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 43017U 17073E 22179.44933681 .00002135 00000-0 16364-3 0 9996
2 43017 97.6747 73.1942 0249149 151.5336 209.9751 14.81449835248741
Epoch (UTC): | 28 June 2022 10:47:02 |
Eccentricity: | 0.0249149 |
inclination: | 97.6747° |
perigee height: | 450 km |
apogee height: | 799 km |
right ascension of ascending node: | 73.1942° |
argument of perigee: | 151.5336° |
revolutions per day: | 14.81449835 |
mean anomaly at epoch: | 209.9751° |
orbit number at epoch: | 24874 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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