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 25634U 99008A 24259.91306728 .00000465 00000-0 23925-3 0 9993
2 25634 98.4286 242.3508 0011423 93.8649 266.3834 14.19727857323587
| Epoch (UTC): | 15 September 2024 21:54:49 |
| Eccentricity: | 0.0011423 |
| inclination: | 98.4286° |
| perigee height: | 818 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 242.3508° |
| argument of perigee: | 93.8649° |
| revolutions per day: | 14.19727857 |
| mean anomaly at epoch: | 266.3834° |
| orbit number at epoch: | 32358 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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