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 22177.89796625 .00007687 00000-0 33774-3 0 9993
2 37855 101.7101 301.9699 0152621 34.0795 327.0107 15.12558676582666
| Epoch (UTC): | 26 June 2022 21:33:04 |
| Eccentricity: | 0.0152621 |
| inclination: | 101.7101° |
| perigee height: | 423 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 301.9699° |
| argument of perigee: | 34.0795° |
| revolutions per day: | 15.12558676 |
| mean anomaly at epoch: | 327.0107° |
| orbit number at epoch: | 58266 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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