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 22286U 26020.26252787 +.00000000 +00000-0 +35910-3 0 00003
2 22286 82.5188 283.6757 0019577 102.9973 257.3437 14.96935338 04
| Epoch (UTC): | 20 January 2026 06:18:02 |
| Eccentricity: | 0.0019577 |
| inclination: | 82.5188° |
| perigee height: | 563 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 283.6757° |
| argument of perigee: | 102.9973° |
| revolutions per day: | 14.96935338 |
| mean anomaly at epoch: | 257.3437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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