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 17620U 81053KP 24357.47667727 .00011032 00000-0 39149-2 0 9995
2 17620 83.1746 176.7212 0019772 146.6525 213.5915 14.34253841 35760
| Epoch (UTC): | 22 December 2024 11:26:24 |
| Eccentricity: | 0.0019772 |
| inclination: | 83.1746° |
| perigee height: | 763 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 176.7212° |
| argument of perigee: | 146.6525° |
| revolutions per day: | 14.34253841 |
| mean anomaly at epoch: | 213.5915° |
| orbit number at epoch: | 3576 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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