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 37224U 10062C 25140.44271687 .00002460 00000-0 25217-3 0 9990
2 37224 71.9714 248.3131 0012976 96.0506 264.2142 14.91369823 58046
Epoch (UTC): | 20 May 2025 10:37:30 |
Eccentricity: | 0.0012976 |
inclination: | 71.9714° |
perigee height: | 584 km |
apogee height: | 603 km |
right ascension of ascending node: | 248.3131° |
argument of perigee: | 96.0506° |
revolutions per day: | 14.91369823 |
mean anomaly at epoch: | 264.2142° |
orbit number at epoch: | 5804 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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