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 39090U 13009E 24262.56514686 .00001035 00000-0 36854-3 0 9999
2 39090 98.3820 88.2991 0008469 341.1945 18.8928 14.36280805605648
| Epoch (UTC): | 18 September 2024 13:33:48 |
| Eccentricity: | 0.0008469 |
| inclination: | 98.3820° |
| perigee height: | 765 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 88.2991° |
| argument of perigee: | 341.1945° |
| revolutions per day: | 14.36280805 |
| mean anomaly at epoch: | 18.8928° |
| orbit number at epoch: | 60564 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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