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 11574U 79089B 23342.50728664 .00000245 00000-0 83593-4 0 9996
2 11574 74.0674 171.8011 0016039 197.4355 162.6252 14.41336016317600
Epoch (UTC): | 08 December 2023 12:10:29 |
Eccentricity: | 0.0016039 |
inclination: | 74.0674° |
perigee height: | 742 km |
apogee height: | 765 km |
right ascension of ascending node: | 171.8011° |
argument of perigee: | 197.4355° |
revolutions per day: | 14.41336016 |
mean anomaly at epoch: | 162.6252° |
orbit number at epoch: | 31760 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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