| 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 |
| calculateBetaAngle(SpacecraftState, PVCoordinatesProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| BetaAngleDetector(AdaptableInterval, double, int, EventHandler, double, PVCoordinatesProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| create(AdaptableInterval, double, int, EventHandler) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| BetaAngleDetector(double, PVCoordinatesProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| g(SpacecraftState) | | 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 |
| lambda$new$0(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |