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 26017.70719832 +.00000000 +00000-0 +24346-3 0 00003
2 20580 28.4679 27.5688 0001726 259.6743 100.3658 15.28570103 06
| Epoch (UTC): | 17 January 2026 16:58:21 |
| Eccentricity: | 0.0001726 |
| inclination: | 28.4679° |
| perigee height: | 479 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 27.5688° |
| argument of perigee: | 259.6743° |
| revolutions per day: | 15.28570103 |
| mean anomaly at epoch: | 100.3658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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