Table 1
Orbit propagation conditions

Propagator	Type	RK89	Orbit element	Semi major axis	1,850 km
	Accuracy	1.00E-13		Eccentricity	0.01
	Step size	1 sec		Inclination	90°
	Propagation span	20 days		Right ascension of ascending node	0°
Dynamic model	Lunar model	LP-165 165 ×165		Argument of perigee	120°
Coordinate system	Lunar center inertial			True anomaly	0°