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 5392U 70025KX 24357.90792287 .00003352 00000-0 19453-2 0 9995
2 5392 100.0332 238.2803 0046932 301.7635 57.8963 14.09012301768498
| Epoch (UTC): | 22 December 2024 21:47:24 |
| Eccentricity: | 0.0046932 |
| inclination: | 100.0332° |
| perigee height: | 829 km |
| apogee height: | 897 km |
| right ascension of ascending node: | 238.2803° |
| argument of perigee: | 301.7635° |
| revolutions per day: | 14.09012301 |
| mean anomaly at epoch: | 57.8963° |
| orbit number at epoch: | 76849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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