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 38735U 12041C 25137.87558595 .00000016 00000-0 44635-4 0 9997
2 38735 82.4747 321.1853 0017019 207.2673 152.7514 12.42631515580747
Epoch (UTC): | 17 May 2025 21:00:50 |
Eccentricity: | 0.0017019 |
inclination: | 82.4747° |
perigee height: | 1482 km |
apogee height: | 1509 km |
right ascension of ascending node: | 321.1853° |
argument of perigee: | 207.2673° |
revolutions per day: | 12.42631515 |
mean anomaly at epoch: | 152.7514° |
orbit number at epoch: | 58074 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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