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 00046U 60007B 21016.55946885 -.00000030 00000-0 17251-4 0 9997
2 00046 66.6889 190.7035 0213896 330.6464 28.2761 14.49358964169998
Epoch (UTC): | 16 January 2021 13:25:38 |
Eccentricity: | 0.0213896 |
inclination: | 66.6889° |
perigee height: | 576 km |
apogee height: | 880 km |
right ascension of ascending node: | 190.7035° |
argument of perigee: | 330.6464° |
revolutions per day: | 14.49358964 |
mean anomaly at epoch: | 28.2761° |
orbit number at epoch: | 16999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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