| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 6 of 45 | 86% | 0 of 0 | n/a | 1 | 9 | 2 | 11 | 1 | 9 |
| init(FieldSpacecraftState, FieldAbsoluteDate) | | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 1 | |
| init(SpacecraftState, AbsoluteDate) | | 100% | n/a | 0 | 1 | 0 | 2 | 0 | 1 | |
| acceleration(SpacecraftState, double[]) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| acceleration(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getFieldEventDetectors(Field) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| dependsOnPositionOnly() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| dependsOnAttitudeRate() | | 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 |