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 00050U 60009B 24277.73722727 -.00000059 00000-0 24453-3 0 9995
2 00050 47.2313 290.6569 0113868 322.3395 36.9463 12.20146710861828
| Epoch (UTC): | 03 October 2024 17:41:36 |
| Eccentricity: | 0.0113868 |
| inclination: | 47.2313° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 290.6569° |
| argument of perigee: | 322.3395° |
| revolutions per day: | 12.20146710 |
| mean anomaly at epoch: | 36.9463° |
| orbit number at epoch: | 86182 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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