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 62122U 26145.48065465 +.00000000 +00000-0 +90115-3 0 00001
2 62122 43.0024 62.4679 0001510 275.0722 84.9957 15.27595509 04
| Epoch (UTC): | 25 May 2026 11:32:08 |
| Eccentricity: | 0.0001510 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 62.4679° |
| argument of perigee: | 275.0722° |
| revolutions per day: | 15.27595509 |
| mean anomaly at epoch: | 84.9957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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