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 23156.68884819 .00000286 00000-0 96800-4 0 9993
2 11574 74.0674 155.1304 0016818 227.8422 132.1306 14.41157677290839
| Epoch (UTC): | 05 June 2023 16:31:56 |
| Eccentricity: | 0.0016818 |
| inclination: | 74.0674° |
| perigee height: | 742 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 155.1304° |
| argument of perigee: | 227.8422° |
| revolutions per day: | 14.41157677 |
| mean anomaly at epoch: | 132.1306° |
| orbit number at epoch: | 29083 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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