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 67822U 26145.53618028 +.00000000 +00000-0 +25131-3 0 00004
2 67822 43.0012 193.3370 0001509 254.8643 105.2041 15.27582588 04
| Epoch (UTC): | 25 May 2026 12:52:05 |
| Eccentricity: | 0.0001509 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.3370° |
| argument of perigee: | 254.8643° |
| revolutions per day: | 15.27582588 |
| mean anomaly at epoch: | 105.2041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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