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 26128.20729250 +.00000000 +00000-0 +92952-4 0 00005
2 20805 82.9368 169.5785 0029598 324.4167 102.0384 13.76235658 08
| Epoch (UTC): | 08 May 2026 04:58:30 |
| Eccentricity: | 0.0029598 |
| inclination: | 82.9368° |
| perigee height: | 955 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 169.5785° |
| argument of perigee: | 324.4167° |
| revolutions per day: | 13.76235658 |
| mean anomaly at epoch: | 102.0384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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