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 24310.58382313 .00001824 00000-0 20684-3 0 9997
2 16496 82.5263 359.6605 0019449 154.6942 321.4337 14.85716838 76553
Epoch (UTC): | 05 November 2024 14:00:42 |
Eccentricity: | 0.0019449 |
inclination: | 82.5263° |
perigee height: | 598 km |
apogee height: | 625 km |
right ascension of ascending node: | 359.6605° |
argument of perigee: | 154.6942° |
revolutions per day: | 14.85716838 |
mean anomaly at epoch: | 321.4337° |
orbit number at epoch: | 7655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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