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 32791U 08021J 22221.39714887 .00002215 00000-0 21867-3 0 9996
2 32791 97.6151 196.0208 0013259 21.0632 339.1131 14.92889553775096
| Epoch (UTC): | 09 August 2022 09:31:53 |
| Eccentricity: | 0.0013259 |
| inclination: | 97.6151° |
| perigee height: | 579 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 196.0208° |
| argument of perigee: | 21.0632° |
| revolutions per day: | 14.92889553 |
| mean anomaly at epoch: | 339.1131° |
| orbit number at epoch: | 77509 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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