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 21021.73127598 -.00000260 00000-0 -10782-3 0 9999
2 19650 71.0009 130.9170 0015338 333.2411 26.7918 14.15799741662058
Epoch (UTC): | 21 January 2021 17:33:02 |
Eccentricity: | 0.0015338 |
inclination: | 71.0009° |
perigee height: | 828 km |
apogee height: | 850 km |
right ascension of ascending node: | 130.9170° |
argument of perigee: | 333.2411° |
revolutions per day: | 14.15799741 |
mean anomaly at epoch: | 26.7918° |
orbit number at epoch: | 66205 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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