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 23157.64655006 .00002688 00000-0 47122-3 0 9998
2 39430 97.7810 49.4002 0145934 7.3968 352.9340 14.61792113507992
| Epoch (UTC): | 06 June 2023 15:31:01 |
| Eccentricity: | 0.0145934 |
| inclination: | 97.7810° |
| perigee height: | 584 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 49.4002° |
| argument of perigee: | 7.3968° |
| revolutions per day: | 14.61792113 |
| mean anomaly at epoch: | 352.9340° |
| orbit number at epoch: | 50799 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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