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 23087U 94023A 22224.78570700 -.00000093 00000-0 -24031-4 0 9992
2 23087 71.0534 24.0111 0010459 229.1429 130.8787 14.13870652460336
Epoch (UTC): | 12 August 2022 18:51:25 |
Eccentricity: | 0.0010459 |
inclination: | 71.0534° |
perigee height: | 838 km |
apogee height: | 854 km |
right ascension of ascending node: | 24.0111° |
argument of perigee: | 229.1429° |
revolutions per day: | 14.13870652 |
mean anomaly at epoch: | 130.8787° |
orbit number at epoch: | 46033 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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