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 39439U 13066Z 24277.89047939 .00054967 00000-0 36719-2 0 9994
2 39439 97.7232 241.0123 0042301 124.1064 236.4188 15.06037156587209
Epoch (UTC): | 03 October 2024 21:22:17 |
Eccentricity: | 0.0042301 |
inclination: | 97.7232° |
perigee height: | 519 km |
apogee height: | 577 km |
right ascension of ascending node: | 241.0123° |
argument of perigee: | 124.1064° |
revolutions per day: | 15.06037156 |
mean anomaly at epoch: | 236.4188° |
orbit number at epoch: | 58720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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