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 20466U 26039.75209051 +.00000000 +00000-0 +58475-4 0 00003
2 20466 82.5028 294.5715 0020810 38.7660 321.5043 14.83543405 04
| Epoch (UTC): | 08 February 2026 18:03:00 |
| Eccentricity: | 0.0020810 |
| inclination: | 82.5028° |
| perigee height: | 604 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 294.5715° |
| argument of perigee: | 38.7660° |
| revolutions per day: | 14.83543405 |
| mean anomaly at epoch: | 321.5043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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