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 22285U 26044.42896329 +.00000000 +00000-0 +12641-3 0 00008
2 22285 71.0200 55.1959 0005297 319.7181 40.3549 14.15441969 07
| Epoch (UTC): | 13 February 2026 10:17:42 |
| Eccentricity: | 0.0005297 |
| inclination: | 71.0200° |
| perigee height: | 837 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 55.1959° |
| argument of perigee: | 319.7181° |
| revolutions per day: | 14.15441969 |
| mean anomaly at epoch: | 40.3549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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