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 20682U 26071.49035597 +.00000000 +00000-0 +37544-3 0 00005
2 20682 63.2947 109.4943 0879658 81.0597 288.8860 13.64557990 03
| Epoch (UTC): | 12 March 2026 11:46:06 |
| Eccentricity: | 0.0879658 |
| inclination: | 63.2947° |
| perigee height: | 368 km |
| apogee height: | 1670 km |
| right ascension of ascending node: | 109.4943° |
| argument of perigee: | 81.0597° |
| revolutions per day: | 13.64557990 |
| mean anomaly at epoch: | 288.8860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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