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 23343.48999123 .00000304 00000-0 11979-3 0 9991
2 39090 98.3800 172.0328 0009981 100.1069 260.1243 14.35805309564874
| Epoch (UTC): | 09 December 2023 11:45:35 |
| Eccentricity: | 0.0009981 |
| inclination: | 98.3800° |
| perigee height: | 765 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 172.0328° |
| argument of perigee: | 100.1069° |
| revolutions per day: | 14.35805309 |
| mean anomaly at epoch: | 260.1243° |
| orbit number at epoch: | 56487 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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