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 25137.42427056 .00003391 00000-0 34524-3 0 9992
2 37224 71.9717 255.1248 0013051 102.7375 257.5254 14.91354686 57597
Epoch (UTC): | 17 May 2025 10:10:56 |
Eccentricity: | 0.0013051 |
inclination: | 71.9717° |
perigee height: | 584 km |
apogee height: | 603 km |
right ascension of ascending node: | 255.1248° |
argument of perigee: | 102.7375° |
revolutions per day: | 14.91354686 |
mean anomaly at epoch: | 257.5254° |
orbit number at epoch: | 5759 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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