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 26156.84353016 +.00000000 +00000-0 +10196-4 0 00005
2 22566 71.0081 30.0338 0010952 200.1426 159.9266 14.15308518 03
| Epoch (UTC): | 05 June 2026 20:14:41 |
| Eccentricity: | 0.0010952 |
| inclination: | 71.0081° |
| perigee height: | 833 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 30.0338° |
| argument of perigee: | 200.1426° |
| revolutions per day: | 14.15308518 |
| mean anomaly at epoch: | 159.9266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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