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 26041.72948372 +.00000000 +00000-0 +26523-3 0 00004
2 20580 28.4663 223.8541 0001677 163.3807 196.6844 15.29047891 04
| Epoch (UTC): | 10 February 2026 17:30:27 |
| Eccentricity: | 0.0001677 |
| inclination: | 28.4663° |
| perigee height: | 478 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 223.8541° |
| argument of perigee: | 163.3807° |
| revolutions per day: | 15.29047891 |
| mean anomaly at epoch: | 196.6844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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