| calculateBetaAngle(SpacecraftState, PVCoordinatesProvider, Frame) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| BetaAngleDetector(EventDetectionSettings, EventHandler, double, PVCoordinatesProvider, Frame) |  | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| withCelestialProvider(PVCoordinatesProvider) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| withBetaThreshold(double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| withInertialFrame(Frame) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| g(SpacecraftState) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| create(EventDetectionSettings, EventHandler) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| BetaAngleDetector(double, PVCoordinatesProvider, Frame) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| BetaAngleDetector(double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| calculateBetaAngle(SpacecraftState, PVCoordinatesProvider) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCelestialBodyProvider() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getInertialFrame() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getBetaAngleThreshold() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |