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 48426U 26145.33605884 +.00000000 +00000-0 +31711-3 0 00008
2 48426 34.9979 107.0167 0002645 103.0374 257.0632 15.11810891 04
| Epoch (UTC): | 25 May 2026 08:03:55 |
| Eccentricity: | 0.0002645 |
| inclination: | 34.9979° |
| perigee height: | 529 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 107.0167° |
| argument of perigee: | 103.0374° |
| revolutions per day: | 15.11810891 |
| mean anomaly at epoch: | 257.0632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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