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 10962U 78063B 23147.77352935 .00000110 00000-0 41668-4 0 9991
2 10962 74.0774 170.9857 0026141 236.4563 123.4096 14.41594303358576
Epoch (UTC): | 27 May 2023 18:33:52 |
Eccentricity: | 0.0026141 |
inclination: | 74.0774° |
perigee height: | 734 km |
apogee height: | 772 km |
right ascension of ascending node: | 170.9857° |
argument of perigee: | 236.4563° |
revolutions per day: | 14.41594303 |
mean anomaly at epoch: | 123.4096° |
orbit number at epoch: | 35857 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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