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 40911U 15049N 23092.17045444 .00022109 00000-0 86599-3 0 9993
2 40911 97.4939 99.9843 0013498 69.4659 354.7878 15.25722344416765
Epoch (UTC): | 02 April 2023 04:05:27 |
Eccentricity: | 0.0013498 |
inclination: | 97.4939° |
perigee height: | 479 km |
apogee height: | 498 km |
right ascension of ascending node: | 99.9843° |
argument of perigee: | 69.4659° |
revolutions per day: | 15.25722344 |
mean anomaly at epoch: | 354.7878° |
orbit number at epoch: | 41676 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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