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 44742U 19074AF 21022.89454145 .00001868 00000-0 14192-3 0 9992
2 44742 52.9994 327.9394 0002011 49.2248 310.8915 15.07038459 66361
Epoch (UTC): | 22 January 2021 21:28:08 |
Eccentricity: | 0.0002011 |
inclination: | 52.9994° |
perigee height: | 544 km |
apogee height: | 546 km |
right ascension of ascending node: | 327.9394° |
argument of perigee: | 49.2248° |
revolutions per day: | 15.07038459 |
mean anomaly at epoch: | 310.8915° |
orbit number at epoch: | 6636 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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