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 23151.46267012 .00000529 00000-0 59439-4 0 9996
2 16496 82.5231 131.6205 0020779 91.5009 29.2627 14.84697820998751
| Epoch (UTC): | 31 May 2023 11:06:14 |
| Eccentricity: | 0.0020779 |
| inclination: | 82.5231° |
| perigee height: | 600 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 131.6205° |
| argument of perigee: | 91.5009° |
| revolutions per day: | 14.84697820 |
| mean anomaly at epoch: | 29.2627° |
| orbit number at epoch: | 99875 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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