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 58206U 26145.37857542 +.00000000 +00000-0 +10057-4 0 00000
2 58206 43.0065 121.4957 0001424 257.8328 102.2364 15.27578235 09
| Epoch (UTC): | 25 May 2026 09:05:08 |
| Eccentricity: | 0.0001424 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.4957° |
| argument of perigee: | 257.8328° |
| revolutions per day: | 15.27578235 |
| mean anomaly at epoch: | 102.2364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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