| GNSSOrbitalElements(FieldGnssOrbitalElements) |  | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
| GNSSOrbitalElements(double, double, int, TimeScales, SatelliteSystem) |  | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| getMeanMotion0() |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setGnssDate(GNSSDate) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setSma(double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setE(double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setI0(double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setOmega0(double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setPa(double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setM0(double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getSma() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getE() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getI0() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getOmega0() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPa() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getM0() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDate() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMu() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSmaDriver() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEDriver() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getI0Driver() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getOmega0Driver() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPaDriver() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getM0Driver() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |