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 00050U 60009B 22147.26627544 -.00000100 00000-0 -15052-3 0 9991
2 00050 47.2323 81.3418 0114225 278.4589 80.3268 12.20121531756767
Epoch (UTC): | 27 May 2022 06:23:26 |
Eccentricity: | 0.0114225 |
inclination: | 47.2323° |
perigee height: | 1501 km |
apogee height: | 1683 km |
right ascension of ascending node: | 81.3418° |
argument of perigee: | 278.4589° |
revolutions per day: | 12.20121531 |
mean anomaly at epoch: | 80.3268° |
orbit number at epoch: | 75676 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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