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 26044.74320907 +.00000000 +00000-0 +50861-4 0 00003
2 20466 82.5021 289.8844 0020457 22.9960 337.2166 14.83548037 08
| Epoch (UTC): | 13 February 2026 17:50:13 |
| Eccentricity: | 0.0020457 |
| inclination: | 82.5021° |
| perigee height: | 604 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 289.8844° |
| argument of perigee: | 22.9960° |
| revolutions per day: | 14.83548037 |
| mean anomaly at epoch: | 337.2166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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