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 16682U 86030B 23340.14232932 .00000346 00000-0 12690-3 0 9992
2 16682 74.0245 205.9521 0015086 326.9408 151.8308 14.36426536970049
| Epoch (UTC): | 06 December 2023 03:24:57 |
| Eccentricity: | 0.0015086 |
| inclination: | 74.0245° |
| perigee height: | 759 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 205.9521° |
| argument of perigee: | 326.9408° |
| revolutions per day: | 14.36426536 |
| mean anomaly at epoch: | 151.8308° |
| orbit number at epoch: | 97004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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