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 47596U 26145.05735240 +.00000000 +00000-0 +61117-3 0 00007
2 47596 53.0423 10.4366 0004641 99.4837 260.6702 15.64926923 05
| Epoch (UTC): | 25 May 2026 01:22:35 |
| Eccentricity: | 0.0004641 |
| inclination: | 53.0423° |
| perigee height: | 370 km |
| apogee height: | 377 km |
| right ascension of ascending node: | 10.4366° |
| argument of perigee: | 99.4837° |
| revolutions per day: | 15.64926923 |
| mean anomaly at epoch: | 260.6702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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