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 10521U 77119B 23028.12989662 .00000380 00000-0 12599-3 0 9992
2 10521 74.0265 70.6037 0022175 301.5559 58.3431 14.41034086367633
Epoch (UTC): | 28 January 2023 03:07:03 |
Eccentricity: | 0.0022175 |
inclination: | 74.0265° |
perigee height: | 739 km |
apogee height: | 771 km |
right ascension of ascending node: | 70.6037° |
argument of perigee: | 301.5559° |
revolutions per day: | 14.41034086 |
mean anomaly at epoch: | 58.3431° |
orbit number at epoch: | 36763 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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