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 16511U 86008B 22225.17937796 -.00000001 00000-0 -16840-4 0 9994
2 16511 82.9411 263.4446 0025344 64.1869 355.6376 13.75812102835193
Epoch (UTC): | 13 August 2022 04:18:18 |
Eccentricity: | 0.0025344 |
inclination: | 82.9411° |
perigee height: | 960 km |
apogee height: | 997 km |
right ascension of ascending node: | 263.4446° |
argument of perigee: | 64.1869° |
revolutions per day: | 13.75812102 |
mean anomaly at epoch: | 355.6376° |
orbit number at epoch: | 83519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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