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 23332.10113621 .00050855 00000-0 11556-2 0 9998
2 37855 101.6978 27.9300 0094854 254.3484 104.7264 15.38169993661655
| Epoch (UTC): | 28 November 2023 02:25:38 |
| Eccentricity: | 0.0094854 |
| inclination: | 101.6978° |
| perigee height: | 387 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 27.9300° |
| argument of perigee: | 254.3484° |
| revolutions per day: | 15.38169993 |
| mean anomaly at epoch: | 104.7264° |
| orbit number at epoch: | 66165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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