| interpolate(AbstractFieldTimeInterpolator.InterpolationData) |   | 94% | | 69% | 8 | 14 | 4 | 55 | 0 | 1 |
| interpolateAttitude(FieldAbsoluteDate, List, FieldPVCoordinatesProvider) | | 43% | | 50% | 1 | 2 | 2 | 4 | 0 | 1 |
| interpolate(FieldAbsoluteDate, Collection) | | 94% | | 66% | 2 | 4 | 0 | 7 | 0 | 1 |
| interpolateAdditionalState(FieldAbsoluteDate, Map) | | 100% | | 100% | 0 | 4 | 0 | 17 | 0 | 1 |
| FieldSpacecraftStateInterpolator(int, double, Frame, Frame, CartesianDerivativesFilter, AngularDerivativesFilter) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getSubInterpolators() | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
| FieldSpacecraftStateInterpolator(Frame, FieldTimeInterpolator, FieldTimeInterpolator, FieldTimeInterpolator, FieldTimeInterpolator, FieldTimeInterpolator) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| createAdditionalStateSample(List) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| lambda$interpolateAdditionalState$0(List, int, Pair) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| checkAtLeastOneInterpolator(FieldTimeInterpolator, FieldTimeInterpolator) | | 100% | | 75% | 1 | 3 | 0 | 3 | 0 | 1 |
| FieldSpacecraftStateInterpolator(int, double, Frame, Frame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldSpacecraftStateInterpolator(int, Frame, Frame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getNbInterpolationPoints() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| FieldSpacecraftStateInterpolator(int, Frame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldSpacecraftStateInterpolator(Frame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getOrbitInterpolator() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAbsPVAInterpolator() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getMassInterpolator() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAttitudeInterpolator() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAdditionalStateInterpolator() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getOutputFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |