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 44881U 19093C 23337.54389813 .00002024 00000-0 25495-3 0 9992
2 44881 97.8487 53.0411 0013325 243.0887 116.8966 14.83047521213895
Epoch (UTC): | 03 December 2023 13:03:12 |
Eccentricity: | 0.0013325 |
inclination: | 97.8487° |
perigee height: | 610 km |
apogee height: | 629 km |
right ascension of ascending node: | 53.0411° |
argument of perigee: | 243.0887° |
revolutions per day: | 14.83047521 |
mean anomaly at epoch: | 116.8966° |
orbit number at epoch: | 21389 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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