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 16U 58002A 23336.52588276 .00000804 00000-0 11348-2 0 9993
2 16 34.2592 107.2432 2020560 163.9686 203.5753 10.48986887591444
| Epoch (UTC): | 02 December 2023 12:37:16 |
| Eccentricity: | 0.2020560 |
| inclination: | 34.2592° |
| perigee height: | 656 km |
| apogee height: | 4218 km |
| right ascension of ascending node: | 107.2432° |
| argument of perigee: | 163.9686° |
| revolutions per day: | 10.48986887 |
| mean anomaly at epoch: | 203.5753° |
| orbit number at epoch: | 59144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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