Research Article
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 |
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