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 24258.86787643 -.00000013 00000-0 83287-3 0 9993
2 23439 64.8136 258.7391 0147645 126.8186 234.6385 11.27578670223704
Epoch (UTC): | 14 September 2024 20:49:44 |
Eccentricity: | 0.0147645 |
inclination: | 64.8136° |
perigee height: | 1898 km |
apogee height: | 2146 km |
right ascension of ascending node: | 258.7391° |
argument of perigee: | 126.8186° |
revolutions per day: | 11.27578670 |
mean anomaly at epoch: | 234.6385° |
orbit number at epoch: | 22370 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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