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 20929U 90095A 21015.73286018 -.00000225 00000-0 00000-0 0 9999
2 20929 15.1721 358.8488 0008677 28.6077 331.4594 0.98399027 5992
Epoch (UTC): | 15 January 2021 17:35:19 |
Eccentricity: | 0.0008677 |
inclination: | 15.1721° |
perigee height: | 36282 km |
apogee height: | 36356 km |
right ascension of ascending node: | 358.8488° |
argument of perigee: | 28.6077° |
revolutions per day: | 0.98399027 |
mean anomaly at epoch: | 331.4594° |
orbit number at epoch: | 599 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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