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 32785U 08021C 23083.62408694 .00010228 00000-0 10250-2 0 9994
2 32785 97.6978 51.4800 0013383 32.0973 328.1058 14.91482476808282
| Epoch (UTC): | 24 March 2023 14:58:41 |
| Eccentricity: | 0.0013383 |
| inclination: | 97.6978° |
| perigee height: | 584 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 51.4800° |
| argument of perigee: | 32.0973° |
| revolutions per day: | 14.91482476 |
| mean anomaly at epoch: | 328.1058° |
| orbit number at epoch: | 80828 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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