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 22182.58720716 .00000843 00000-0 86856-4 0 9996
2 32791 97.6119 158.4667 0013779 136.9652 223.2648 14.92724082769304
| Epoch (UTC): | 01 July 2022 14:05:34 |
| Eccentricity: | 0.0013779 |
| inclination: | 97.6119° |
| perigee height: | 580 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 158.4667° |
| argument of perigee: | 136.9652° |
| revolutions per day: | 14.92724082 |
| mean anomaly at epoch: | 223.2648° |
| orbit number at epoch: | 76930 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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