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 23147.16452456 .00005175 00000-0 38927-3 0 9998
2 21393 24.9824 209.3773 0874443 332.6231 23.0683 13.59682794545088
Epoch (UTC): | 27 May 2023 03:56:54 |
Eccentricity: | 0.0874443 |
inclination: | 24.9824° |
perigee height: | 388 km |
apogee height: | 1685 km |
right ascension of ascending node: | 209.3773° |
argument of perigee: | 332.6231° |
revolutions per day: | 13.59682794 |
mean anomaly at epoch: | 23.0683° |
orbit number at epoch: | 54508 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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