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 37932U 11068C 24277.13377308 .00000999 00000-0 46365-3 0 9998
2 37932 98.8054 218.7708 0035651 251.7642 119.2037 14.22632164668071
| Epoch (UTC): | 03 October 2024 03:12:37 |
| Eccentricity: | 0.0035651 |
| inclination: | 98.8054° |
| perigee height: | 791 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 218.7708° |
| argument of perigee: | 251.7642° |
| revolutions per day: | 14.22632164 |
| mean anomaly at epoch: | 119.2037° |
| orbit number at epoch: | 66807 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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