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 23086.88244015 .00009712 00000-0 87912-3 0 9993
2 32791 97.6500 59.9268 0011124 335.4940 24.5751 14.95554017809582
| Epoch (UTC): | 27 March 2023 21:10:42 |
| Eccentricity: | 0.0011124 |
| inclination: | 97.6500° |
| perigee height: | 573 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 59.9268° |
| argument of perigee: | 335.4940° |
| revolutions per day: | 14.95554017 |
| mean anomaly at epoch: | 24.5751° |
| orbit number at epoch: | 80958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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