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 25082.88220920 .00008856 00000-0 90179-3 0 9991
2 37224 71.9737 18.1639 0016371 211.1341 148.8859 14.90825884 49468
Epoch (UTC): | 23 March 2025 21:10:22 |
Eccentricity: | 0.0016371 |
inclination: | 71.9737° |
perigee height: | 584 km |
apogee height: | 607 km |
right ascension of ascending node: | 18.1639° |
argument of perigee: | 211.1341° |
revolutions per day: | 14.90825884 |
mean anomaly at epoch: | 148.8859° |
orbit number at epoch: | 4946 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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