| baseFactory(Frame, Frame) |  | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| toField(FieldKeplerianOrbit, CalculusFieldElement[], DoubleFunction) |  | 100% | | n/a | 0 | 1 | 0 | 18 | 0 | 1 |
| BeidouCivilianNavigationMessage(BeidouCivilianType, TimeScales, int, GNSSDate, KeplerianOrbit, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, GNSSDate, GNSSDate, int, int, double, double, double, int, int, int, int, int, int, int, double, double, double, BeidouSatelliteType) | | 100% | | n/a | 0 | 1 | 0 | 20 | 0 | 1 |
| BeidouCivilianNavigationMessage(FieldBeidouCivilianNavigationMessage) | | 100% | | n/a | 0 | 1 | 0 | 19 | 0 | 1 |
| getBeidouType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getIODE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getIODC() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getIscB1CD() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getIscB2AD() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getIscB1CP() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSisaiOe() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSisaiOcb() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSisaiOc1() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSisaiOc2() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSismai() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getHealth() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getIntegrityFlags() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTgdB1Cp() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTgdB2ap() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTgdB2bI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSatelliteType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| isCivilianMessage() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |