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 22175.84733629 .00005882 00000-0 26041-3 0 9995
2 37855 101.7095 298.8343 0152717 40.2670 320.9739 15.12526109582350
| Epoch (UTC): | 24 June 2022 20:20:09 |
| Eccentricity: | 0.0152717 |
| inclination: | 101.7095° |
| perigee height: | 423 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 298.8343° |
| argument of perigee: | 40.2670° |
| revolutions per day: | 15.12526109 |
| mean anomaly at epoch: | 320.9739° |
| orbit number at epoch: | 58235 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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