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 47657U 26145.46542617 +.00000000 +00000-0 +71889-3 0 00001
2 47657 53.1577 50.7420 0002635 154.4710 205.6440 15.73441035 09
| Epoch (UTC): | 25 May 2026 11:10:12 |
| Eccentricity: | 0.0002635 |
| inclination: | 53.1577° |
| perigee height: | 347 km |
| apogee height: | 351 km |
| right ascension of ascending node: | 50.7420° |
| argument of perigee: | 154.4710° |
| revolutions per day: | 15.73441035 |
| mean anomaly at epoch: | 205.6440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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