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 26022.46769159 +.00000000 +00000-0 +14497-3 0 00000
2 20855 98.8149 6.8814 0023766 184.8141 286.4913 14.09150251 00
| Epoch (UTC): | 22 January 2026 11:13:28 |
| Eccentricity: | 0.0023766 |
| inclination: | 98.8149° |
| perigee height: | 845 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 6.8814° |
| argument of perigee: | 184.8141° |
| revolutions per day: | 14.09150251 |
| mean anomaly at epoch: | 286.4913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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