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 00047U 60007C 21057.67070777 .00000006 00000-0 26446-4 0 9992
2 00047 66.6656 195.2255 0220835 118.1871 244.1731 14.42134335171331
Epoch (UTC): | 26 February 2021 16:05:49 |
Eccentricity: | 0.0220835 |
inclination: | 66.6656° |
perigee height: | 594 km |
apogee height: | 909 km |
right ascension of ascending node: | 195.2255° |
argument of perigee: | 118.1871° |
revolutions per day: | 14.42134335 |
mean anomaly at epoch: | 244.1731° |
orbit number at epoch: | 17133 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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