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 23338.61972716 .00000696 00000-0 97740-3 0 9991
2 00016 34.2608 101.1938 2020581 172.8049 190.6795 10.48989574591674
| Epoch (UTC): | 04 December 2023 14:52:24 |
| Eccentricity: | 0.2020581 |
| inclination: | 34.2608° |
| perigee height: | 656 km |
| apogee height: | 4218 km |
| right ascension of ascending node: | 101.1938° |
| argument of perigee: | 172.8049° |
| revolutions per day: | 10.48989574 |
| mean anomaly at epoch: | 190.6795° |
| orbit number at epoch: | 59167 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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