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 20580U 90037B 21023.58407407 .00000519 00000-0 20500-4 0 9993
2 20580 28.4702 303.5690 0002485 303.4704 62.1921 15.09540399489193
Epoch (UTC): | 23 January 2021 14:01:04 |
Eccentricity: | 0.0002485 |
inclination: | 28.4702° |
perigee height: | 536 km |
apogee height: | 539 km |
right ascension of ascending node: | 303.5690° |
argument of perigee: | 303.4704° |
revolutions per day: | 15.09540399 |
mean anomaly at epoch: | 62.1921° |
orbit number at epoch: | 48919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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