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 43641U 26145.58756795 +.00000000 +00000-0 -22616-4 0 00003
2 43641 97.8892 332.6646 0001504 80.6600 279.4783 14.82152403 03
| Epoch (UTC): | 25 May 2026 14:06:05 |
| Eccentricity: | 0.0001504 |
| inclination: | 97.8892° |
| perigee height: | 621 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 332.6646° |
| argument of perigee: | 80.6600° |
| revolutions per day: | 14.82152403 |
| mean anomaly at epoch: | 279.4783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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