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 21016.41003858 .00000067 00000-0 29272-4 0 9992
2 10521 74.0284 3.7716 0019801 54.9556 305.3453 14.40807879260541
Epoch (UTC): | 16 January 2021 09:50:27 |
Eccentricity: | 0.0019801 |
inclination: | 74.0284° |
perigee height: | 742 km |
apogee height: | 770 km |
right ascension of ascending node: | 3.7716° |
argument of perigee: | 54.9556° |
revolutions per day: | 14.40807879 |
mean anomaly at epoch: | 305.3453° |
orbit number at epoch: | 26054 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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