Orbit model parameters used in the EKF runs (only the terms different from those used in simulating photon timestamps are provided)
| Item | Value |
|---|---|
| Initial CR uncertainty (1 σ) | 1.3 * 20% |
| Earth gravity | 10 × 10 GGM02C |
| Lunar gravity | 10 × 10 GL0660B |
| qc | ∼2 × 10–20 (m/s2)2 |