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 00005U 58002B 25186.42991674 -.00000037 00000-0 -29307-4 0 9991
2 00005 34.2485 304.5890 1841335 15.0409 349.8185 10.85926411405583
Epoch (UTC): | 05 July 2025 10:19:04 |
Eccentricity: | 0.1841335 |
inclination: | 34.2485° |
perigee height: | 649 km |
apogee height: | 3822 km |
right ascension of ascending node: | 304.5890° |
argument of perigee: | 15.0409° |
revolutions per day: | 10.85926411 |
mean anomaly at epoch: | 349.8185° |
orbit number at epoch: | 40558 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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