Research Article
Influence of Steering Angle Profiles on the Orbit Transfer Trajectory
Table 5
Boundary conditions for the initial and final orbits (Example 2).
| | Initial orbit | Target orbit |
| Semimajor axis | −7341.7191 km | 3869.5815 km | Eccentricity | 1.2571∼1.2843 | 0.4993 | Argument of the periapsis | 0 degree | Free | Periapsis altitude | 150∼350 km | 200 km | Orbital period | — | 6.0 hour |
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