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 26019.07944922 +.00000000 +00000-0 +52737-3 0 00003
2 20682 63.2925 251.2325 0882065 80.0831 289.8503 13.63755304 08
| Epoch (UTC): | 19 January 2026 01:54:24 |
| Eccentricity: | 0.0882065 |
| inclination: | 63.2925° |
| perigee height: | 369 km |
| apogee height: | 1675 km |
| right ascension of ascending node: | 251.2325° |
| argument of perigee: | 80.0831° |
| revolutions per day: | 13.63755304 |
| mean anomaly at epoch: | 289.8503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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