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 50311U 82092AAC 23027.47014539 .00398175 00000-0 18802-2 0 9992
2 50311 82.5000 32.9559 0025580 186.0522 174.0441 15.81570034 66898
| Epoch (UTC): | 27 January 2023 11:17:00 |
| Eccentricity: | 0.0025580 |
| inclination: | 82.5000° |
| perigee height: | 309 km |
| apogee height: | 343 km |
| right ascension of ascending node: | 32.9559° |
| argument of perigee: | 186.0522° |
| revolutions per day: | 15.81570034 |
| mean anomaly at epoch: | 174.0441° |
| orbit number at epoch: | 6689 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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