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 39161U 13021C 22027.72001982 .00000449 00000-0 78175-4 0 9998
2 39161 97.9214 108.5753 0009892 146.6238 213.5589 14.72650984468750
| Epoch (UTC): | 27 January 2022 17:16:49 |
| Eccentricity: | 0.0009892 |
| inclination: | 97.9214° |
| perigee height: | 645 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 108.5753° |
| argument of perigee: | 146.6238° |
| revolutions per day: | 14.72650984 |
| mean anomaly at epoch: | 213.5589° |
| orbit number at epoch: | 46875 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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