| FieldGnssOrbitalElements(CalculusFieldElement, double, int, TimeScales, SatelliteSystem) |  | 0% | | n/a | 1 | 1 | 9 | 9 | 1 | 1 |
| FieldGnssOrbitalElements(Field, GNSSOrbitalElements) |  | 100% | | n/a | 0 | 1 | 0 | 23 | 0 | 1 |
| FieldGnssOrbitalElements(Function, FieldGnssOrbitalElements) |  | 100% | | n/a | 0 | 1 | 0 | 23 | 0 | 1 |
| getMeanMotion0() |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setGnssDate(GNSSDate) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getADot() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDeltaN0() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDeltaN0Dot() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setSma(CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setE(CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setI0(CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setOmega0(CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setPa(CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setM0(CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getDate() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMu() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 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 |