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 20718U 90063D 24357.43082215 .00002955 00000-0 35010-2 0 9994
2 20718 5.1268 232.6050 6082205 152.1846 261.3936 3.81116490401154
Epoch (UTC): | 22 December 2024 10:20:23 |
Eccentricity: | 0.6082205 |
inclination: | 5.1268° |
perigee height: | 404 km |
apogee height: | 21464 km |
right ascension of ascending node: | 232.6050° |
argument of perigee: | 152.1846° |
revolutions per day: | 3.81116490 |
mean anomaly at epoch: | 261.3936° |
orbit number at epoch: | 40115 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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