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 03081U 67127A 22228.72586633 -.00000059 00000-0 23359-4 0 9992
2 03081 65.1448 345.6912 0040309 243.7364 115.9558 13.93236480778462
Epoch (UTC): | 16 August 2022 17:25:14 |
Eccentricity: | 0.0040309 |
inclination: | 65.1448° |
perigee height: | 888 km |
apogee height: | 947 km |
right ascension of ascending node: | 345.6912° |
argument of perigee: | 243.7364° |
revolutions per day: | 13.93236480 |
mean anomaly at epoch: | 115.9558° |
orbit number at epoch: | 77846 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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