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 17974U 87041B 23151.60294347 -.00000095 00000-0 -23378-4 0 9998
2 17974 71.0089 8.2716 0015560 307.1652 118.8407 14.17358725864527
Epoch (UTC): | 31 May 2023 14:28:14 |
Eccentricity: | 0.0015560 |
inclination: | 71.0089° |
perigee height: | 823 km |
apogee height: | 845 km |
right ascension of ascending node: | 8.2716° |
argument of perigee: | 307.1652° |
revolutions per day: | 14.17358725 |
mean anomaly at epoch: | 118.8407° |
orbit number at epoch: | 86452 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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