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 47910U 26145.36813765 +.00000000 +00000-0 +64950-4 0 00009
2 47910 53.1584 271.4899 0001173 81.3889 278.7245 15.31703654 08
| Epoch (UTC): | 25 May 2026 08:50:07 |
| Eccentricity: | 0.0001173 |
| inclination: | 53.1584° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 271.4899° |
| argument of perigee: | 81.3889° |
| revolutions per day: | 15.31703654 |
| mean anomaly at epoch: | 278.7245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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