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 24261.29054559 .00002063 00000-0 25990-2 0 9992
2 5 34.2429 123.1269 1843139 142.5359 231.9187 10.85646277374037
Epoch (UTC): | 17 September 2024 06:58:23 |
Eccentricity: | 0.1843139 |
inclination: | 34.2429° |
perigee height: | 649 km |
apogee height: | 3825 km |
right ascension of ascending node: | 123.1269° |
argument of perigee: | 142.5359° |
revolutions per day: | 10.85646277 |
mean anomaly at epoch: | 231.9187° |
orbit number at epoch: | 37403 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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