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 26039.41485208 +.00000000 +00000-0 +62268-4 0 00001
2 20466 82.5028 294.8882 0020839 39.8159 320.4580 14.83543189 01
| Epoch (UTC): | 08 February 2026 09:57:23 |
| Eccentricity: | 0.0020839 |
| inclination: | 82.5028° |
| perigee height: | 604 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 294.8882° |
| argument of perigee: | 39.8159° |
| revolutions per day: | 14.83543189 |
| mean anomaly at epoch: | 320.4580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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