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 25544U 98067A 23345.00370002 .00009797 00000-0 17741-3 0 9994
2 25544 51.6402 172.7364 0001393 16.7918 82.9368 15.50320011429210
Epoch (UTC): | 11 December 2023 00:05:19 |
Eccentricity: | 0.0001393 |
inclination: | 51.6402° |
perigee height: | 415 km |
apogee height: | 417 km |
right ascension of ascending node: | 172.7364° |
argument of perigee: | 16.7918° |
revolutions per day: | 15.50320011 |
mean anomaly at epoch: | 82.9368° |
orbit number at epoch: | 42921 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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