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 24316.56153444 .00001731 00000-0 90529-3 0 9995
2 00011 32.8675 128.0600 1453783 344.4313 11.5739 11.88906390466057
Epoch (UTC): | 11 November 2024 13:28:36 |
Eccentricity: | 0.1453783 |
inclination: | 32.8675° |
perigee height: | 552 km |
apogee height: | 2910 km |
right ascension of ascending node: | 128.0600° |
argument of perigee: | 344.4313° |
revolutions per day: | 11.88906390 |
mean anomaly at epoch: | 11.5739° |
orbit number at epoch: | 46605 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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