| FieldEcksteinHechlerPropagator(FieldOrbit, RealFieldElement, double, double, double, double, double, double, double) |  | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| computeMeanParameters(FieldCircularOrbit, RealFieldElement) |  | 95% | | 62% | 6 | 9 | 1 | 39 | 0 | 1 |
| resetIntermediateState(FieldSpacecraftState, boolean) | | 76% | | 50% | 1 | 2 | 1 | 6 | 0 | 1 |
| toCartesian(FieldAbsoluteDate, FieldDerivativeStructure[]) | | 100% | | n/a | 0 | 1 | 0 | 33 | 0 | 1 |
| meanToEccentric(FieldDerivativeStructure, FieldDerivativeStructure, FieldDerivativeStructure) | | 100% | | 75% | 1 | 3 | 0 | 17 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, double, double, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 14 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| resetInitialState(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| propagateOrbit(FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, double, double, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, double, double, double, double, double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, UnnormalizedSphericalHarmonicsProvider) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| normalizeAngle(RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, RealFieldElement, UnnormalizedSphericalHarmonicsProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, UnnormalizedSphericalHarmonicsProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getMass(FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |