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 34846U 93036ABQ 23333.43470648 .00003929 00000-0 12532-2 0 9994
2 34846 74.0339 205.5670 0028688 98.1588 262.2823 14.39833855766631
Epoch (UTC): | 29 November 2023 10:25:58 |
Eccentricity: | 0.0028688 |
inclination: | 74.0339° |
perigee height: | 738 km |
apogee height: | 779 km |
right ascension of ascending node: | 205.5670° |
argument of perigee: | 98.1588° |
revolutions per day: | 14.39833855 |
mean anomaly at epoch: | 262.2823° |
orbit number at epoch: | 76663 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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