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 22566U 26020.93135797 +.00000000 +00000-0 +14898-3 0 00001
2 22566 71.0087 315.4900 0009031 24.7752 335.3803 14.15294696 00
| Epoch (UTC): | 20 January 2026 22:21:09 |
| Eccentricity: | 0.0009031 |
| inclination: | 71.0087° |
| perigee height: | 835 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 315.4900° |
| argument of perigee: | 24.7752° |
| revolutions per day: | 14.15294696 |
| mean anomaly at epoch: | 335.3803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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