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 20104U 89050B 21060.47088773 -.00000066 00000-0 -81303-4 0 9995
2 20104 82.9526 247.3775 0043521 356.1081 3.9731 13.77324341590670
Epoch (UTC): | 01 March 2021 11:18:04 |
Eccentricity: | 0.0043521 |
inclination: | 82.9526° |
perigee height: | 941 km |
apogee height: | 1005 km |
right ascension of ascending node: | 247.3775° |
argument of perigee: | 356.1081° |
revolutions per day: | 13.77324341 |
mean anomaly at epoch: | 3.9731° |
orbit number at epoch: | 59067 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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