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 37227U 10062F 25143.79575667 .00001043 00000-0 13146-3 0 9993
2 37227 71.9667 285.7344 0013473 132.9535 227.2763 14.84210589308077
Epoch (UTC): | 23 May 2025 19:05:53 |
Eccentricity: | 0.0013473 |
inclination: | 71.9667° |
perigee height: | 606 km |
apogee height: | 625 km |
right ascension of ascending node: | 285.7344° |
argument of perigee: | 132.9535° |
revolutions per day: | 14.84210589 |
mean anomaly at epoch: | 227.2763° |
orbit number at epoch: | 30807 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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