International Journal of Aerospace Engineering

Research Article

Low-Thrust Transfer Design of Low-Observable Geostationary Earth Orbit Satellite

Table 2

Orbit parameters.
Orbit parametersInitial orbitFinal orbit
GTOGEO
Semimajor axis (km)2473142164
Inclination (deg)28.50
Eccentricity 0.71940
Right ascension (deg)1.7104Free
Argument of perigee (deg)179.6Free
Mean anomaly (deg)2.9044Free