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 47311U 21002C 22228.30231829 .00007084 00000-0 28058-3 0 9990
2 47311 60.6846 136.8162 0027172 21.0378 339.1822 15.26082324 87595
Epoch (UTC): | 16 August 2022 07:15:20 |
Eccentricity: | 0.0027172 |
inclination: | 60.6846° |
perigee height: | 469 km |
apogee height: | 506 km |
right ascension of ascending node: | 136.8162° |
argument of perigee: | 21.0378° |
revolutions per day: | 15.26082324 |
mean anomaly at epoch: | 339.1822° |
orbit number at epoch: | 8759 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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