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 65480U 26144.68907123 +.00000000 +00000-0 +64538-3 0 00008
2 65480 53.1589 264.8530 0001026 73.0848 287.0267 15.34397510 03
| Epoch (UTC): | 24 May 2026 16:32:15 |
| Eccentricity: | 0.0001026 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 264.8530° |
| argument of perigee: | 73.0848° |
| revolutions per day: | 15.34397510 |
| mean anomaly at epoch: | 287.0267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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