The Relative Perturbation Analysis of Satellite Formation under the Requirement of Relative Position Maintenance with Millimeter-Level Accuracy

Table 2

Initial orbit parameters when the two satellites are 200 m apart.

Parameter name	Satellite 1	Satellite 2
Semimajor axis (km)	6878.14	6878.14
Eccentricity
Inclination (°)	97.4065	97.4065
RAAN (°)
Argument of perigee (°)	0	0
True anomaly (°)	0	0.00166603