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 26075.15446161 +.00000000 +00000-0 +39845-3 0 00001
2 20682 63.2939 99.5788 0879565 81.1321 288.8154 13.64607416 08
| Epoch (UTC): | 16 March 2026 03:42:25 |
| Eccentricity: | 0.0879565 |
| inclination: | 63.2939° |
| perigee height: | 368 km |
| apogee height: | 1670 km |
| right ascension of ascending node: | 99.5788° |
| argument of perigee: | 81.1321° |
| revolutions per day: | 13.64607416 |
| mean anomaly at epoch: | 288.8154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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