| GroundStation(TopocentricFrame, EOPHistory, StationDisplacement[]) |   | 95% | | 75% | 1 | 3 | 1 | 21 | 0 | 1 |
| getOffsetGeodeticPoint(AbsoluteDate) | | 85% | | 50% | 1 | 2 | 1 | 9 | 0 | 1 |
| getEstimatedUT1() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getOffsetToInertial(Frame, FieldAbsoluteDate, DSFactory, Map) | | 100% | | n/a | 0 | 1 | 0 | 18 | 0 | 1 |
| getOffsetToInertial(Frame, FieldAbsoluteDate, int, Map) | | 100% | | n/a | 0 | 1 | 0 | 18 | 0 | 1 |
| getOffsetToInertial(Frame, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 15 | 0 | 1 |
| computeDisplacement(AbsoluteDate, Vector3D) | | 100% | | 100% | 0 | 3 | 0 | 6 | 0 | 1 |
| getOffsetToInertial(Frame, AbsoluteDate, DSFactory, Map) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getOffsetToInertial(Frame, AbsoluteDate, int, Map) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| GroundStation(TopocentricFrame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getDisplacements() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPrimeMeridianOffsetDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPrimeMeridianDriftDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPolarOffsetXDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPolarDriftXDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPolarOffsetYDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPolarDriftYDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getClockOffsetDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getClockDriftDriver() | | 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 |
| getEstimatedEarthFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |