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 19650U 88102B 21025.68781815 -.00000318 00000-0 -13729-3 0 9993
2 19650 71.0005 122.5977 0015524 327.6921 32.3250 14.15797833662339
Epoch (UTC): | 25 January 2021 16:30:27 |
Eccentricity: | 0.0015524 |
inclination: | 71.0005° |
perigee height: | 828 km |
apogee height: | 851 km |
right ascension of ascending node: | 122.5977° |
argument of perigee: | 327.6921° |
revolutions per day: | 14.15797833 |
mean anomaly at epoch: | 32.3250° |
orbit number at epoch: | 66233 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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