| computePVCoordinates() |   | 97% | | 85% | 2 | 8 | 1 | 91 | 0 | 1 |
| FieldTLEPropagator(FieldTLE, AttitudeProvider, CalculusFieldElement, CalculusFieldElement[]) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| propagateOrbit(FieldAbsoluteDate, CalculusFieldElement[]) | | 91% | | 50% | 1 | 2 | 1 | 5 | 0 | 1 |
| getTLE() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getFrame() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getMU() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| initializeCommons(CalculusFieldElement[]) | | 100% | | 100% | 0 | 3 | 0 | 68 | 0 | 1 |
| selectExtrapolator(FieldTLE, AttitudeProvider, CalculusFieldElement, Frame, CalculusFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
| FieldTLEPropagator(FieldTLE, AttitudeProvider, CalculusFieldElement, Frame, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
| resetIntermediateState(FieldSpacecraftState, boolean) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| resetInitialState(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| initializeTle(FieldTLE) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| resetTle(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| selectExtrapolator(FieldTLE, Frame, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getPVCoordinates(FieldAbsoluteDate, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| selectExtrapolator(FieldTLE, AttitudeProvider, CalculusFieldElement, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getMass(FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| selectExtrapolator(FieldTLE, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |