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 26073.11865009 +.00000000 +00000-0 +28927-3 0 00007
2 20580 28.4724 9.7854 0001781 169.7396 190.3236 15.29559924 00
| Epoch (UTC): | 14 March 2026 02:50:51 |
| Eccentricity: | 0.0001781 |
| inclination: | 28.4724° |
| perigee height: | 476 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 9.7854° |
| argument of perigee: | 169.7396° |
| revolutions per day: | 15.29559924 |
| mean anomaly at epoch: | 190.3236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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