Research Article
The Influence of Orbital Element Error on Satellite Coverage Calculation
Table 8
Orbital element of each satellite.
| | Semi major axis (km) | Eccentricity | True anomaly (°) | Inclination of orbit (°) | Argument of perigee (°) | Right ascension of ascending node (°) |
| | 10,424 | 0.3 | 0 | 45 | 45 | 20 | | 10,424 | 0.3 | 0 | 45 | 45 | 40 | | 10,424 | 0.3 | 0 | 45 | 45 | 60 |
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