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 09482U 26041.21817125 +.00000000 +00000-0 +45910-4 0 00009
2 09482 81.2563 292.8900 0082528 243.1866 116.0847 14.07972594 00
| Epoch (UTC): | 10 February 2026 05:14:09 |
| Eccentricity: | 0.0082528 |
| inclination: | 81.2563° |
| perigee height: | 807 km |
| apogee height: | 926 km |
| right ascension of ascending node: | 292.8900° |
| argument of perigee: | 243.1866° |
| revolutions per day: | 14.07972594 |
| mean anomaly at epoch: | 116.0847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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