlock() | 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 | ||
| getMass() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
| getUserDefinedBlock() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |