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 23332.52829832 .00000794 00000-0 11278-2 0 9995
2 00016 34.2571 118.7921 2020617 147.1002 227.3323 10.48980152591031
| Epoch (UTC): | 28 November 2023 12:40:44 |
| Eccentricity: | 0.2020617 |
| inclination: | 34.2571° |
| perigee height: | 656 km |
| apogee height: | 4218 km |
| right ascension of ascending node: | 118.7921° |
| argument of perigee: | 147.1002° |
| revolutions per day: | 10.48980152 |
| mean anomaly at epoch: | 227.3323° |
| orbit number at epoch: | 59103 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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