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 26111.39817700 +.00000000 +00000-0 -12068-3 0 00001
2 22566 71.0040 125.4837 0012648 260.4067 99.5627 14.15311172 05
| Epoch (UTC): | 21 April 2026 09:33:22 |
| Eccentricity: | 0.0012648 |
| inclination: | 71.0040° |
| perigee height: | 832 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 125.4837° |
| argument of perigee: | 260.4067° |
| revolutions per day: | 14.15311172 |
| mean anomaly at epoch: | 99.5627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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