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 22175.62123203 .00008610 00000-0 47766-3 0 9994
2 32789 97.3383 201.6603 0008290 303.5826 56.4614 15.13965064773012
| Epoch (UTC): | 24 June 2022 14:54:34 |
| Eccentricity: | 0.0008290 |
| inclination: | 97.3383° |
| perigee height: | 518 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 201.6603° |
| argument of perigee: | 303.5826° |
| revolutions per day: | 15.13965064 |
| mean anomaly at epoch: | 56.4614° |
| orbit number at epoch: | 77301 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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