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 26044.82825369 +.00000000 +00000-0 +19697-3 0 00007
2 20666 62.7848 334.9872 0021172 340.4877 19.5409 15.03472165 01
| Epoch (UTC): | 13 February 2026 19:52:41 |
| Eccentricity: | 0.0021172 |
| inclination: | 62.7848° |
| perigee height: | 542 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 334.9872° |
| argument of perigee: | 340.4877° |
| revolutions per day: | 15.03472165 |
| mean anomaly at epoch: | 19.5409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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