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 28647U 05016B 22144.65527359 .00002263 00000-0 14257-3 0 9999
2 28647 56.9969 246.2912 0119922 340.9955 18.6627 15.07612955166383
Epoch (UTC): | 24 May 2022 15:43:35 |
Eccentricity: | 0.0119922 |
inclination: | 56.9969° |
perigee height: | 460 km |
apogee height: | 626 km |
right ascension of ascending node: | 246.2912° |
argument of perigee: | 340.9955° |
revolutions per day: | 15.07612955 |
mean anomaly at epoch: | 18.6627° |
orbit number at epoch: | 16638 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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