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 35869U 09049E 21015.88188626 -.00000015 00000-0 11828-4 0 9990
2 35869 98.4598 359.1614 0003475 293.1454 66.9358 14.22448126588206
Epoch (UTC): | 15 January 2021 21:09:54 |
Eccentricity: | 0.0003475 |
inclination: | 98.4598° |
perigee height: | 814 km |
apogee height: | 819 km |
right ascension of ascending node: | 359.1614° |
argument of perigee: | 293.1454° |
revolutions per day: | 14.22448126 |
mean anomaly at epoch: | 66.9358° |
orbit number at epoch: | 58820 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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