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 22137.05247181 .00002920 00000-0 31009-3 0 9992
2 40032 97.9373 69.7120 0012272 151.0176 209.1725 14.89776548429469
Epoch (UTC): | 17 May 2022 01:15:33 |
Eccentricity: | 0.0012272 |
inclination: | 97.9373° |
perigee height: | 590 km |
apogee height: | 607 km |
right ascension of ascending node: | 69.7120° |
argument of perigee: | 151.0176° |
revolutions per day: | 14.89776548 |
mean anomaly at epoch: | 209.1725° |
orbit number at epoch: | 42946 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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