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 22348U 92093AM 24358.15581821 .00001012 00000-0 58630-3 0 9994
2 22348 71.2588 239.4120 0103445 136.9727 19.0317 14.08473338637441
Epoch (UTC): | 23 December 2024 03:44:22 |
Eccentricity: | 0.0103445 |
inclination: | 71.2588° |
perigee height: | 789 km |
apogee height: | 939 km |
right ascension of ascending node: | 239.4120° |
argument of perigee: | 136.9727° |
revolutions per day: | 14.08473338 |
mean anomaly at epoch: | 19.0317° |
orbit number at epoch: | 63744 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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