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 65475U 26144.80882531 +.00000000 +00000-0 +10710-2 0 00003
2 65475 53.1591 264.2074 0000487 92.2258 267.8800 15.34420145 05
| Epoch (UTC): | 24 May 2026 19:24:42 |
| Eccentricity: | 0.0000487 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 264.2074° |
| argument of perigee: | 92.2258° |
| revolutions per day: | 15.34420145 |
| mean anomaly at epoch: | 267.8800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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