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 20855U 26106.69037625 +.00000000 +00000-0 +75997-4 0 00007
2 20855 98.8269 89.3452 0023139 311.6396 221.7783 14.09168525 03
| Epoch (UTC): | 16 April 2026 16:34:08 |
| Eccentricity: | 0.0023139 |
| inclination: | 98.8269° |
| perigee height: | 845 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 89.3452° |
| argument of perigee: | 311.6396° |
| revolutions per day: | 14.09168525 |
| mean anomaly at epoch: | 221.7783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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