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 39134U 13015E 22179.88133904 .00006957 00000-0 25075-3 0 9996
2 39134 64.8622 24.3795 0035106 277.6327 82.0818 15.28777007508609
Epoch (UTC): | 28 June 2022 21:09:07 |
Eccentricity: | 0.0035106 |
inclination: | 64.8622° |
perigee height: | 455 km |
apogee height: | 503 km |
right ascension of ascending node: | 24.3795° |
argument of perigee: | 277.6327° |
revolutions per day: | 15.28777007 |
mean anomaly at epoch: | 82.0818° |
orbit number at epoch: | 50860 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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