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 20805U 90083B 23033.33162355 .00000092 00000-0 78630-4 0 9993
2 20805 82.9395 334.2149 0031856 51.2996 116.9296 13.75999959626143
Epoch (UTC): | 02 February 2023 07:57:32 |
Eccentricity: | 0.0031856 |
inclination: | 82.9395° |
perigee height: | 954 km |
apogee height: | 1001 km |
right ascension of ascending node: | 334.2149° |
argument of perigee: | 51.2996° |
revolutions per day: | 13.75999959 |
mean anomaly at epoch: | 116.9296° |
orbit number at epoch: | 62614 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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