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 26038.16242265 +.00000000 +00000-0 +66928-4 0 00008
2 09482 81.2568 295.8503 0082429 251.8780 107.3400 14.07972062 06
| Epoch (UTC): | 07 February 2026 03:53:53 |
| Eccentricity: | 0.0082429 |
| inclination: | 81.2568° |
| perigee height: | 807 km |
| apogee height: | 926 km |
| right ascension of ascending node: | 295.8503° |
| argument of perigee: | 251.8780° |
| revolutions per day: | 14.07972062 |
| mean anomaly at epoch: | 107.3400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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