Low-Thrust Out-of-Plane Orbital Station-Keeping Maneuvers for Satellites

Table 7

Data for transfer Maneuver 3.

Orbits	Initial	Final
Semimajor axis	8000.00	8000.00
Eccentricity	0.05	0.02
Inclination (degrees)	3.00	2.50
Ascending node (degrees)	0.00	Free
Argument of perigee (degrees)	0.00	Free
Mean anomaly (degrees)	0.00	Free