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 21016.83052202 -.00000043 00000-0 39456-3 0 9990
2 00050 47.2289 179.0194 0113463 241.4364 117.4966 12.20114293696271
Epoch (UTC): | 16 January 2021 19:55:57 |
Eccentricity: | 0.0113463 |
inclination: | 47.2289° |
perigee height: | 1501 km |
apogee height: | 1682 km |
right ascension of ascending node: | 179.0194° |
argument of perigee: | 241.4364° |
revolutions per day: | 12.20114293 |
mean anomaly at epoch: | 117.4966° |
orbit number at epoch: | 69627 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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