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 65565U 26145.40167184 +.00000000 +00000-0 +67984-4 0 00007
2 65565 81.3048 31.8756 0004930 254.8548 105.2064 13.84340638 03
| Epoch (UTC): | 25 May 2026 09:38:24 |
| Eccentricity: | 0.0004930 |
| inclination: | 81.3048° |
| perigee height: | 945 km |
| apogee height: | 952 km |
| right ascension of ascending node: | 31.8756° |
| argument of perigee: | 254.8548° |
| revolutions per day: | 13.84340638 |
| mean anomaly at epoch: | 105.2064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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