Initial Parameter Analysis about Resonant Orbits in Earth-Moon System

Table 5

Simulation results for 2:1 resonant orbits when the initial parameters can cause the closest distance to lie within the Moon’s sphere of influence.

Initial Phase	Eccentricity	Simulation Results
50°	0.85	Resonance transition
	0.9	Flyby
60°	0.75	Resonance transition
	0.83	Resonance transition
	0.88	Flyby
70°	0.61	Resonance transition
	0.7	Resonance transition
	0.78	Flyby
	0.87	Resonance transition
80°	0.45	Resonance transition
	0.57	Resonance transition
	0.66	Flyby
	0.79	Resonance transition
90°	0.89	Resonance transition
	0.33	Resonance transition
	0.43	Resonance transition
	0.58	Resonance transition
	0.7	Resonance transition