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 21017.51592498 -.00000029 00000-0 18556-4 0 9999
2 00047 66.6669 302.5929 0223622 148.2883 213.1921 14.42126174165545
Epoch (UTC): | 17 January 2021 12:22:55 |
Eccentricity: | 0.0223622 |
inclination: | 66.6669° |
perigee height: | 592 km |
apogee height: | 911 km |
right ascension of ascending node: | 302.5929° |
argument of perigee: | 148.2883° |
revolutions per day: | 14.42126174 |
mean anomaly at epoch: | 213.1921° |
orbit number at epoch: | 16554 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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