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 00016U 58002A 23337.47763725 .00000827 00000-0 11652-2 0 9995
2 00016 34.2600 104.4935 2020562 167.9854 197.7384 10.48988585591557
| Epoch (UTC): | 03 December 2023 11:27:47 |
| Eccentricity: | 0.2020562 |
| inclination: | 34.2600° |
| perigee height: | 656 km |
| apogee height: | 4218 km |
| right ascension of ascending node: | 104.4935° |
| argument of perigee: | 167.9854° |
| revolutions per day: | 10.48988585 |
| mean anomaly at epoch: | 197.7384° |
| orbit number at epoch: | 59155 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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