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 26044.79705700 +.00000000 +00000-0 +24111-3 0 00001
2 20580 28.4663 202.9407 0001437 193.7591 166.2965 15.29093803 05
| Epoch (UTC): | 13 February 2026 19:07:45 |
| Eccentricity: | 0.0001437 |
| inclination: | 28.4663° |
| perigee height: | 478 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 202.9407° |
| argument of perigee: | 193.7591° |
| revolutions per day: | 15.29093803 |
| mean anomaly at epoch: | 166.2965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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