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 57850U 26145.36939654 +.00000000 +00000-0 +46517-4 0 00008
2 57850 53.1622 288.0256 0000748 104.7365 255.3719 15.30192463 08
| Epoch (UTC): | 25 May 2026 08:51:55 |
| Eccentricity: | 0.0000748 |
| inclination: | 53.1622° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 288.0256° |
| argument of perigee: | 104.7365° |
| revolutions per day: | 15.30192463 |
| mean anomaly at epoch: | 255.3719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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