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 24278.14740682 .00000453 00000-0 54505-3 0 9994
2 59588 97.4388 321.0969 0049394 187.3923 172.6506 13.69948898 22307
| Epoch (UTC): | 04 October 2024 03:32:15 |
| Eccentricity: | 0.0049394 |
| inclination: | 97.4388° |
| perigee height: | 963 km |
| apogee height: | 1036 km |
| right ascension of ascending node: | 321.0969° |
| argument of perigee: | 187.3923° |
| revolutions per day: | 13.69948898 |
| mean anomaly at epoch: | 172.6506° |
| orbit number at epoch: | 2230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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