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 23333.10650502 .00000738 00000-0 26963-3 0 9994
2 39090 98.3806 161.9378 0009720 128.3224 231.8837 14.35792196563409
| Epoch (UTC): | 29 November 2023 02:33:22 |
| Eccentricity: | 0.0009720 |
| inclination: | 98.3806° |
| perigee height: | 765 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 161.9378° |
| argument of perigee: | 128.3224° |
| revolutions per day: | 14.35792196 |
| mean anomaly at epoch: | 231.8837° |
| orbit number at epoch: | 56340 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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