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 65344U 26145.43869447 +.00000000 +00000-0 +36937-3 0 00009
2 65344 53.1596 210.5169 0000860 72.5021 287.6073 15.30204678 07
| Epoch (UTC): | 25 May 2026 10:31:43 |
| Eccentricity: | 0.0000860 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.5169° |
| argument of perigee: | 72.5021° |
| revolutions per day: | 15.30204678 |
| mean anomaly at epoch: | 287.6073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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