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 23081.81266782 .00005854 00000-0 58983-3 0 9998
2 32785 97.6976 49.7117 0013636 37.8584 322.3591 14.91449371808019
| Epoch (UTC): | 22 March 2023 19:30:14 |
| Eccentricity: | 0.0013636 |
| inclination: | 97.6976° |
| perigee height: | 584 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 49.7117° |
| argument of perigee: | 37.8584° |
| revolutions per day: | 14.91449371 |
| mean anomaly at epoch: | 322.3591° |
| orbit number at epoch: | 80801 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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