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 26099.93133483 +.00000000 +00000-0 +21245-3 0 00005
2 20580 28.4726 186.7986 0002367 109.8379 250.2472 15.30004343 01
| Epoch (UTC): | 09 April 2026 22:21:07 |
| Eccentricity: | 0.0002367 |
| inclination: | 28.4726° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 186.7986° |
| argument of perigee: | 109.8379° |
| revolutions per day: | 15.30004343 |
| mean anomaly at epoch: | 250.2472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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