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 23033.19868018 .00001919 00000-0 30218-3 0 9996
2 39161 97.8855 109.2763 0009949 49.6112 310.5954 14.73573308523295
| Epoch (UTC): | 02 February 2023 04:46:05 |
| Eccentricity: | 0.0009949 |
| inclination: | 97.8855° |
| perigee height: | 642 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 109.2763° |
| argument of perigee: | 49.6112° |
| revolutions per day: | 14.73573308 |
| mean anomaly at epoch: | 310.5954° |
| orbit number at epoch: | 52329 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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