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 10962U 26022.48585606 +.00000000 +00000-0 +16107-3 0 00003
2 10962 74.0776 175.6245 0025073 346.4791 13.5691 14.42806672 07
| Epoch (UTC): | 22 January 2026 11:39:37 |
| Eccentricity: | 0.0025073 |
| inclination: | 74.0776° |
| perigee height: | 731 km |
| apogee height: | 767 km |
| right ascension of ascending node: | 175.6245° |
| argument of perigee: | 346.4791° |
| revolutions per day: | 14.42806672 |
| mean anomaly at epoch: | 13.5691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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