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 32376U 07059A 19348.45263376 -.00000339 00000-0 -36070-4 0 9990
2 32376 97.8827 169.3105 0001232 96.3275 263.8090 14.82156720650026
Epoch (UTC): | 14 December 2019 10:51:47 |
Eccentricity: | 0.0001232 |
inclination: | 97.8827° |
perigee height: | 621 km |
apogee height: | 623 km |
right ascension of ascending node: | 169.3105° |
argument of perigee: | 96.3275° |
revolutions per day: | 14.82156720 |
mean anomaly at epoch: | 263.8090° |
orbit number at epoch: | 65002 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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