Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
Total | 0 of 87 | 100% | 0 of 6 | 100% | 0 | 10 | 0 | 21 | 0 | 7 |
TrajectoryState(OrbitElementsType, AbsoluteDate, String[], int, List) | 100% | 100% | 0 | 2 | 0 | 7 | 0 | 1 | ||
TrajectoryState(OrbitElementsType, AbsoluteDate, double[]) | 100% | n/a | 0 | 1 | 0 | 5 | 0 | 1 | ||
getAvailableDerivatives() | 100% | 100% | 0 | 3 | 0 | 5 | 0 | 1 | ||
toCartesian(OneAxisEllipsoid, double) | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getElements() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getDate() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | ||
getType() | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |