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 35933U 09051C 23083.57719415 .00002310 00000-0 51980-3 0 9995
2 35933 98.5272 313.2943 0004590 283.9894 76.0793 14.57427255717047
Epoch (UTC): | 24 March 2023 13:51:09 |
Eccentricity: | 0.0004590 |
inclination: | 98.5272° |
perigee height: | 698 km |
apogee height: | 705 km |
right ascension of ascending node: | 313.2943° |
argument of perigee: | 283.9894° |
revolutions per day: | 14.57427255 |
mean anomaly at epoch: | 76.0793° |
orbit number at epoch: | 71704 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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