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 00016U 58002A 21112.61215679 .00000196 00000-0 29783-3 0 9994
2 00016 34.2660 342.1370 2025007 101.1942 282.1607 10.48712491491292
Epoch (UTC): | 22 April 2021 14:41:30 |
Eccentricity: | 0.2025007 |
inclination: | 34.2660° |
perigee height: | 653 km |
apogee height: | 4224 km |
right ascension of ascending node: | 342.1370° |
argument of perigee: | 101.1942° |
revolutions per day: | 10.48712491 |
mean anomaly at epoch: | 282.1607° |
orbit number at epoch: | 49129 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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