| setObservedValue(double[]) |  | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
| modifyEstimatedValue(EstimationModifier, double[]) |  | 90% | | 75% | 1 | 3 | 1 | 8 | 0 | 1 |
| EstimatedMeasurementBase(ObservedMeasurement, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| setEstimatedValue(double[]) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| getTimeOffset() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getStates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParticipants() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getOriginalEstimatedValue() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEstimatedValue() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getObservedValue() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setStatus(EstimatedMeasurementBase.Status) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getObservedMeasurement() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getIteration() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCount() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAppliedEffects() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getStatus() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |