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 26049.56140836 +.00000000 +00000-0 +23228-3 0 00002
2 20580 28.4682 170.4553 0001159 251.4362 108.6108 15.29162623 02
| Epoch (UTC): | 18 February 2026 13:28:25 |
| Eccentricity: | 0.0001159 |
| inclination: | 28.4682° |
| perigee height: | 478 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 170.4553° |
| argument of perigee: | 251.4362° |
| revolutions per day: | 15.29162623 |
| mean anomaly at epoch: | 108.6108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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