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 13154U 82039B 25197.89699965 .00002371 00000-0 14937-3 0 9991
2 13154 81.1838 127.0057 0032080 11.4744 348.7204 15.08373870346071
Epoch (UTC): | 16 July 2025 21:31:40 |
Eccentricity: | 0.0032080 |
inclination: | 81.1838° |
perigee height: | 519 km |
apogee height: | 563 km |
right ascension of ascending node: | 127.0057° |
argument of perigee: | 11.4744° |
revolutions per day: | 15.08373870 |
mean anomaly at epoch: | 348.7204° |
orbit number at epoch: | 34607 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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