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 23334.82643908 .00009596 00000-0 87712-3 0 9992
2 40032 97.9853 277.8633 0012040 96.8574 263.4016 14.95182618513370
Epoch (UTC): | 30 November 2023 19:50:04 |
Eccentricity: | 0.0012040 |
inclination: | 97.9853° |
perigee height: | 573 km |
apogee height: | 590 km |
right ascension of ascending node: | 277.8633° |
argument of perigee: | 96.8574° |
revolutions per day: | 14.95182618 |
mean anomaly at epoch: | 263.4016° |
orbit number at epoch: | 51337 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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