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 37152U 10043A 23084.47542729 .00000008 00000-0 -10207-4 0 9996
2 37152 82.4520 82.9498 0001601 143.3868 333.3071 12.42923037568992
Epoch (UTC): | 25 March 2023 11:24:36 |
Eccentricity: | 0.0001601 |
inclination: | 82.4520° |
perigee height: | 1493 km |
apogee height: | 1495 km |
right ascension of ascending node: | 82.9498° |
argument of perigee: | 143.3868° |
revolutions per day: | 12.42923037 |
mean anomaly at epoch: | 333.3071° |
orbit number at epoch: | 56899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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