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 23334.47418867 .00012796 00000-0 10457-2 0 9997
2 32791 97.6801 302.6949 0008874 197.5497 162.5420 14.99479706846630
| Epoch (UTC): | 30 November 2023 11:22:49 |
| Eccentricity: | 0.0008874 |
| inclination: | 97.6801° |
| perigee height: | 562 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 302.6949° |
| argument of perigee: | 197.5497° |
| revolutions per day: | 14.99479706 |
| mean anomaly at epoch: | 162.5420° |
| orbit number at epoch: | 84663 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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