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

Table 5

Orbit elements for a solution in Case (72% area coverage and 1 hour and 19 minutes of ART).

Orbit element	Sat	Sat	Sat
(km)	6978	6978	6978
	0	0	0
(deg)	42	42	44
(deg)	90	90	131
(deg)	324	326	284
(deg)	0	0	0