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 37632U 82102C 24352.45132930 .00000832 00000-0 78164-3 0 9999
2 37632 82.9640 258.5456 0031781 344.6720 15.3473 13.80220439510420
| Epoch (UTC): | 17 December 2024 10:49:54 |
| Eccentricity: | 0.0031781 |
| inclination: | 82.9640° |
| perigee height: | 940 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 258.5456° |
| argument of perigee: | 344.6720° |
| revolutions per day: | 13.80220439 |
| mean anomaly at epoch: | 15.3473° |
| orbit number at epoch: | 51042 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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