Table 1
Initial orbit element for reference orbit generation

Value	Parameters
Epoch	2023 1/1 00:00:00 (UTC)
Coordinate frame	Moon TOD
Apoapsis altitude	128 km
Periapsis altitude	72 km
Inclination	89.4 deg
Right ascension of ascending node	316.8 deg
Argument of periapsis	165.5 deg
True anomaly	0 deg

TOD, true of date.