| computeLocalParametersWith(SpacecraftState[], ObservableSatellite, AbsoluteDate, boolean, List) |   | 98% | | 50% | 1 | 2 | 0 | 21 | 0 | 1 |
| computeLocalParametersWithout(SpacecraftState[], ObservableSatellite, AbsoluteDate, boolean) | | 97% | | 50% | 1 | 2 | 0 | 15 | 0 | 1 |
| computeRemoteParametersWith(SpacecraftState[], ObservableSatellite, AbsoluteDate, boolean, List) | | 100% | | n/a | 0 | 1 | 0 | 25 | 0 | 1 |
| computeRemoteParametersWithout(SpacecraftState[], ObservableSatellite, AbsoluteDate, boolean) | | 100% | | n/a | 0 | 1 | 0 | 16 | 0 | 1 |
| getParamaterIndices(SpacecraftState[], List) | | 100% | | 100% | 0 | 4 | 0 | 8 | 0 | 1 |
| getOffsetToInertial(Frame, AbsoluteDate, int, Map) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getPosition(AbsoluteDate, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPVCoordinates(AbsoluteDate, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |