| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 0 of 59 | 100% | 0 of 4 | 100% | 0 | 9 | 0 | 9 | 0 | 7 |
| getAttitudeRotation(SpacecraftState, double[]) | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getAttitudeRotation(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getAttitudeRotation(FieldPVCoordinatesProvider, FieldAbsoluteDate, Frame) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getFieldEventDetectors(Field) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getEventDetectors() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getParametersDrivers() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |