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 57847U 26145.66130689 +.00000000 +00000-0 +14710-3 0 00007
2 57847 53.1603 286.4926 0001205 83.0956 277.0182 15.31702881 00
| Epoch (UTC): | 25 May 2026 15:52:16 |
| Eccentricity: | 0.0001205 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 286.4926° |
| argument of perigee: | 83.0956° |
| revolutions per day: | 15.31702881 |
| mean anomaly at epoch: | 277.0182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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