Initial Parameter Analysis about Resonant Orbits in Earth-Moon System

Table 4

Simulation results for 1:2 resonant orbits when the initial parameters cause closest distance r₁ .

Initial Phase	Eccentricity e	Simulation Results
10°	0.11	Steady ratio
20°	0.23	Steady ratio
30°	0.11	Steady ratio
40°	0.11	Steady ratio
50°	0.11	Steady ratio
60°	0.11	Steady ratio
70°	0.11	Steady ratio
	0.21	Steady ratio
80°	0.11	Steady ratio
	0.21	Steady ratio
90°	0.21	Steady ratio
	0.33	Steady ratio
100°	0.22	Steady ratio
	0.33	Steady ratio
110°	0.12	Steady ratio
	0.22	Steady ratio
120°	0.12	Steady ratio
	0.21	Steady ratio
	0.32	Steady ratio
130°	0.12	Steady ratio
	0.21	Steady ratio
140°	0.13	Steady ratio
	0.32	Steady ratio
150°	0.13	Steady ratio
	0.32	Steady ratio
160°	0.13	Steady ratio
	0.32	Steady ratio
170°	0.13	Steady ratio
	0.32	Steady ratio
180°	0.13	Steady ratio
	0.32	Steady ratio
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