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 7648U 75011A 24337.22572470 -.00000227 00000-0 00000+0 0 9998
2 7648 6.8866 289.4013 0013999 264.3250 290.7551 0.99514340130144
Epoch (UTC): | 02 December 2024 05:25:02 |
Eccentricity: | 0.0013999 |
inclination: | 6.8866° |
perigee height: | 35940 km |
apogee height: | 36059 km |
right ascension of ascending node: | 289.4013° |
argument of perigee: | 264.3250° |
revolutions per day: | 0.99514340 |
mean anomaly at epoch: | 290.7551° |
orbit number at epoch: | 13014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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