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 55522U 22151XU 23333.45734689 .00011362 00000-0 34797-2 0 9995
2 55522 98.6649 345.0193 0104246 258.2083 100.7395 14.38788191 49506
Epoch (UTC): | 29 November 2023 10:58:34 |
Eccentricity: | 0.0104246 |
inclination: | 98.6649° |
perigee height: | 688 km |
apogee height: | 837 km |
right ascension of ascending node: | 345.0193° |
argument of perigee: | 258.2083° |
revolutions per day: | 14.38788191 |
mean anomaly at epoch: | 100.7395° |
orbit number at epoch: | 4950 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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