Research on Formation of Microsatellite Communication with Genetic Algorithm

Table 1

Orbit elements of formation flying satellites including several satellites.

Orbital element	Host satellite	Difference of orbit element 1	Difference of orbit element 2
𝑎 (Km)	7555	−3.1816𝐸−7	3.2870𝐸−7
𝑒	0.0001	−4.5999𝐸−5	6.0762𝐸−5
𝑖 (deg)	48	1.76130𝐸−6	−1.7613𝐸−6
𝜔 (deg)	30	3.7782𝐸+1	−1.1876𝐸+1
Ω (deg)	30	−8.8383𝐸−3	8.8383𝐸−3
𝑀 (deg)	0	−3.7776𝐸+1	1.1870𝐸+1