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 37855U 11061F 23333.14188500 .00053013 00000-0 12000-2 0 9995
2 37855 101.6973 29.5834 0094663 251.1624 107.9321 15.38287819662286
| Epoch (UTC): | 29 November 2023 03:24:18 |
| Eccentricity: | 0.0094663 |
| inclination: | 101.6973° |
| perigee height: | 386 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 29.5834° |
| argument of perigee: | 251.1624° |
| revolutions per day: | 15.38287819 |
| mean anomaly at epoch: | 107.9321° |
| orbit number at epoch: | 66228 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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