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 23333.16792698 .00003489 00000-0 52358-3 0 9999
2 39161 97.8555 40.6855 0009761 152.4875 207.6853 14.75163445567485
| Epoch (UTC): | 29 November 2023 04:01:48 |
| Eccentricity: | 0.0009761 |
| inclination: | 97.8555° |
| perigee height: | 638 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 40.6855° |
| argument of perigee: | 152.4875° |
| revolutions per day: | 14.75163445 |
| mean anomaly at epoch: | 207.6853° |
| orbit number at epoch: | 56748 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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