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 40552U 15020A 23341.50672106 .00000008 00000-0 -11729-4 0 9997
2 40552 82.4862 245.8449 0015378 215.4254 144.5806 12.42889729394119
Epoch (UTC): | 07 December 2023 12:09:40 |
Eccentricity: | 0.0015378 |
inclination: | 82.4862° |
perigee height: | 1482 km |
apogee height: | 1506 km |
right ascension of ascending node: | 245.8449° |
argument of perigee: | 215.4254° |
revolutions per day: | 12.42889729 |
mean anomaly at epoch: | 144.5806° |
orbit number at epoch: | 39411 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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