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 57250U 26145.14515898 +.00000000 +00000-0 +34635-4 0 00006
2 57250 43.0032 308.0409 0001075 266.8779 93.1949 15.27578559 04
| Epoch (UTC): | 25 May 2026 03:29:01 |
| Eccentricity: | 0.0001075 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 308.0409° |
| argument of perigee: | 266.8779° |
| revolutions per day: | 15.27578559 |
| mean anomaly at epoch: | 93.1949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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