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

Table 3

Initial orbit parameters when the two satellites are 100 m apart.

Parameter name	Satellite 1	Satellite 2
Semimajor axis (km)	6878.14	6878.14
Eccentricity	0	0
Inclination (°)	97.4065	97.4065
RAAN (°)	0	0
Argument of perigee (°)	0	0
True anomaly (°)	0	0.000833015