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 23090.82163453 .00036426 00000-0 12584-2 0 9996
2 37855 101.7036 9.4482 0127343 276.4558 82.2176 15.22388909625244
| Epoch (UTC): | 31 March 2023 19:43:09 |
| Eccentricity: | 0.0127343 |
| inclination: | 101.7036° |
| perigee height: | 411 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 9.4482° |
| argument of perigee: | 276.4558° |
| revolutions per day: | 15.22388909 |
| mean anomaly at epoch: | 82.2176° |
| orbit number at epoch: | 62524 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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