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 26017.31546323 +.00000000 +00000-0 +23622-3 0 00009
2 20580 28.4678 30.2374 0001747 254.1050 105.9352 15.28565513 03
| Epoch (UTC): | 17 January 2026 07:34:16 |
| Eccentricity: | 0.0001747 |
| inclination: | 28.4678° |
| perigee height: | 479 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 30.2374° |
| argument of perigee: | 254.1050° |
| revolutions per day: | 15.28565513 |
| mean anomaly at epoch: | 105.9352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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