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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2017
/
Article
/
Tab 7
/
Research Article
Satellite Constellation Orbit Design Optimization with Combined Genetic Algorithm and Semianalytical Approach
Table 7
Orbit elements for a solution in Case
(best 74% area coverage and 9 hours of ART).
Orbit element
Sat
Sat
Sat
(km)
6936
6936
6884
0
0
0
(deg)
38
38
75
(deg)
199
199
9
(deg)
251
159
158
(deg)
335
163
202