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 47874U 26145.41191828 +.00000000 +00000-0 +14519-2 0 00007
2 47874 53.1437 219.1500 0004094 344.6079 15.4798 15.35359047 09
| Epoch (UTC): | 25 May 2026 09:53:09 |
| Eccentricity: | 0.0004094 |
| inclination: | 53.1437° |
| perigee height: | 457 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.1500° |
| argument of perigee: | 344.6079° |
| revolutions per day: | 15.35359047 |
| mean anomaly at epoch: | 15.4798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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