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 65906U 26145.33816228 +.00000000 +00000-0 +55703-3 0 00003
2 65906 53.1589 14.3138 0002041 75.2632 284.8597 15.34399721 08
| Epoch (UTC): | 25 May 2026 08:06:57 |
| Eccentricity: | 0.0002041 |
| inclination: | 53.1589° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 14.3138° |
| argument of perigee: | 75.2632° |
| revolutions per day: | 15.34399721 |
| mean anomaly at epoch: | 284.8597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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