Research Article
Randomly Weighted CKF for Multisensor Integrated Systems
Table 2
Rocket orbital parameters.
| Parameters | Values |
| Semimajor axis | 6976.023529 km | Orbital eccentricity | 0.001159 | Orbital inclination | 28.948° | RAAN | 340.61° | Argument of periapsis | 342.274° | True anomaly | 230.52° | Orbit time period | 49866 s |
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