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 16496U 86006B 23151.92276428 .00000529 00000-0 59425-4 0 9993
2 16496 82.5231 131.1889 0020783 90.0975 328.3099 14.84698340998827
| Epoch (UTC): | 31 May 2023 22:08:46 |
| Eccentricity: | 0.0020783 |
| inclination: | 82.5231° |
| perigee height: | 600 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 131.1889° |
| argument of perigee: | 90.0975° |
| revolutions per day: | 14.84698340 |
| mean anomaly at epoch: | 328.3099° |
| orbit number at epoch: | 99882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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