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 22177.53792655 .00009856 00000-0 54563-3 0 9995
2 32789 97.3381 203.5080 0008095 295.8446 64.1951 15.14004074773302
| Epoch (UTC): | 26 June 2022 12:54:36 |
| Eccentricity: | 0.0008095 |
| inclination: | 97.3381° |
| perigee height: | 518 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 203.5080° |
| argument of perigee: | 295.8446° |
| revolutions per day: | 15.14004074 |
| mean anomaly at epoch: | 64.1951° |
| orbit number at epoch: | 77330 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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