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 59588U 24077B 24283.11311538 .00004250 00000-0 47994-2 0 9993
2 59588 97.4473 324.9447 0051100 181.8727 178.2242 13.70328921 22988
| Epoch (UTC): | 09 October 2024 02:42:53 |
| Eccentricity: | 0.0051100 |
| inclination: | 97.4473° |
| perigee height: | 960 km |
| apogee height: | 1036 km |
| right ascension of ascending node: | 324.9447° |
| argument of perigee: | 181.8727° |
| revolutions per day: | 13.70328921 |
| mean anomaly at epoch: | 178.2242° |
| orbit number at epoch: | 2298 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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