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 20438U 90005C 21023.58974559 -.00000003 00000-0 16452-4 0 9997
2 20438 98.8925 9.1628 0009687 350.4653 128.7451 14.31070417618328
Epoch (UTC): | 23 January 2021 14:09:14 |
Eccentricity: | 0.0009687 |
inclination: | 98.8925° |
perigee height: | 781 km |
apogee height: | 795 km |
right ascension of ascending node: | 9.1628° |
argument of perigee: | 350.4653° |
revolutions per day: | 14.31070417 |
mean anomaly at epoch: | 128.7451° |
orbit number at epoch: | 61832 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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