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 11326U 79030A 24337.46345522 .00000167 00000-0 15782-3 0 9992
2 11326 82.9476 101.9591 0028340 227.4078 175.8226 13.75575169525398
| Epoch (UTC): | 02 December 2024 11:07:22 |
| Eccentricity: | 0.0028340 |
| inclination: | 82.9476° |
| perigee height: | 959 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 101.9591° |
| argument of perigee: | 227.4078° |
| revolutions per day: | 13.75575169 |
| mean anomaly at epoch: | 175.8226° |
| orbit number at epoch: | 52539 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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