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 00022U 26149.51229005 +.00000000 +00000-0 +40679-3 0 00002
2 00022 50.2422 192.4406 0078740 48.6397 312.1301 15.28370097 03
| Epoch (UTC): | 29 May 2026 12:17:41 |
| Eccentricity: | 0.0078740 |
| inclination: | 50.2422° |
| perigee height: | 427 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 192.4406° |
| argument of perigee: | 48.6397° |
| revolutions per day: | 15.28370097 |
| mean anomaly at epoch: | 312.1301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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