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 17191U 86097A 23266.52304348 .00007059 00000-0 33109-3 0 9997
2 17191 82.4697 288.9131 0005487 97.6643 262.5215 15.19495249 9605
Epoch (UTC): | 23 September 2023 12:33:10 |
Eccentricity: | 0.0005487 |
inclination: | 82.4697° |
perigee height: | 503 km |
apogee height: | 511 km |
right ascension of ascending node: | 288.9131° |
argument of perigee: | 97.6643° |
revolutions per day: | 15.19495249 |
mean anomaly at epoch: | 262.5215° |
orbit number at epoch: | 960 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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