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 19119U 88039A 24277.22737719 .00000917 00000-0 49321-3 0 9998
2 19119 71.0012 264.1234 0012986 315.2819 55.5131 14.15522086879144
| Epoch (UTC): | 03 October 2024 05:27:25 |
| Eccentricity: | 0.0012986 |
| inclination: | 71.0012° |
| perigee height: | 831 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 264.1234° |
| argument of perigee: | 315.2819° |
| revolutions per day: | 14.15522086 |
| mean anomaly at epoch: | 55.5131° |
| orbit number at epoch: | 87914 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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