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 23035.26588143 -.00000090 00000-0 -50387-4 0 9998
2 00050 47.2344 16.1088 0114277 312.0914 47.0203 12.20126058787653
| Epoch (UTC): | 04 February 2023 06:22:52 |
| Eccentricity: | 0.0114277 |
| inclination: | 47.2344° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 16.1088° |
| argument of perigee: | 312.0914° |
| revolutions per day: | 12.20126058 |
| mean anomaly at epoch: | 47.0203° |
| orbit number at epoch: | 78765 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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