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 35933U 09051C 24315.90983829 .00005032 00000-0 10636-2 0 9999
2 35933 98.4420 202.7824 0004184 231.5316 128.5508 14.59762915804027
Epoch (UTC): | 10 November 2024 21:50:10 |
Eccentricity: | 0.0004184 |
inclination: | 98.4420° |
perigee height: | 691 km |
apogee height: | 697 km |
right ascension of ascending node: | 202.7824° |
argument of perigee: | 231.5316° |
revolutions per day: | 14.59762915 |
mean anomaly at epoch: | 128.5508° |
orbit number at epoch: | 80402 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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