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 24256.83258804 .00038544 00000-0 70362-3 0 9992
2 25544 51.6364 241.2184 0007518 344.4386 15.6370 15.49004202472149
| Epoch (UTC): | 12 September 2024 19:58:55 |
| Eccentricity: | 0.0007518 |
| inclination: | 51.6364° |
| perigee height: | 414 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 241.2184° |
| argument of perigee: | 344.4386° |
| revolutions per day: | 15.49004202 |
| mean anomaly at epoch: | 15.6370° |
| orbit number at epoch: | 47214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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