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 09062U 76078B 21023.62293250 -.00000056 00000-0 -70447-4 0 9991
2 09062 82.9305 46.2839 0029785 127.1487 350.5682 13.78419118236967
Epoch (UTC): | 23 January 2021 14:57:01 |
Eccentricity: | 0.0029785 |
inclination: | 82.9305° |
perigee height: | 947 km |
apogee height: | 991 km |
right ascension of ascending node: | 46.2839° |
argument of perigee: | 127.1487° |
revolutions per day: | 13.78419118 |
mean anomaly at epoch: | 350.5682° |
orbit number at epoch: | 23696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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