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 26040.08493729 +.00000000 +00000-0 -65608-4 0 00008
2 22566 71.0066 275.2634 0010325 353.0260 7.0718 14.15303599 05
| Epoch (UTC): | 09 February 2026 02:02:18 |
| Eccentricity: | 0.0010325 |
| inclination: | 71.0066° |
| perigee height: | 834 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 275.2634° |
| argument of perigee: | 353.0260° |
| revolutions per day: | 14.15303599 |
| mean anomaly at epoch: | 7.0718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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