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 20775U 26041.15023913 +.00000000 +00000-0 +43682-3 0 00007
2 20775 82.9019 276.0595 0366873 106.2701 257.9199 14.88150451 05
| Epoch (UTC): | 10 February 2026 03:36:20 |
| Eccentricity: | 0.0366873 |
| inclination: | 82.9019° |
| perigee height: | 348 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 276.0595° |
| argument of perigee: | 106.2701° |
| revolutions per day: | 14.88150451 |
| mean anomaly at epoch: | 257.9199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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