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 32789U 08021G 22179.52066344 .00006162 00000-0 34230-3 0 9991
2 32789 97.3375 205.4197 0008037 287.1915 72.8437 15.14036656773605
| Epoch (UTC): | 28 June 2022 12:29:45 |
| Eccentricity: | 0.0008037 |
| inclination: | 97.3375° |
| perigee height: | 518 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 205.4197° |
| argument of perigee: | 287.1915° |
| revolutions per day: | 15.14036656 |
| mean anomaly at epoch: | 72.8437° |
| orbit number at epoch: | 77360 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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