Research Article
Low-Thrust Out-of-Plane Orbital Station-Keeping Maneuvers for Satellites
Table 1
Data for Maneuver 1.
| | Orbits | Initial | Final |
| | Semimajor axis | 7060.00 | 7090.00 | | Eccentricity | 0.03 | 0.01 | | Inclination (degrees) | 1.00 | 0.50 | | Ascending node (degrees) | 0.00 | Free | | Argument of perigee (degrees) | 0.00 | Free | | Mean anomaly (degrees) | 0.00 | Free |
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