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 23439U 94085A 23266.09295391 -.00000037 00000-0 15214-3 0 9991
2 23439 64.8136 117.3423 0159504 192.8946 166.7874 11.27575651183657
Epoch (UTC): | 23 September 2023 02:13:51 |
Eccentricity: | 0.0159504 |
inclination: | 64.8136° |
perigee height: | 1888 km |
apogee height: | 2156 km |
right ascension of ascending node: | 117.3423° |
argument of perigee: | 192.8946° |
revolutions per day: | 11.27575651 |
mean anomaly at epoch: | 166.7874° |
orbit number at epoch: | 18365 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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