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 5U 58002B 24314.09631426 .00001123 00000-0 14272-2 0 9990
2 5 34.2485 320.1943 1842784 20.4940 346.0746 10.85773274379775
Epoch (UTC): | 09 November 2024 02:18:41 |
Eccentricity: | 0.1842784 |
inclination: | 34.2485° |
perigee height: | 649 km |
apogee height: | 3824 km |
right ascension of ascending node: | 320.1943° |
argument of perigee: | 20.4940° |
revolutions per day: | 10.85773274 |
mean anomaly at epoch: | 346.0746° |
orbit number at epoch: | 37977 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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