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 11788U 80034A 22181.58799472 -.00000056 00000-0 27309-4 0 9992
2 11788 64.8280 243.4373 0049021 333.3251 26.5291 13.92980862140173
Epoch (UTC): | 30 June 2022 14:06:42 |
Eccentricity: | 0.0049021 |
inclination: | 64.8280° |
perigee height: | 882 km |
apogee height: | 954 km |
right ascension of ascending node: | 243.4373° |
argument of perigee: | 333.3251° |
revolutions per day: | 13.92980862 |
mean anomaly at epoch: | 26.5291° |
orbit number at epoch: | 14017 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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