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 52153U 22032A 24358.21438477 .00004176 00000-0 38984-3 0 9996
2 52153 97.6610 39.1441 0010641 183.0996 177.0161 14.94676357148959
| Epoch (UTC): | 23 December 2024 05:08:42 |
| Eccentricity: | 0.0010641 |
| inclination: | 97.6610° |
| perigee height: | 576 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 39.1441° |
| argument of perigee: | 183.0996° |
| revolutions per day: | 14.94676357 |
| mean anomaly at epoch: | 177.0161° |
| orbit number at epoch: | 14895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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