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 58122U 26145.48235387 +.00000000 +00000-0 +27680-4 0 00006
2 58122 43.0086 58.6300 0001715 254.8433 105.2229 15.27582895 09
| Epoch (UTC): | 25 May 2026 11:34:35 |
| Eccentricity: | 0.0001715 |
| inclination: | 43.0086° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 58.6300° |
| argument of perigee: | 254.8433° |
| revolutions per day: | 15.27582895 |
| mean anomaly at epoch: | 105.2229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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