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 35532U 91082CP 23331.59418607 .00014687 00000-0 67918-2 0 9999
2 35532 98.7272 102.5481 0120849 268.5050 90.2279 14.17147507533148
| Epoch (UTC): | 27 November 2023 14:15:37 |
| Eccentricity: | 0.0120849 |
| inclination: | 98.7272° |
| perigee height: | 748 km |
| apogee height: | 922 km |
| right ascension of ascending node: | 102.5481° |
| argument of perigee: | 268.5050° |
| revolutions per day: | 14.17147507 |
| mean anomaly at epoch: | 90.2279° |
| orbit number at epoch: | 53314 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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