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 65583U 26145.40792072 +.00000000 +00000-0 +93903-4 0 00007
2 65583 81.3050 31.8821 0006594 249.0472 110.9979 13.83615554 08
| Epoch (UTC): | 25 May 2026 09:47:24 |
| Eccentricity: | 0.0006594 |
| inclination: | 81.3050° |
| perigee height: | 946 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 31.8821° |
| argument of perigee: | 249.0472° |
| revolutions per day: | 13.83615554 |
| mean anomaly at epoch: | 110.9979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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