| getOffsetDerivatives(int, int, int, int) |   | 77% | | 50% | 2 | 3 | 2 | 33 | 0 | 1 |
| GroundStation(TopocentricFrame) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| combine(Vector3D, FieldVector3D, FieldVector3D) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| getOffsetFrame() | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
| downlinkTimeOfFlight(SpacecraftState, AbsoluteDate) | | 100% | | 75% | 1 | 3 | 0 | 11 | 0 | 1 |
| uplinkTimeOfFlight(SpacecraftState) | | 100% | | 75% | 1 | 3 | 0 | 11 | 0 | 1 |
| centerOfCurvature(Vector3D, Vector3D) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEastOffsetDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getNorthOffsetDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getZenithOffsetDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getBaseFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |