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 65566U 26145.42115485 +.00000000 +00000-0 +12342-3 0 00004
2 65566 81.3054 31.7578 0008524 254.6828 105.3386 13.83902386 05
| Epoch (UTC): | 25 May 2026 10:06:27 |
| Eccentricity: | 0.0008524 |
| inclination: | 81.3054° |
| perigee height: | 944 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 31.7578° |
| argument of perigee: | 254.6828° |
| revolutions per day: | 13.83902386 |
| mean anomaly at epoch: | 105.3386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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