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 23080.30611691 .00007150 00000-0 70857-3 0 9993
2 40032 97.9614 19.8360 0009598 214.9902 145.0687 14.92088222475388
Epoch (UTC): | 21 March 2023 07:20:48 |
Eccentricity: | 0.0009598 |
inclination: | 97.9614° |
perigee height: | 585 km |
apogee height: | 598 km |
right ascension of ascending node: | 19.8360° |
argument of perigee: | 214.9902° |
revolutions per day: | 14.92088222 |
mean anomaly at epoch: | 145.0687° |
orbit number at epoch: | 47538 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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