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 23276.43324964 .00015082 00000-0 14595-2 0 9991
2 39439 97.6921 239.1068 0051874 278.6450 80.8894 14.91828780533444
| Epoch (UTC): | 03 October 2023 10:23:52 |
| Eccentricity: | 0.0051874 |
| inclination: | 97.6921° |
| perigee height: | 556 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 239.1068° |
| argument of perigee: | 278.6450° |
| revolutions per day: | 14.91828780 |
| mean anomaly at epoch: | 80.8894° |
| orbit number at epoch: | 53344 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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