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 50U 60009B 23028.14024689 -.00000084 00000-0 87974-5 0 9992
2 50 47.2332 38.2238 0114325 290.8472 68.0106 12.20126189787232
| Epoch (UTC): | 28 January 2023 03:21:57 |
| Eccentricity: | 0.0114325 |
| inclination: | 47.2332° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 38.2238° |
| argument of perigee: | 290.8472° |
| revolutions per day: | 12.20126189 |
| mean anomaly at epoch: | 68.0106° |
| orbit number at epoch: | 78723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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