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 24281.06296976 .00001886 00000-0 23373-2 0 9995
2 5 34.2553 62.1087 1843561 231.6581 110.3667 10.85695898376174
Epoch (UTC): | 07 October 2024 01:30:40 |
Eccentricity: | 0.1843561 |
inclination: | 34.2553° |
perigee height: | 649 km |
apogee height: | 3825 km |
right ascension of ascending node: | 62.1087° |
argument of perigee: | 231.6581° |
revolutions per day: | 10.85695898 |
mean anomaly at epoch: | 110.3667° |
orbit number at epoch: | 37617 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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