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 20826U 26037.84954831 +.00000000 +00000-0 +32336-4 0 00002
2 20826 82.5260 301.4936 0014188 35.7207 324.4900 13.84451659 03
| Epoch (UTC): | 06 February 2026 20:23:20 |
| Eccentricity: | 0.0014188 |
| inclination: | 82.5260° |
| perigee height: | 938 km |
| apogee height: | 959 km |
| right ascension of ascending node: | 301.4936° |
| argument of perigee: | 35.7207° |
| revolutions per day: | 13.84451659 |
| mean anomaly at epoch: | 324.4900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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