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 32062U 26053.70810369 +.00000000 +00000-0 +11416-3 0 00002
2 32062 98.3808 0.4352 0030349 321.5081 105.4111 14.41404566 02
| Epoch (UTC): | 22 February 2026 16:59:40 |
| Eccentricity: | 0.0030349 |
| inclination: | 98.3808° |
| perigee height: | 732 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 0.4352° |
| argument of perigee: | 321.5081° |
| revolutions per day: | 14.41404566 |
| mean anomaly at epoch: | 105.4111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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