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 19256U 88053A 24251.87974712 .00000807 00000-0 29477-3 0 9993
2 19256 74.0479 148.3782 0016631 318.5882 41.4009 14.34570690894155
| Epoch (UTC): | 07 September 2024 21:06:50 |
| Eccentricity: | 0.0016631 |
| inclination: | 74.0479° |
| perigee height: | 764 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 148.3782° |
| argument of perigee: | 318.5882° |
| revolutions per day: | 14.34570690 |
| mean anomaly at epoch: | 41.4009° |
| orbit number at epoch: | 89415 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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