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 26040.93602793 +.00000000 +00000-0 -42906-4 0 00000
2 22565 70.7627 222.1437 0003154 105.0288 255.1181 14.12376388 05
| Epoch (UTC): | 09 February 2026 22:27:52 |
| Eccentricity: | 0.0003154 |
| inclination: | 70.7627° |
| perigee height: | 849 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 222.1437° |
| argument of perigee: | 105.0288° |
| revolutions per day: | 14.12376388 |
| mean anomaly at epoch: | 255.1181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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