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 23337.47701938 .00009727 00000-0 79469-3 0 9993
2 32791 97.6817 305.6558 0009195 186.8111 173.2989 14.99561243847006
| Epoch (UTC): | 03 December 2023 11:26:54 |
| Eccentricity: | 0.0009195 |
| inclination: | 97.6817° |
| perigee height: | 562 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 305.6558° |
| argument of perigee: | 186.8111° |
| revolutions per day: | 14.99561243 |
| mean anomaly at epoch: | 173.2989° |
| orbit number at epoch: | 84700 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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