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

Table 8

Orbit elements for a solution in Case with best maximum revisit time at 2 hours and 30 minutes and 44% area coverage.

Orbit element	Sat	Sat	Sat
(km)	6938	6938	6871
	0	0	0
(deg)	39	39	78
(deg)	198	198	118
(deg)	251	245	291
(deg)	333	342	23