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 47565U 26145.66668980 +.00000000 +00000-0 +83583-3 0 00007
2 47565 53.0376 305.1004 0007369 239.9192 359.0880 15.87057793 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0007369 |
| inclination: | 53.0376° |
| perigee height: | 306 km |
| apogee height: | 315 km |
| right ascension of ascending node: | 305.1004° |
| argument of perigee: | 239.9192° |
| revolutions per day: | 15.87057793 |
| mean anomaly at epoch: | 359.0880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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