View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 58210U 26145.32089851 +.00000000 +00000-0 +16008-4 0 00002
2 58210 43.0045 121.9308 0001243 275.2081 84.8629 15.27580102 01
| Epoch (UTC): | 25 May 2026 07:42:05 |
| Eccentricity: | 0.0001243 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.9308° |
| argument of perigee: | 275.2081° |
| revolutions per day: | 15.27580102 |
| mean anomaly at epoch: | 84.8629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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