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 26018.68652911 +.00000000 +00000-0 +24968-3 0 00005
2 20580 28.4679 20.8973 0001680 272.2114 87.8289 15.28583946 09
| Epoch (UTC): | 18 January 2026 16:28:36 |
| Eccentricity: | 0.0001680 |
| inclination: | 28.4679° |
| perigee height: | 479 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 20.8973° |
| argument of perigee: | 272.2114° |
| revolutions per day: | 15.28583946 |
| mean anomaly at epoch: | 87.8289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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