Influence of Three-Body Gravitational Perturbation for Drag-Free Spacecraft

Table 1

The parameters of the sun orbit and Earth orbit [25].

Orbit parameters	Sun orbit	Earth orbit
Semimajor axis (km)	149597870.700	99995.5723
Eccentricity	0.009648	0.00043
Orbit inclination (°)	0.9529	74.5362
RAAN (°)	348.16	211.6003
Argument of perigee (°)	270	346.5528
True anomaly (°)	180	61.3296