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 26020.11744185 +.00000000 +00000-0 +15719-4 0 00006
2 20805 82.9339 249.8716 0029373 264.2708 260.8679 13.76230374 05
| Epoch (UTC): | 20 January 2026 02:49:06 |
| Eccentricity: | 0.0029373 |
| inclination: | 82.9339° |
| perigee height: | 956 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 249.8716° |
| argument of perigee: | 264.2708° |
| revolutions per day: | 13.76230374 |
| mean anomaly at epoch: | 260.8679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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