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 54847U 26145.40940259 +.00000000 +00000-0 -84570-7 0 00004
2 54847 43.0051 37.0155 0001156 263.5869 96.4851 15.27575293 05
| Epoch (UTC): | 25 May 2026 09:49:32 |
| Eccentricity: | 0.0001156 |
| inclination: | 43.0051° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.0155° |
| argument of perigee: | 263.5869° |
| revolutions per day: | 15.27575293 |
| mean anomaly at epoch: | 96.4851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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