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 22182.78859439 .00000787 00000-0 87527-4 0 9993
2 40032 97.9382 115.6272 0012092 15.4907 344.6678 14.89972136435755
Epoch (UTC): | 01 July 2022 18:55:34 |
Eccentricity: | 0.0012092 |
inclination: | 97.9382° |
perigee height: | 589 km |
apogee height: | 606 km |
right ascension of ascending node: | 115.6272° |
argument of perigee: | 15.4907° |
revolutions per day: | 14.89972136 |
mean anomaly at epoch: | 344.6678° |
orbit number at epoch: | 43575 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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