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 48274U 21035A 23267.09533853 .00022985 00000-0 25063-3 0 9997
2 48274 41.4731 274.1029 0008013 96.5137 263.6615 15.62801436137292
Epoch (UTC): | 24 September 2023 02:17:17 |
Eccentricity: | 0.0008013 |
inclination: | 41.4731° |
perigee height: | 374 km |
apogee height: | 385 km |
right ascension of ascending node: | 274.1029° |
argument of perigee: | 96.5137° |
revolutions per day: | 15.62801436 |
mean anomaly at epoch: | 263.6615° |
orbit number at epoch: | 13729 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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