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 38341U 12025E 25192.56574384 .00001704 00000-0 16642-3 0 9994
2 38341 98.4376 136.3331 0046883 22.2409 338.0828 14.93134839712294
Epoch (UTC): | 11 July 2025 13:34:40 |
Eccentricity: | 0.0046883 |
inclination: | 98.4376° |
perigee height: | 555 km |
apogee height: | 621 km |
right ascension of ascending node: | 136.3331° |
argument of perigee: | 22.2409° |
revolutions per day: | 14.93134839 |
mean anomaly at epoch: | 338.0828° |
orbit number at epoch: | 71229 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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