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 20805U 26106.70708587 +.00000000 +00000-0 +63895-4 0 00000
2 20805 82.9396 185.5448 0030999 24.9256 140.1399 13.76231575 04
| Epoch (UTC): | 16 April 2026 16:58:12 |
| Eccentricity: | 0.0030999 |
| inclination: | 82.9396° |
| perigee height: | 954 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 185.5448° |
| argument of perigee: | 24.9256° |
| revolutions per day: | 13.76231575 |
| mean anomaly at epoch: | 140.1399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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