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 32788U 08021F 24262.49678097 .00043801 00000-0 17614-2 0 9992
2 32788 97.6005 243.4543 0005764 150.8028 209.3532 15.24759634892502
| Epoch (UTC): | 18 September 2024 11:55:21 |
| Eccentricity: | 0.0005764 |
| inclination: | 97.6005° |
| perigee height: | 487 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 243.4543° |
| argument of perigee: | 150.8028° |
| revolutions per day: | 15.24759634 |
| mean anomaly at epoch: | 209.3532° |
| orbit number at epoch: | 89250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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