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 44715C 19074C 21016.82409289 -.00000122 00000-0 -81527-5 0 169
2 44715 53.0556 336.6632 0001852 75.4642 355.5369 15.06404786 18
Epoch (UTC): | 16 January 2021 19:46:41 |
Eccentricity: | 0.0001852 |
inclination: | 53.0556° |
perigee height: | 546 km |
apogee height: | 548 km |
right ascension of ascending node: | 336.6632° |
argument of perigee: | 75.4642° |
revolutions per day: | 15.06404786 |
mean anomaly at epoch: | 355.5369° |
orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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