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 38272U 79095BS 24257.25162248 .00029653 00000-0 11768-1 0 9991
2 38272 81.2020 70.3024 0027133 106.7533 10.8184 14.28407531685156
Epoch (UTC): | 13 September 2024 06:02:20 |
Eccentricity: | 0.0027133 |
inclination: | 81.2020° |
perigee height: | 777 km |
apogee height: | 816 km |
right ascension of ascending node: | 70.3024° |
argument of perigee: | 106.7533° |
revolutions per day: | 14.28407531 |
mean anomaly at epoch: | 10.8184° |
orbit number at epoch: | 68515 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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