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 3230U 68040B 25189.15940968 .00002175 00000-0 17168-3 0 9994
2 3230 74.0326 92.4961 0025482 334.4942 25.4986 15.01195982 74537
Epoch (UTC): | 08 July 2025 03:49:32 |
Eccentricity: | 0.0025482 |
inclination: | 74.0326° |
perigee height: | 545 km |
apogee height: | 581 km |
right ascension of ascending node: | 92.4961° |
argument of perigee: | 334.4942° |
revolutions per day: | 15.01195982 |
mean anomaly at epoch: | 25.4986° |
orbit number at epoch: | 7453 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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