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 34430U 93036RX 24358.07136326 .00002525 00000-0 81997-3 0 9996
2 34430 74.0515 237.0939 0061119 36.2272 324.2997 14.38315350828817
Epoch (UTC): | 23 December 2024 01:42:45 |
Eccentricity: | 0.0061119 |
inclination: | 74.0515° |
perigee height: | 720 km |
apogee height: | 808 km |
right ascension of ascending node: | 237.0939° |
argument of perigee: | 36.2272° |
revolutions per day: | 14.38315350 |
mean anomaly at epoch: | 324.2997° |
orbit number at epoch: | 82881 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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