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 22141.75400150 .00004721 00000-0 49693-3 0 9990
2 40032 97.9365 74.4304 0012760 136.7294 223.4927 14.89813252429647
Epoch (UTC): | 21 May 2022 18:05:45 |
Eccentricity: | 0.0012760 |
inclination: | 97.9365° |
perigee height: | 589 km |
apogee height: | 607 km |
right ascension of ascending node: | 74.4304° |
argument of perigee: | 136.7294° |
revolutions per day: | 14.89813252 |
mean anomaly at epoch: | 223.4927° |
orbit number at epoch: | 42964 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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