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 26022.30571247 +.00000000 +00000-0 +59542-3 0 00000
2 20682 63.2917 242.5127 0881785 80.1463 289.7865 13.63841450 00
| Epoch (UTC): | 22 January 2026 07:20:13 |
| Eccentricity: | 0.0881785 |
| inclination: | 63.2917° |
| perigee height: | 369 km |
| apogee height: | 1674 km |
| right ascension of ascending node: | 242.5127° |
| argument of perigee: | 80.1463° |
| revolutions per day: | 13.63841450 |
| mean anomaly at epoch: | 289.7865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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