| directLocation(AbsoluteDate, Vector3D, Vector3D) |   | 97% | | 83% | 1 | 4 | 0 | 33 | 0 | 1 |
| isInRange(AbsoluteDate) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getAlgorithm() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| directLocation(String, double) | | 100% | | 100% | 0 | 5 | 0 | 37 | 0 | 1 |
| inverseLocation(String, GeodeticPoint, int, int) | | 100% | | 100% | 0 | 3 | 0 | 30 | 0 | 1 |
| Rugged(IntersectionAlgorithm, ExtendedEllipsoid, boolean, boolean, SpacecraftToObservedBody, Collection) | | 100% | | 100% | 0 | 2 | 0 | 12 | 0 | 1 |
| getPlaneCrossing(String, int, int) | | 100% | | 67% | 2 | 4 | 0 | 6 | 0 | 1 |
| dateLocation(String, GeodeticPoint, int, int) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getLineSensor(String) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| dateLocation(String, double, double, int, int) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| inverseLocation(String, double, double, int, int) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setPlaneCrossing(SensorMeanPlaneCrossing) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getScToInertial(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getInertialToBody(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getBodyToInertial(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLineSensors() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMinDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMaxDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| isLightTimeCorrected() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| isAberrationOfLightCorrected() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEllipsoid() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |