Parameters of force models and integrator used in the generation of the assumed true satellite orbits
| Item | Value | Item | Value | |
|---|---|---|---|---|
| Planetary ephemeris | JPL DE405 (Standish, 1998) | SRP | Area-mass-ratio | Planetary ephemeris |
| Reference frame | J2000 | CR | Reference frame | |
| Earth gravity | 20 × 20 GGM02C (Tapley et al, 2005) | Integ | Runge-Kutta-7(8) | Earth gravity |
| Lunar gravity | 20 × 20 GL0660B (Konopliv et al., 2013) | Relative error | Lunar gravity | |
| Sun gravity | Point mass | Max step size | Sun gravity |