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 22565U 26039.80285731 +.00000000 +00000-0 -47082-4 0 00003
2 22565 70.7626 224.5416 0003177 107.8711 252.2755 14.12376579 00
| Epoch (UTC): | 08 February 2026 19:16:06 |
| Eccentricity: | 0.0003177 |
| inclination: | 70.7626° |
| perigee height: | 849 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 224.5416° |
| argument of perigee: | 107.8711° |
| revolutions per day: | 14.12376579 |
| mean anomaly at epoch: | 252.2755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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