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 24311.33547778 .00001260 00000-0 15931-2 0 9995
2 00005 34.2515 328.7181 1843011 8.0409 354.5916 10.85767134379370
Epoch (UTC): | 06 November 2024 08:03:05 |
Eccentricity: | 0.1843011 |
inclination: | 34.2515° |
perigee height: | 649 km |
apogee height: | 3824 km |
right ascension of ascending node: | 328.7181° |
argument of perigee: | 8.0409° |
revolutions per day: | 10.85767134 |
mean anomaly at epoch: | 354.5916° |
orbit number at epoch: | 37937 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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