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

Figure 29

Satellites’ full ground track (a) and close-up (b) for a solution in Case with best maximum revisit time at 2 hours and 30 minutes and 44% area coverage. Purple line: ground track of sat and blue line: ground track of sat . Red star: area covered by sat .

(a)

(b)