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 37855U 11061F 23341.13995665 .00038555 00000-0 85457-3 0 9992
2 37855 101.6967 42.2974 0093074 226.4547 132.8926 15.39131472663047
Epoch (UTC): | 07 December 2023 03:21:32 |
Eccentricity: | 0.0093074 |
inclination: | 101.6967° |
perigee height: | 385 km |
apogee height: | 512 km |
right ascension of ascending node: | 42.2974° |
argument of perigee: | 226.4547° |
revolutions per day: | 15.39131472 |
mean anomaly at epoch: | 132.8926° |
orbit number at epoch: | 66304 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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