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 22178.89019056 .00005623 00000-0 24901-3 0 9990
2 37855 101.7106 303.4875 0152658 31.0888 329.9251 15.12571071582816
| Epoch (UTC): | 27 June 2022 21:21:52 |
| Eccentricity: | 0.0152658 |
| inclination: | 101.7106° |
| perigee height: | 423 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 303.4875° |
| argument of perigee: | 31.0888° |
| revolutions per day: | 15.12571071 |
| mean anomaly at epoch: | 329.9251° |
| orbit number at epoch: | 58281 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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