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 41926U 26145.37632477 +.00000000 +00000-0 +59777-4 0 00001
2 41926 86.3952 97.9152 0002868 82.1466 278.0055 14.34210433 03
| Epoch (UTC): | 25 May 2026 09:01:54 |
| Eccentricity: | 0.0002868 |
| inclination: | 86.3952° |
| perigee height: | 776 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 97.9152° |
| argument of perigee: | 82.1466° |
| revolutions per day: | 14.34210433 |
| mean anomaly at epoch: | 278.0055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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