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 48274U 21035A 24282.82642207 .00046973 00000-0 47892-3 0 9997
2 48274 41.4658 110.0263 0003261 159.8914 200.2055 15.64267061196870
Epoch (UTC): | 08 October 2024 19:50:02 |
Eccentricity: | 0.0003261 |
inclination: | 41.4658° |
perigee height: | 373 km |
apogee height: | 377 km |
right ascension of ascending node: | 110.0263° |
argument of perigee: | 159.8914° |
revolutions per day: | 15.64267061 |
mean anomaly at epoch: | 200.2055° |
orbit number at epoch: | 19687 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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