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 26040.76380508 +.00000000 +00000-0 +58500-4 0 00002
2 20466 82.5026 293.6215 0020740 35.6089 324.6505 14.83544518 03
| Epoch (UTC): | 09 February 2026 18:19:52 |
| Eccentricity: | 0.0020740 |
| inclination: | 82.5026° |
| perigee height: | 604 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 293.6215° |
| argument of perigee: | 35.6089° |
| revolutions per day: | 14.83544518 |
| mean anomaly at epoch: | 324.6505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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