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 57626U 23121A 24358.37151024 .00003066 00000-0 67959-3 0 9994
2 57626 45.0024 88.1430 0006853 331.5901 28.4581 14.58949863 72544
| Epoch (UTC): | 23 December 2024 08:54:58 |
| Eccentricity: | 0.0006853 |
| inclination: | 45.0024° |
| perigee height: | 692 km |
| apogee height: | 701 km |
| right ascension of ascending node: | 88.1430° |
| argument of perigee: | 331.5901° |
| revolutions per day: | 14.58949863 |
| mean anomaly at epoch: | 28.4581° |
| orbit number at epoch: | 7254 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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