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 10962U 78063B 24280.87578160 .00001563 00000-0 48031-3 0 9994
2 10962 74.0797 330.2710 0026173 266.3104 93.5059 14.42227513430167
| Epoch (UTC): | 06 October 2024 21:01:07 |
| Eccentricity: | 0.0026173 |
| inclination: | 74.0797° |
| perigee height: | 732 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 330.2710° |
| argument of perigee: | 266.3104° |
| revolutions per day: | 14.42227513 |
| mean anomaly at epoch: | 93.5059° |
| orbit number at epoch: | 43016 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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