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 22279.83816648 .00005892 00000-0 56786-3 0 9998
2 32791 97.6240 252.6351 0012707 170.8336 189.3118 14.93226243783893
| Epoch (UTC): | 06 October 2022 20:06:57 |
| Eccentricity: | 0.0012707 |
| inclination: | 97.6240° |
| perigee height: | 579 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 252.6351° |
| argument of perigee: | 170.8336° |
| revolutions per day: | 14.93226243 |
| mean anomaly at epoch: | 189.3118° |
| orbit number at epoch: | 78389 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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