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 00005U 58002B 24316.30493617 .00001000 00000-0 12770-2 0 9999
2 00005 34.2482 313.3771 1842739 30.4510 339.1234 10.85777768379912
Epoch (UTC): | 11 November 2024 07:19:06 |
Eccentricity: | 0.1842739 |
inclination: | 34.2482° |
perigee height: | 649 km |
apogee height: | 3824 km |
right ascension of ascending node: | 313.3771° |
argument of perigee: | 30.4510° |
revolutions per day: | 10.85777768 |
mean anomaly at epoch: | 339.1234° |
orbit number at epoch: | 37991 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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