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 20682U 26041.65998859 +.00000000 +00000-0 +41900-3 0 00000
2 20682 63.2943 190.1838 0880601 80.5030 289.4313 13.64194283 07
| Epoch (UTC): | 10 February 2026 15:50:23 |
| Eccentricity: | 0.0880601 |
| inclination: | 63.2943° |
| perigee height: | 369 km |
| apogee height: | 1672 km |
| right ascension of ascending node: | 190.1838° |
| argument of perigee: | 80.5030° |
| revolutions per day: | 13.64194283 |
| mean anomaly at epoch: | 289.4313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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