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 62847U 26103.74178117 +.00000000 +00000-0 +29676-3 0 00001
2 62847 43.0022 250.8564 0002073 277.2930 82.7686 15.27590352 08
| Epoch (UTC): | 13 April 2026 17:48:09 |
| Eccentricity: | 0.0002073 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 250.8564° |
| argument of perigee: | 277.2930° |
| revolutions per day: | 15.27590352 |
| mean anomaly at epoch: | 82.7686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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