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 00011U 59001A 24306.89887056 .00002002 00000-0 10321-2 0 9996
2 00011 32.8746 164.5369 1454736 289.5957 55.3565 11.88868074464906
Epoch (UTC): | 01 November 2024 21:34:22 |
Eccentricity: | 0.1454736 |
inclination: | 32.8746° |
perigee height: | 551 km |
apogee height: | 2911 km |
right ascension of ascending node: | 164.5369° |
argument of perigee: | 289.5957° |
revolutions per day: | 11.88868074 |
mean anomaly at epoch: | 55.3565° |
orbit number at epoch: | 46490 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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