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 24312.54714669 .00001894 00000-0 15739-2 0 9994
2 00082 38.8653 17.9232 1166831 267.1978 79.4893 12.27213704 4705
Epoch (UTC): | 07 November 2024 13:07:53 |
Eccentricity: | 0.1166831 |
inclination: | 38.8653° |
perigee height: | 635 km |
apogee height: | 2487 km |
right ascension of ascending node: | 17.9232° |
argument of perigee: | 267.1978° |
revolutions per day: | 12.27213704 |
mean anomaly at epoch: | 79.4893° |
orbit number at epoch: | 470 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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