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 26044.81196485 +.00000000 +00000-0 +34567-3 0 00007
2 20682 63.2947 181.6600 0880444 80.5697 289.3655 13.64234596 07
| Epoch (UTC): | 13 February 2026 19:29:13 |
| Eccentricity: | 0.0880444 |
| inclination: | 63.2947° |
| perigee height: | 369 km |
| apogee height: | 1672 km |
| right ascension of ascending node: | 181.6600° |
| argument of perigee: | 80.5697° |
| revolutions per day: | 13.64234596 |
| mean anomaly at epoch: | 289.3655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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