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 23439U 94085A 22135.84764149 -.00000037 00000-0 15882-3 0 9991
2 23439 64.8125 198.3491 0167640 278.1052 80.0882 11.27571737127819
Epoch (UTC): | 15 May 2022 20:20:36 |
Eccentricity: | 0.0167640 |
inclination: | 64.8125° |
perigee height: | 1881 km |
apogee height: | 2163 km |
right ascension of ascending node: | 198.3491° |
argument of perigee: | 278.1052° |
revolutions per day: | 11.27571737 |
mean anomaly at epoch: | 80.0882° |
orbit number at epoch: | 12781 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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