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 24337.69815449 .00018847 00000-0 33543-3 0 9994
2 25544 51.6392 200.5348 0006936 293.3311 173.4353 15.50149230484682
| Epoch (UTC): | 02 December 2024 16:45:20 |
| Eccentricity: | 0.0006936 |
| inclination: | 51.6392° |
| perigee height: | 411 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 200.5348° |
| argument of perigee: | 293.3311° |
| revolutions per day: | 15.50149230 |
| mean anomaly at epoch: | 173.4353° |
| orbit number at epoch: | 48468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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