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 23335.83027407 .00009406 00000-0 85946-3 0 9991
2 40032 97.9852 278.8856 0011972 94.3648 265.8940 14.95199845513524
Epoch (UTC): | 01 December 2023 19:55:35 |
Eccentricity: | 0.0011972 |
inclination: | 97.9852° |
perigee height: | 573 km |
apogee height: | 590 km |
right ascension of ascending node: | 278.8856° |
argument of perigee: | 94.3648° |
revolutions per day: | 14.95199845 |
mean anomaly at epoch: | 265.8940° |
orbit number at epoch: | 51352 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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