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 41604U 16040F 25131.82490932 .00029560 00000-0 36056-3 0 9990
2 41604 97.0882 160.7145 0003029 274.7238 85.3674 15.60429138495013
Epoch (UTC): | 11 May 2025 19:47:52 |
Eccentricity: | 0.0003029 |
inclination: | 97.0882° |
perigee height: | 384 km |
apogee height: | 388 km |
right ascension of ascending node: | 160.7145° |
argument of perigee: | 274.7238° |
revolutions per day: | 15.60429138 |
mean anomaly at epoch: | 85.3674° |
orbit number at epoch: | 49501 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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