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 20666U 26042.23432437 +.00000000 +00000-0 +23806-3 0 00007
2 20666 62.7847 343.8062 0020801 339.7259 20.3012 15.03457534 06
| Epoch (UTC): | 11 February 2026 05:37:25 |
| Eccentricity: | 0.0020801 |
| inclination: | 62.7847° |
| perigee height: | 542 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 343.8062° |
| argument of perigee: | 339.7259° |
| revolutions per day: | 15.03457534 |
| mean anomaly at epoch: | 20.3012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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