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 22272.80821193 .00002865 00000-0 30302-3 0 9995
2 32785 97.6699 240.4323 0010960 245.0253 114.9827 14.89921526782026
| Epoch (UTC): | 29 September 2022 19:23:49 |
| Eccentricity: | 0.0010960 |
| inclination: | 97.6699° |
| perigee height: | 590 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 240.4323° |
| argument of perigee: | 245.0253° |
| revolutions per day: | 14.89921526 |
| mean anomaly at epoch: | 114.9827° |
| orbit number at epoch: | 78202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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