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 00020U 59007A 23027.27744071 .00002998 00000-0 12200-2 0 9994
2 00020 33.3576 22.4891 1660824 288.8011 54.0043 11.56630082341008
| Epoch (UTC): | 27 January 2023 06:39:30 |
| Eccentricity: | 0.1660824 |
| inclination: | 33.3576° |
| perigee height: | 509 km |
| apogee height: | 3253 km |
| right ascension of ascending node: | 22.4891° |
| argument of perigee: | 288.8011° |
| revolutions per day: | 11.56630082 |
| mean anomaly at epoch: | 54.0043° |
| orbit number at epoch: | 34100 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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