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 26070.83080326 +.00000000 +00000-0 +35433-3 0 00007
2 20682 63.2946 111.2787 0879676 81.0463 288.8991 13.64549537 04
| Epoch (UTC): | 11 March 2026 19:56:21 |
| Eccentricity: | 0.0879676 |
| inclination: | 63.2946° |
| perigee height: | 368 km |
| apogee height: | 1670 km |
| right ascension of ascending node: | 111.2787° |
| argument of perigee: | 81.0463° |
| revolutions per day: | 13.64549537 |
| mean anomaly at epoch: | 288.8991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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