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 23333.48014262 .00000826 00000-0 11715-2 0 9996
2 00016 34.2575 116.0426 2020586 151.1154 221.8131 10.48981875591134
| Epoch (UTC): | 29 November 2023 11:31:24 |
| Eccentricity: | 0.2020586 |
| inclination: | 34.2575° |
| perigee height: | 656 km |
| apogee height: | 4218 km |
| right ascension of ascending node: | 116.0426° |
| argument of perigee: | 151.1154° |
| revolutions per day: | 10.48981875 |
| mean anomaly at epoch: | 221.8131° |
| orbit number at epoch: | 59113 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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