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 00059U 60013B 24305.32884702 .00000288 00000-0 26877-3 0 9993
2 00059 28.2492 294.8951 0188993 10.1043 350.3232 13.53104768162676
Epoch (UTC): | 31 October 2024 07:53:32 |
Eccentricity: | 0.0188993 |
inclination: | 28.2492° |
perigee height: | 920 km |
apogee height: | 1201 km |
right ascension of ascending node: | 294.8951° |
argument of perigee: | 10.1043° |
revolutions per day: | 13.53104768 |
mean anomaly at epoch: | 350.3232° |
orbit number at epoch: | 16267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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