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 26105.30483406 +.00000000 +00000-0 +44827-4 0 00009
2 20805 82.9396 186.5859 0031088 28.7860 32.8368 13.76231368 07
| Epoch (UTC): | 15 April 2026 07:18:57 |
| Eccentricity: | 0.0031088 |
| inclination: | 82.9396° |
| perigee height: | 954 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 186.5859° |
| argument of perigee: | 28.7860° |
| revolutions per day: | 13.76231368 |
| mean anomaly at epoch: | 32.8368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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