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

Table 1

Parameters variation for constellation visibility GA simulation.

Variation parameter	Value
Inclination	0–90 degrees
Semimajor axis	6538 to 6978 km, orbit height 160 to 600 km (LEO)
Longitude of ascending node	0–360 degrees
Argument of latitude	0–360 degrees