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 40032U 14033Y 24357.85335472 .00012589 00000-0 91590-3 0 9990
2 40032 98.0232 316.1602 0007984 201.8467 158.2418 15.03930944570975
Epoch (UTC): | 22 December 2024 20:28:49 |
Eccentricity: | 0.0007984 |
inclination: | 98.0232° |
perigee height: | 549 km |
apogee height: | 560 km |
right ascension of ascending node: | 316.1602° |
argument of perigee: | 201.8467° |
revolutions per day: | 15.03930944 |
mean anomaly at epoch: | 158.2418° |
orbit number at epoch: | 57097 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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