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 39430U 13066Q 23160.65829377 .00002678 00000-0 46970-3 0 9996
2 39430 97.7805 52.2363 0145637 357.8783 2.1784 14.61809462508438
| Epoch (UTC): | 09 June 2023 15:47:56 |
| Eccentricity: | 0.0145637 |
| inclination: | 97.7805° |
| perigee height: | 584 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 52.2363° |
| argument of perigee: | 357.8783° |
| revolutions per day: | 14.61809462 |
| mean anomaly at epoch: | 2.1784° |
| orbit number at epoch: | 50843 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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