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 36794U 10034C 24282.30793342 .00010323 00000-0 30551-2 0 9991
2 36794 49.5109 301.7629 5442967 112.8796 312.0139 4.86535786245347
| Epoch (UTC): | 08 October 2024 07:23:25 |
| Eccentricity: | 0.5442967 |
| inclination: | 49.5109° |
| perigee height: | 326 km |
| apogee height: | 16341 km |
| right ascension of ascending node: | 301.7629° |
| argument of perigee: | 112.8796° |
| revolutions per day: | 4.86535786 |
| mean anomaly at epoch: | 312.0139° |
| orbit number at epoch: | 24534 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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