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 44725C 19074N 21016.81454036 .00003400 00000-0 22792-3 0 166
2 44725 53.0580 356.7091 0001601 61.3651 7.7209 15.06380602 13
Epoch (UTC): | 16 January 2021 19:32:56 |
Eccentricity: | 0.0001601 |
inclination: | 53.0580° |
perigee height: | 546 km |
apogee height: | 548 km |
right ascension of ascending node: | 356.7091° |
argument of perigee: | 61.3651° |
revolutions per day: | 15.06380602 |
mean anomaly at epoch: | 7.7209° |
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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