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 29092U 06015A 21019.82111049 .00000024 00000-0 94540-5 0 9996
2 29092 97.9234 48.5775 0001395 92.7101 267.4272 14.83122359796800
Epoch (UTC): | 19 January 2021 19:42:23 |
Eccentricity: | 0.0001395 |
inclination: | 97.9234° |
perigee height: | 618 km |
apogee height: | 620 km |
right ascension of ascending node: | 48.5775° |
argument of perigee: | 92.7101° |
revolutions per day: | 14.83122359 |
mean anomaly at epoch: | 267.4272° |
orbit number at epoch: | 79680 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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