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 21393U 91037B 22142.13110042 .00006141 00000-0 47907-3 0 9993
2 21393 24.9815 47.9849 0896385 147.0363 218.9380 13.54555124494792
Epoch (UTC): | 22 May 2022 03:08:47 |
Eccentricity: | 0.0896385 |
inclination: | 24.9815° |
perigee height: | 389 km |
apogee height: | 1722 km |
right ascension of ascending node: | 47.9849° |
argument of perigee: | 147.0363° |
revolutions per day: | 13.54555124 |
mean anomaly at epoch: | 218.9380° |
orbit number at epoch: | 49479 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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