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 22U 59009A 23334.36318156 .00012766 00000-0 80834-3 0 9993
2 22 50.2802 285.4415 0121267 53.3929 307.8105 15.03341148414263
| Epoch (UTC): | 30 November 2023 08:42:58 |
| Eccentricity: | 0.0121267 |
| inclination: | 50.2802° |
| perigee height: | 472 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 285.4415° |
| argument of perigee: | 53.3929° |
| revolutions per day: | 15.03341148 |
| mean anomaly at epoch: | 307.8105° |
| orbit number at epoch: | 41426 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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