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 22177.91883106 .00011480 00000-0 40864-3 0 9994
2 39134 64.8626 30.8229 0034975 278.1058 81.6106 15.28745075508309
Epoch (UTC): | 26 June 2022 22:03:07 |
Eccentricity: | 0.0034975 |
inclination: | 64.8626° |
perigee height: | 455 km |
apogee height: | 503 km |
right ascension of ascending node: | 30.8229° |
argument of perigee: | 278.1058° |
revolutions per day: | 15.28745075 |
mean anomaly at epoch: | 81.6106° |
orbit number at epoch: | 50830 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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