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 23335.87553286 .00015023 00000-0 12252-2 0 9998
2 32791 97.6811 304.0762 0009051 192.1232 167.9775 14.99518478846762
| Epoch (UTC): | 01 December 2023 21:00:46 |
| Eccentricity: | 0.0009051 |
| inclination: | 97.6811° |
| perigee height: | 562 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 304.0762° |
| argument of perigee: | 192.1232° |
| revolutions per day: | 14.99518478 |
| mean anomaly at epoch: | 167.9775° |
| orbit number at epoch: | 84676 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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