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 24316.53574350 .00001602 00000-0 13372-2 0 9996
2 00082 38.8649 3.1318 1166720 286.4597 61.1198 12.27227937 5193
Epoch (UTC): | 11 November 2024 12:51:28 |
Eccentricity: | 0.1166720 |
inclination: | 38.8649° |
perigee height: | 635 km |
apogee height: | 2487 km |
right ascension of ascending node: | 3.1318° |
argument of perigee: | 286.4597° |
revolutions per day: | 12.27227937 |
mean anomaly at epoch: | 61.1198° |
orbit number at epoch: | 519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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