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 51857U 26145.40876589 +.00000000 +00000-0 -29786-4 0 00001
2 51857 53.2146 34.7241 0001292 87.1704 272.9436 15.08831593 07
| Epoch (UTC): | 25 May 2026 09:48:37 |
| Eccentricity: | 0.0001292 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 34.7241° |
| argument of perigee: | 87.1704° |
| revolutions per day: | 15.08831593 |
| mean anomaly at epoch: | 272.9436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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