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 32205U 99025CVB 22225.86708542 .00000125 00000-0 90618-4 0 9996
2 32205 98.7279 248.2177 0011592 152.6422 335.1894 14.12670592773105
| Epoch (UTC): | 13 August 2022 20:48:36 |
| Eccentricity: | 0.0011592 |
| inclination: | 98.7279° |
| perigee height: | 842 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 248.2177° |
| argument of perigee: | 152.6422° |
| revolutions per day: | 14.12670592 |
| mean anomaly at epoch: | 335.1894° |
| orbit number at epoch: | 77310 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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