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 21016.40822287 .00000069 00000-0 12643-3 0 9999
2 00016 34.2580 259.8649 2022426 55.5675 321.9878 10.48689296481199
Epoch (UTC): | 16 January 2021 09:47:50 |
Eccentricity: | 0.2022426 |
inclination: | 34.2580° |
perigee height: | 655 km |
apogee height: | 4221 km |
right ascension of ascending node: | 259.8649° |
argument of perigee: | 55.5675° |
revolutions per day: | 10.48689296 |
mean anomaly at epoch: | 321.9878° |
orbit number at epoch: | 48119 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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