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 24277.14709244 .00000326 00000-0 18805-3 0 9995
2 11608 81.2129 144.5218 0053053 234.9262 124.6925 14.06408481304619
Epoch (UTC): | 03 October 2024 03:31:48 |
Eccentricity: | 0.0053053 |
inclination: | 81.2129° |
perigee height: | 833 km |
apogee height: | 910 km |
right ascension of ascending node: | 144.5218° |
argument of perigee: | 234.9262° |
revolutions per day: | 14.06408481 |
mean anomaly at epoch: | 124.6925° |
orbit number at epoch: | 30461 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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