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 25348.35400003 -.00000012 00000-0 12715-4 0 9993
2 00016 34.2597 119.5338 2022707 60.0487 318.5609 10.49576979669497
| Epoch (UTC): | 14 December 2025 08:29:45 |
| Eccentricity: | 0.2022707 |
| inclination: | 34.2597° |
| perigee height: | 651 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 119.5338° |
| argument of perigee: | 60.0487° |
| revolutions per day: | 10.49576979 |
| mean anomaly at epoch: | 318.5609° |
| orbit number at epoch: | 66949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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