| g(FieldSpacecraftState) |   | 53% | | 50% | 2 | 3 | 3 | 10 | 0 | 1 |
| withRefraction(AtmosphericRefractionModel) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| FieldElevationDetector(Field, TopocentricFrame) | | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
| withElevationMask(ElevationMask) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| create(FieldAdaptableInterval, CalculusFieldElement, int, FieldEventHandler) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getElevationMask() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getRefractionModel() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| lambda$new$0(FieldSpacecraftState) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| FieldElevationDetector(FieldAdaptableInterval, CalculusFieldElement, int, FieldEventHandler, double, ElevationMask, AtmosphericRefractionModel, TopocentricFrame) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| withConstantElevation(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| FieldElevationDetector(CalculusFieldElement, CalculusFieldElement, TopocentricFrame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getMinElevation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTopocentricFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$new$1(CalculusFieldElement, FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |