| toField(FieldKeplerianOrbit, CalculusFieldElement[], DoubleFunction) |  | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
| BeidouLegacyNavigationMessage(boolean, TimeScales, String, int, GNSSDate, KeplerianOrbit, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, GNSSDate, GNSSDate, int, int, int, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| BeidouLegacyNavigationMessage(FieldBeidouLegacyNavigationMessage) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| baseFactory(Frame, Frame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| isD2() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAODC() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAODE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTGD1() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTGD2() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSvAccuracy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSatH1() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |