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 22488U 26020.11537411 +.00000000 +00000-0 +45180-4 0 00002
2 22488 82.9409 262.1784 0026515 68.2724 41.8886 13.77997287 01
| Epoch (UTC): | 20 January 2026 02:46:08 |
| Eccentricity: | 0.0026515 |
| inclination: | 82.9409° |
| perigee height: | 952 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 262.1784° |
| argument of perigee: | 68.2724° |
| revolutions per day: | 13.77997287 |
| mean anomaly at epoch: | 41.8886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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