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 23027.84496461 -.00115221 00000-0 -13566-2 0 9999
2 48274 41.4699 291.5042 0003086 37.7554 42.1941 15.60829393 99882
Epoch (UTC): | 27 January 2023 20:16:44 |
Eccentricity: | 0.0003086 |
inclination: | 41.4699° |
perigee height: | 383 km |
apogee height: | 387 km |
right ascension of ascending node: | 291.5042° |
argument of perigee: | 37.7554° |
revolutions per day: | 15.60829393 |
mean anomaly at epoch: | 42.1941° |
orbit number at epoch: | 9988 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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