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 00022U 59009A 23332.36899271 .00012634 00000-0 80115-3 0 9999
2 00022 50.2799 294.9175 0121423 45.6478 315.4346 15.03284777659002
| Epoch (UTC): | 28 November 2023 08:51:20 |
| Eccentricity: | 0.0121423 |
| inclination: | 50.2799° |
| perigee height: | 472 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 294.9175° |
| argument of perigee: | 45.6478° |
| revolutions per day: | 15.03284777 |
| mean anomaly at epoch: | 315.4346° |
| orbit number at epoch: | 65900 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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