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 00082U 61004B 24306.93104096 .00002306 00000-0 19126-2 0 9990
2 00082 38.8638 38.7490 1166542 240.0720 107.9130 12.27189690 4010
Epoch (UTC): | 01 November 2024 22:20:41 |
Eccentricity: | 0.1166542 |
inclination: | 38.8638° |
perigee height: | 635 km |
apogee height: | 2487 km |
right ascension of ascending node: | 38.7490° |
argument of perigee: | 240.0720° |
revolutions per day: | 12.27189690 |
mean anomaly at epoch: | 107.9130° |
orbit number at epoch: | 401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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