Satellite Constellation Orbit Design Optimization with Combined Genetic Algorithm and Semianalytical Approach

Table 6

Orbit elements for a solution in Case with best maximum revisit time at 3 hours and 24 minutes and 32% area coverage.

Orbit element	Sat	Sat	Sat
(km)	6978	6978	6978
	0	0	0
(deg)	42	42	53
(deg)	154	154	136
(deg)	261	274	76
(deg)	0	0	0