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 23331.74348554 .00003575 00000-0 53636-3 0 9995
2 39161 97.8560 39.3028 0009715 156.5251 203.6404 14.75151841567238
| Epoch (UTC): | 27 November 2023 17:50:37 |
| Eccentricity: | 0.0009715 |
| inclination: | 97.8560° |
| perigee height: | 638 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 39.3028° |
| argument of perigee: | 156.5251° |
| revolutions per day: | 14.75151841 |
| mean anomaly at epoch: | 203.6404° |
| orbit number at epoch: | 56723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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