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 11608U 79095B 24284.54594505 .00000254 00000-0 14493-3 0 9998
2 11608 81.2116 137.3384 0053577 214.1434 145.6285 14.06411564305418
Epoch (UTC): | 10 October 2024 13:06:09 |
Eccentricity: | 0.0053577 |
inclination: | 81.2116° |
perigee height: | 833 km |
apogee height: | 910 km |
right ascension of ascending node: | 137.3384° |
argument of perigee: | 214.1434° |
revolutions per day: | 14.06411564 |
mean anomaly at epoch: | 145.6285° |
orbit number at epoch: | 30541 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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