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 21891U 92009B 24278.81311879 .00009986 00000-0 97108-3 0 9992
2 21891 19.9956 101.4827 0041448 295.6041 64.0099 14.89168720742011
| Epoch (UTC): | 04 October 2024 19:30:53 |
| Eccentricity: | 0.0041448 |
| inclination: | 19.9956° |
| perigee height: | 571 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 101.4827° |
| argument of perigee: | 295.6041° |
| revolutions per day: | 14.89168720 |
| mean anomaly at epoch: | 64.0099° |
| orbit number at epoch: | 74201 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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