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 23332.46119149 .00001051 00000-0 42952-3 0 9993
2 00020 33.3454 11.8747 1656411 112.7777 265.5939 11.57973967376370
| Epoch (UTC): | 28 November 2023 11:04:06 |
| Eccentricity: | 0.1656411 |
| inclination: | 33.3454° |
| perigee height: | 507 km |
| apogee height: | 3241 km |
| right ascension of ascending node: | 11.8747° |
| argument of perigee: | 112.7777° |
| revolutions per day: | 11.57973967 |
| mean anomaly at epoch: | 265.5939° |
| orbit number at epoch: | 37637 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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