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 39439U 13066Z 23153.71302056 .00008746 00000-0 89732-3 0 9999
2 39439 97.6791 119.6880 0055344 327.1418 32.6362 14.89507994514074
| Epoch (UTC): | 02 June 2023 17:06:44 |
| Eccentricity: | 0.0055344 |
| inclination: | 97.6791° |
| perigee height: | 561 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 119.6880° |
| argument of perigee: | 327.1418° |
| revolutions per day: | 14.89507994 |
| mean anomaly at epoch: | 32.6362° |
| orbit number at epoch: | 51407 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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