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 23086.81082536 .00006123 00000-0 60607-3 0 9996
2 40032 97.9613 26.4085 0010219 192.7652 167.3309 14.92196152475832
Epoch (UTC): | 27 March 2023 19:27:35 |
Eccentricity: | 0.0010219 |
inclination: | 97.9613° |
perigee height: | 584 km |
apogee height: | 598 km |
right ascension of ascending node: | 26.4085° |
argument of perigee: | 192.7652° |
revolutions per day: | 14.92196152 |
mean anomaly at epoch: | 167.3309° |
orbit number at epoch: | 47583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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