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 65519U 26144.88040786 +.00000000 +00000-0 +83124-3 0 00008
2 65519 53.1589 276.4942 0001137 69.4441 290.6684 15.34409767 04
| Epoch (UTC): | 24 May 2026 21:07:47 |
| Eccentricity: | 0.0001137 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 276.4942° |
| argument of perigee: | 69.4441° |
| revolutions per day: | 15.34409767 |
| mean anomaly at epoch: | 290.6684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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