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 42832U 17042H 24284.44583129 .00015669 00000-0 12685-2 0 9990
2 42832 97.3870 100.8004 0013320 48.3378 311.8984 14.99746935394513
Epoch (UTC): | 10 October 2024 10:41:59 |
Eccentricity: | 0.0013320 |
inclination: | 97.3870° |
perigee height: | 558 km |
apogee height: | 577 km |
right ascension of ascending node: | 100.8004° |
argument of perigee: | 48.3378° |
revolutions per day: | 14.99746935 |
mean anomaly at epoch: | 311.8984° |
orbit number at epoch: | 39451 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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