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 23149.74715465 .00000236 00000-0 81175-4 0 9996
2 11574 74.0677 167.9549 0016979 241.6789 118.2654 14.41152792289834
| Epoch (UTC): | 29 May 2023 17:55:54 |
| Eccentricity: | 0.0016979 |
| inclination: | 74.0677° |
| perigee height: | 742 km |
| apogee height: | 767 km |
| right ascension of ascending node: | 167.9549° |
| argument of perigee: | 241.6789° |
| revolutions per day: | 14.41152792 |
| mean anomaly at epoch: | 118.2654° |
| orbit number at epoch: | 28983 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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