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 26036.97986804 +.00000000 +00000-0 +30727-3 0 00003
2 20666 62.7852 1.6695 0020032 337.8166 22.2064 15.03423586 03
| Epoch (UTC): | 05 February 2026 23:31:00 |
| Eccentricity: | 0.0020032 |
| inclination: | 62.7852° |
| perigee height: | 542 km |
| apogee height: | 570 km |
| right ascension of ascending node: | 1.6695° |
| argument of perigee: | 337.8166° |
| revolutions per day: | 15.03423586 |
| mean anomaly at epoch: | 22.2064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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