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 00046U 60007B 24317.86277690 .00002238 00000-0 43913-3 0 9993
2 00046 66.6919 11.2103 0198739 7.6237 352.7815 14.52945926372481
Epoch (UTC): | 12 November 2024 20:42:23 |
Eccentricity: | 0.0198739 |
inclination: | 66.6919° |
perigee height: | 575 km |
apogee height: | 857 km |
right ascension of ascending node: | 11.2103° |
argument of perigee: | 7.6237° |
revolutions per day: | 14.52945926 |
mean anomaly at epoch: | 352.7815° |
orbit number at epoch: | 37248 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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