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 11574U 79089B 24281.40747521 .00001515 00000-0 47140-3 0 9999
2 11574 74.0702 330.0397 0017057 275.0602 84.8607 14.41761017361394
| Epoch (UTC): | 07 October 2024 09:46:45 |
| Eccentricity: | 0.0017057 |
| inclination: | 74.0702° |
| perigee height: | 740 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 330.0397° |
| argument of perigee: | 275.0602° |
| revolutions per day: | 14.41761017 |
| mean anomaly at epoch: | 84.8607° |
| orbit number at epoch: | 36139 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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