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 24276.34214250 .00001560 00000-0 48506-3 0 9991
2 11574 74.0711 339.4057 0016928 284.9241 75.0041 14.41748049360667
| Epoch (UTC): | 02 October 2024 08:12:41 |
| Eccentricity: | 0.0016928 |
| inclination: | 74.0711° |
| perigee height: | 740 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 339.4057° |
| argument of perigee: | 284.9241° |
| revolutions per day: | 14.41748049 |
| mean anomaly at epoch: | 75.0041° |
| orbit number at epoch: | 36066 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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