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 32785U 08021C 22179.91693705 .00000930 00000-0 10291-3 0 9995
2 32785 97.6577 150.4024 0012198 188.5592 171.5420 14.89625201768192
| Epoch (UTC): | 28 June 2022 22:00:23 |
| Eccentricity: | 0.0012198 |
| inclination: | 97.6577° |
| perigee height: | 590 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 150.4024° |
| argument of perigee: | 188.5592° |
| revolutions per day: | 14.89625201 |
| mean anomaly at epoch: | 171.5420° |
| orbit number at epoch: | 76819 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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