| withRefraction(AtmosphericRefractionModel) |   | 55% | | 50% | 1 | 2 | 2 | 5 | 0 | 1 |
| create(FieldEventDetectionSettings, FieldEventHandler) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getElevationMask() | | 81% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
| getMinElevation() | | 81% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
| FieldElevationDetector(CalculusFieldElement, CalculusFieldElement, TopocentricFrame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldElevationDetector(Field, TopocentricFrame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| withConstantElevation(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| withElevationMask(ElevationMask) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| toEventDetector(EventHandler) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldElevationDetector(FieldEventDetectionSettings, FieldEventHandler, AbstractElevationCrossingFunction) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getRefractionModel() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| g(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |