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 62211U 26145.58180014 +.00000000 +00000-0 +49796-3 0 00008
2 62211 43.0015 196.2435 0001623 270.7593 89.3073 15.27592420 09
| Epoch (UTC): | 25 May 2026 13:57:47 |
| Eccentricity: | 0.0001623 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 196.2435° |
| argument of perigee: | 270.7593° |
| revolutions per day: | 15.27592420 |
| mean anomaly at epoch: | 89.3073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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