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 57856U 26145.37697770 +.00000000 +00000-0 +13570-4 0 00008
2 57856 53.1610 287.5978 0001297 98.5783 261.5365 15.31696599 06
| Epoch (UTC): | 25 May 2026 09:02:50 |
| Eccentricity: | 0.0001297 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 287.5978° |
| argument of perigee: | 98.5783° |
| revolutions per day: | 15.31696599 |
| mean anomaly at epoch: | 261.5365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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