Research Article
The Influence of Orbital Element Error on Satellite Coverage Calculation
Table 3
Data of orbital elements.
| Semimajor axis (km) | Eccentricity | True anomaly (°) | Inclination of orbit (°) | Argument of perigee (°) | Right ascension of ascending node (°) |
| 10,424 | 0.3 | 0 | 45 | 45 | 20 |
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