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 65468U 26145.57550903 +.00000000 +00000-0 +23162-3 0 00001
2 65468 53.1608 260.4546 0000629 118.2062 241.9003 15.31706204 06
| Epoch (UTC): | 25 May 2026 13:48:43 |
| Eccentricity: | 0.0000629 |
| inclination: | 53.1608° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 260.4546° |
| argument of perigee: | 118.2062° |
| revolutions per day: | 15.31706204 |
| mean anomaly at epoch: | 241.9003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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