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 26088.19769691 +.00000000 +00000-0 +59591-3 0 00005
2 20682 63.2942 64.2745 0879097 81.3904 288.5616 13.64781622 05
| Epoch (UTC): | 29 March 2026 04:44:41 |
| Eccentricity: | 0.0879097 |
| inclination: | 63.2942° |
| perigee height: | 368 km |
| apogee height: | 1669 km |
| right ascension of ascending node: | 64.2745° |
| argument of perigee: | 81.3904° |
| revolutions per day: | 13.64781622 |
| mean anomaly at epoch: | 288.5616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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