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 24281.13129070 .00010842 00000-0 15244-2 0 9990
2 39161 97.8164 344.1928 0008090 220.5922 139.4686 14.77510739613659
| Epoch (UTC): | 07 October 2024 03:09:03 |
| Eccentricity: | 0.0008090 |
| inclination: | 97.8164° |
| perigee height: | 631 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 344.1928° |
| argument of perigee: | 220.5922° |
| revolutions per day: | 14.77510739 |
| mean anomaly at epoch: | 139.4686° |
| orbit number at epoch: | 61365 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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