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 47810U 26145.03886851 +.00000000 +00000-0 -56155-4 0 00007
2 47810 53.1609 260.6067 0000305 127.0786 233.0243 15.31698717 07
| Epoch (UTC): | 25 May 2026 00:55:58 |
| Eccentricity: | 0.0000305 |
| inclination: | 53.1609° |
| perigee height: | 471 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 260.6067° |
| argument of perigee: | 127.0786° |
| revolutions per day: | 15.31698717 |
| mean anomaly at epoch: | 233.0243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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