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 26040.47141530 +.00000000 +00000-0 +40952-5 0 00004
2 22285 71.0200 63.5052 0005163 323.4452 36.6318 14.15441002 09
| Epoch (UTC): | 09 February 2026 11:18:50 |
| Eccentricity: | 0.0005163 |
| inclination: | 71.0200° |
| perigee height: | 837 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 63.5052° |
| argument of perigee: | 323.4452° |
| revolutions per day: | 14.15441002 |
| mean anomaly at epoch: | 36.6318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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