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 47256U 26145.52891845 +.00000000 +00000-0 +00000-0 0 00007
2 47256 0.0244 82.5272 0003790 208.4060 225.5857 1.00270300 08
| Epoch (UTC): | 25 May 2026 12:41:38 |
| Eccentricity: | 0.0003790 |
| inclination: | 0.0244° |
| perigee height: | 35771 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 82.5272° |
| argument of perigee: | 208.4060° |
| revolutions per day: | 1.00270300 |
| mean anomaly at epoch: | 225.5857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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