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 23087.78245798 .00063694 00000-0 23286-2 0 9991
2 32789 97.3142 110.2876 0009116 66.5872 293.6325 15.27802016815177
| Epoch (UTC): | 28 March 2023 18:46:44 |
| Eccentricity: | 0.0009116 |
| inclination: | 97.3142° |
| perigee height: | 476 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 110.2876° |
| argument of perigee: | 66.5872° |
| revolutions per day: | 15.27802016 |
| mean anomaly at epoch: | 293.6325° |
| orbit number at epoch: | 81517 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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