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 00050U 60009B 23263.77507574 -.00000122 00000-0 -35314-3 0 9994
2 00050 47.2340 26.8732 0113482 273.0791 85.7019 12.20131486815555
| Epoch (UTC): | 20 September 2023 18:36:06 |
| Eccentricity: | 0.0113482 |
| inclination: | 47.2340° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 26.8732° |
| argument of perigee: | 273.0791° |
| revolutions per day: | 12.20131486 |
| mean anomaly at epoch: | 85.7019° |
| orbit number at epoch: | 81555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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