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 56256U 22151ABY 24276.39080346 .00010160 00000-0 21734-2 0 9996
2 56256 98.6530 311.0617 0151645 291.5067 67.0018 14.51997289 81419
| Epoch (UTC): | 02 October 2024 09:22:45 |
| Eccentricity: | 0.0151645 |
| inclination: | 98.6530° |
| perigee height: | 611 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 311.0617° |
| argument of perigee: | 291.5067° |
| revolutions per day: | 14.51997289 |
| mean anomaly at epoch: | 67.0018° |
| orbit number at epoch: | 8141 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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