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 43792U 26050.42410867 +.00000000 +00000-0 +81641-4 0 00007
2 43792 97.4142 92.7873 0012836 23.6350 336.5463 15.03829580 00
| Epoch (UTC): | 19 February 2026 10:10:42 |
| Eccentricity: | 0.0012836 |
| inclination: | 97.4142° |
| perigee height: | 546 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 92.7873° |
| argument of perigee: | 23.6350° |
| revolutions per day: | 15.03829580 |
| mean anomaly at epoch: | 336.5463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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