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 22182.85902126 .00002845 00000-0 12976-3 0 9992
2 37855 101.7117 309.5580 0152494 19.2096 341.4784 15.12603149583414
| Epoch (UTC): | 01 July 2022 20:36:59 |
| Eccentricity: | 0.0152494 |
| inclination: | 101.7117° |
| perigee height: | 423 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 309.5580° |
| argument of perigee: | 19.2096° |
| revolutions per day: | 15.12603149 |
| mean anomaly at epoch: | 341.4784° |
| orbit number at epoch: | 58341 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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