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 25544U 98067A 24281.53350623 .00033313 00000-0 60150-3 0 9992
2 25544 51.6369 118.9253 0008961 46.9406 313.2331 15.49376493475973
| Epoch (UTC): | 07 October 2024 12:48:14 |
| Eccentricity: | 0.0008961 |
| inclination: | 51.6369° |
| perigee height: | 412 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 118.9253° |
| argument of perigee: | 46.9406° |
| revolutions per day: | 15.49376493 |
| mean anomaly at epoch: | 313.2331° |
| orbit number at epoch: | 47597 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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