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 47845U 26145.58311512 +.00000000 +00000-0 +33089-4 0 00002
2 47845 53.1597 260.9182 0001479 92.2724 267.8446 15.30196459 05
| Epoch (UTC): | 25 May 2026 13:59:41 |
| Eccentricity: | 0.0001479 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 260.9182° |
| argument of perigee: | 92.2724° |
| revolutions per day: | 15.30196459 |
| mean anomaly at epoch: | 267.8446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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