| FieldAbstractAnalyticalPropagator.FieldBoundedPropagatorView(FieldAbstractAnalyticalPropagator, FieldAbsoluteDate, FieldAbsoluteDate) |   | 63% | | 50% | 2 | 3 | 6 | 15 | 0 | 1 |
| resetInitialState(FieldSpacecraftState) | | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
| resetIntermediateState(FieldSpacecraftState, boolean) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| getFrame() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| propagateOrbit(FieldAbsoluteDate, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPVCoordinates(FieldAbsoluteDate, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMass(FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getInitialState() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMinDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMaxDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |