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 20827U 26039.15702597 +.00000000 +00000-0 +23078-4 0 00002
2 20827 82.5304 305.2700 0103008 336.8060 22.8467 13.84643848 06
| Epoch (UTC): | 08 February 2026 03:46:07 |
| Eccentricity: | 0.0103008 |
| inclination: | 82.5304° |
| perigee height: | 872 km |
| apogee height: | 1023 km |
| right ascension of ascending node: | 305.2700° |
| argument of perigee: | 336.8060° |
| revolutions per day: | 13.84643848 |
| mean anomaly at epoch: | 22.8467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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