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 07530U 74089B 23333.85164090 -.00000033 00000-0 81720-4 0 9999
2 07530 101.9648 321.7463 0012387 106.2974 317.3005 12.53669718244177
Epoch (UTC): | 29 November 2023 20:26:21 |
Eccentricity: | 0.0012387 |
inclination: | 101.9648° |
perigee height: | 1439 km |
apogee height: | 1459 km |
right ascension of ascending node: | 321.7463° |
argument of perigee: | 106.2974° |
revolutions per day: | 12.53669718 |
mean anomaly at epoch: | 317.3005° |
orbit number at epoch: | 24417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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