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 43775U 26050.10937718 +.00000000 +00000-0 +18337-3 0 00003
2 43775 97.4381 97.9941 0006200 28.7275 331.4294 15.09267755 01
| Epoch (UTC): | 19 February 2026 02:37:30 |
| Eccentricity: | 0.0006200 |
| inclination: | 97.4381° |
| perigee height: | 534 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 97.9941° |
| argument of perigee: | 28.7275° |
| revolutions per day: | 15.09267755 |
| mean anomaly at epoch: | 331.4294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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