Research Article
Indirect Optimization of Satellite Deployment into a Highly Elliptic Orbit
Table 2
Time length and angular length of burn arcs (J2 only).
| | N | | | P1 | A1 | P2 | A2 | A3 |
| | 2.5 | , h | 2.66 | 76.50 | 3.77 | — | — | | , deg | 250.15 | 58.73 | 154.38 | — | | | 3.5 | , h | 0.45 | 35.55 | — | 34.79 | — | | , deg | 121.27 | 18.40 | — | 23.15 | — | | 4.5 | , h | 0.65 | 23.28 | — | 22.95 | 22.63 | | , deg | 152.88 | 10.90 | | 12.97 | 15.02 |
| | N | | | P1 | A1 | P2 | A2 | A3 |
| | 2.5 | , h | 0.09 | 8.50 | — | — | — | | , deg | 28.50 | 4.67 | — | — | — | | 3.5 | , h | 0.09 | 4.29 | — | 4.20 | — | | , deg | 28.97 | 2.04 | — | 2.61 | — | | 4.5 | , h | 0.09 | 2.87 | — | 2.83 | 2.79 | | , deg | 29.05 | 1.30 | — | 1.55 | 1.80 |
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