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 23151.10030298 .00003892 00000-0 38024-3 0 9997
2 40032 97.9665 91.4392 0010608 358.6096 1.5091 14.92940390485940
Epoch (UTC): | 31 May 2023 02:24:26 |
Eccentricity: | 0.0010608 |
inclination: | 97.9665° |
perigee height: | 581 km |
apogee height: | 596 km |
right ascension of ascending node: | 91.4392° |
argument of perigee: | 358.6096° |
revolutions per day: | 14.92940390 |
mean anomaly at epoch: | 1.5091° |
orbit number at epoch: | 48594 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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