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 26041.57731708 +.00000000 +00000-0 +11683-3 0 00009
2 22081 74.0417 59.4599 0036022 332.1703 27.7521 14.34805347 04
| Epoch (UTC): | 10 February 2026 13:51:20 |
| Eccentricity: | 0.0036022 |
| inclination: | 74.0417° |
| perigee height: | 750 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 59.4599° |
| argument of perigee: | 332.1703° |
| revolutions per day: | 14.34805347 |
| mean anomaly at epoch: | 27.7521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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