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 47504U 21006CV 24357.61161142 .00013437 00000-0 47811-3 0 9994
2 47504 97.1179 6.2433 0013437 272.4559 87.5143 15.28996844216863
Epoch (UTC): | 22 December 2024 14:40:43 |
Eccentricity: | 0.0013437 |
inclination: | 97.1179° |
perigee height: | 469 km |
apogee height: | 488 km |
right ascension of ascending node: | 6.2433° |
argument of perigee: | 272.4559° |
revolutions per day: | 15.28996844 |
mean anomaly at epoch: | 87.5143° |
orbit number at epoch: | 21686 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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