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 26101.40910573 +.00000000 +00000-0 +13221-3 0 00007
2 09482 81.2576 234.5633 0085596 73.7303 287.3261 14.07993475 04
| Epoch (UTC): | 11 April 2026 09:49:06 |
| Eccentricity: | 0.0085596 |
| inclination: | 81.2576° |
| perigee height: | 804 km |
| apogee height: | 928 km |
| right ascension of ascending node: | 234.5633° |
| argument of perigee: | 73.7303° |
| revolutions per day: | 14.07993475 |
| mean anomaly at epoch: | 287.3261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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