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 22081U 26040.46173751 +.00000000 +00000-0 +12031-3 0 00002
2 22081 74.0417 61.5034 0035978 334.4530 25.4843 14.34804646 07
| Epoch (UTC): | 09 February 2026 11:04:54 |
| Eccentricity: | 0.0035978 |
| inclination: | 74.0417° |
| perigee height: | 750 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 61.5034° |
| argument of perigee: | 334.4530° |
| revolutions per day: | 14.34804646 |
| mean anomaly at epoch: | 25.4843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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