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 data is extracted from the following two-line orbital elements,
1 50921U 82092AVQ 23090.10248788 .00165049 00000-0 22545-2 0 9995
2 50921 82.5654 339.2715 0023371 125.1925 235.1523 15.56578971 69202
| Epoch (UTC): | 31 March 2023 02:27:34 |
| Eccentricity: | 0.0023371 |
| inclination: | 82.5654° |
| perigee height: | 382 km |
| apogee height: | 413 km |
| right ascension of ascending node: | 339.2715° |
| argument of perigee: | 125.1925° |
| revolutions per day: | 15.56578971 |
| mean anomaly at epoch: | 235.1523° |
| orbit number at epoch: | 6920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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