Research Article
[Retracted] An Improved Orbit Model of Space Target Radar Based on Least Square Method and Its Program Implementation
Table 2
Satellite orbit elements.
| Epoch | Semimajor axis (km) | Eccentricity | Inclination | Argument of perigee | Ascension of ascending node | True anomaly |
| 2020-10-08 04:00:00 | 6678.14 | 0 | 28.5° | 0° | 0° | 0° |
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