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 37159U 10045B 23147.59235341 .00162614 -32999-6 73454-3 0 9999
2 37159 31.8650 221.0079 4327502 254.0123 55.3687 7.00345893190396
Epoch (UTC): | 27 May 2023 14:12:59 |
Eccentricity: | 0.4327502 |
inclination: | 31.8650° |
perigee height: | 168 km |
apogee height: | 10155 km |
right ascension of ascending node: | 221.0079° |
argument of perigee: | 254.0123° |
revolutions per day: | 7.00345893 |
mean anomaly at epoch: | 55.3687° |
orbit number at epoch: | 19039 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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