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 47589U 26145.61053406 +.00000000 +00000-0 +75160-3 0 00001
2 47589 53.0418 344.7314 0002208 47.9995 312.1210 15.71438757 05
| Epoch (UTC): | 25 May 2026 14:39:10 |
| Eccentricity: | 0.0002208 |
| inclination: | 53.0418° |
| perigee height: | 353 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 344.7314° |
| argument of perigee: | 47.9995° |
| revolutions per day: | 15.71438757 |
| mean anomaly at epoch: | 312.1210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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