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 43772U 26050.37681306 +.00000000 +00000-0 +10676-2 0 00005
2 43772 97.4341 125.0359 0002724 256.0813 104.0137 15.54215716 01
| Epoch (UTC): | 19 February 2026 09:02:36 |
| Eccentricity: | 0.0002724 |
| inclination: | 97.4341° |
| perigee height: | 403 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 125.0359° |
| argument of perigee: | 256.0813° |
| revolutions per day: | 15.54215716 |
| mean anomaly at epoch: | 104.0137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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