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 24264.34013905 .00019814 00000-0 36189-3 0 9996
2 25544 51.6387 204.0640 0007518 13.8616 124.3173 15.49370925473307
| Epoch (UTC): | 20 September 2024 08:09:48 |
| Eccentricity: | 0.0007518 |
| inclination: | 51.6387° |
| perigee height: | 413 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 204.0640° |
| argument of perigee: | 13.8616° |
| revolutions per day: | 15.49370925 |
| mean anomaly at epoch: | 124.3173° |
| orbit number at epoch: | 47330 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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