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 25544U 98067A 24317.24127085 .00019805 00000-0 33684-3 0 9996
2 25544 51.6380 301.8966 0008444 165.9795 194.1431 15.51387213481518
Epoch (UTC): | 12 November 2024 05:47:25 |
Eccentricity: | 0.0008444 |
inclination: | 51.6380° |
perigee height: | 407 km |
apogee height: | 418 km |
right ascension of ascending node: | 301.8966° |
argument of perigee: | 165.9795° |
revolutions per day: | 15.51387213 |
mean anomaly at epoch: | 194.1431° |
orbit number at epoch: | 48151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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