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 116U 61015A 21113.19208846 -.00000053 00000-0 18490-4 0 9992
2 116 66.8090 171.0086 0072434 156.7224 203.7163 13.91788131 35416
Epoch (UTC): | 23 April 2021 04:36:36 |
Eccentricity: | 0.0072434 |
inclination: | 66.8090° |
perigee height: | 869 km |
apogee height: | 975 km |
right ascension of ascending node: | 171.0086° |
argument of perigee: | 156.7224° |
revolutions per day: | 13.91788131 |
mean anomaly at epoch: | 203.7163° |
orbit number at epoch: | 3541 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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