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 43911U 26145.63283126 +.00000000 +00000-0 +22915-3 0 00002
2 43911 50.0110 83.1715 0000664 39.2854 320.8109 14.28988114 08
| Epoch (UTC): | 25 May 2026 15:11:16 |
| Eccentricity: | 0.0000664 |
| inclination: | 50.0110° |
| perigee height: | 795 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 83.1715° |
| argument of perigee: | 39.2854° |
| revolutions per day: | 14.28988114 |
| mean anomaly at epoch: | 320.8109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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