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 40032U 14033Y 23333.82259181 .00009071 00000-0 82981-3 0 9998
2 40032 97.9856 276.8410 0012102 99.8778 260.3808 14.95165031513222
Epoch (UTC): | 29 November 2023 19:44:31 |
Eccentricity: | 0.0012102 |
inclination: | 97.9856° |
perigee height: | 573 km |
apogee height: | 590 km |
right ascension of ascending node: | 276.8410° |
argument of perigee: | 99.8778° |
revolutions per day: | 14.95165031 |
mean anomaly at epoch: | 260.3808° |
orbit number at epoch: | 51322 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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