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 20580U 26134.69359843 +.00000000 +00000-0 +14011-3 0 00001
2 20580 28.4753 309.4175 0002090 119.7913 240.2891 15.30378185 04
| Epoch (UTC): | 14 May 2026 16:38:46 |
| Eccentricity: | 0.0002090 |
| inclination: | 28.4753° |
| perigee height: | 473 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 309.4175° |
| argument of perigee: | 119.7913° |
| revolutions per day: | 15.30378185 |
| mean anomaly at epoch: | 240.2891° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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