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 23153.49567176 .00000313 00000-0 10512-3 0 9999
2 11574 74.0674 161.0296 0016907 234.1940 125.7646 14.41155588290373
| Epoch (UTC): | 02 June 2023 11:53:46 |
| Eccentricity: | 0.0016907 |
| inclination: | 74.0674° |
| perigee height: | 742 km |
| apogee height: | 767 km |
| right ascension of ascending node: | 161.0296° |
| argument of perigee: | 234.1940° |
| revolutions per day: | 14.41155588 |
| mean anomaly at epoch: | 125.7646° |
| orbit number at epoch: | 29037 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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