| resetIntermediateState(FieldSpacecraftState, boolean, double, int) |  | 0% | | 0% | 2 | 2 | 7 | 7 | 1 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, CalculusFieldElement, double, CalculusFieldElement, double, double, double, double, double) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| computeMeanParameters(FieldCircularOrbit, CalculusFieldElement, double, int) |  | 95% | | 68% | 5 | 9 | 1 | 37 | 0 | 1 |
| resetInitialState(FieldSpacecraftState, PropagationType) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| resetIntermediateState(FieldSpacecraftState, boolean) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| resetInitialState(FieldSpacecraftState) | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| toCartesian(FieldAbsoluteDate, FieldUnivariateDerivative2[]) | | 100% | | n/a | 0 | 1 | 0 | 33 | 0 | 1 |
| meanToEccentric(FieldUnivariateDerivative2, FieldUnivariateDerivative2, FieldUnivariateDerivative2) | | 100% | | 75% | 1 | 3 | 0 | 17 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, double, CalculusFieldElement, double, double, double, double, double, PropagationType, double, int) | | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
| resetInitialState(FieldSpacecraftState, PropagationType, double, int) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| computeMeanOrbit(FieldOrbit, double, double, double, double, double, double, double, double, int) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| computeMeanOrbit(FieldOrbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, int) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| propagateOrbit(FieldAbsoluteDate, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, double, CalculusFieldElement, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, UnnormalizedSphericalHarmonicsProvider, PropagationType) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, UnnormalizedSphericalHarmonicsProvider) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, double, CalculusFieldElement, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, double, CalculusFieldElement, double, double, double, double, double, PropagationType) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, double, CalculusFieldElement, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider, PropagationType) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, UnnormalizedSphericalHarmonicsProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| computeMeanOrbit(FieldOrbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMass(FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |