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 60235U 24128A 24307.06341367 .00009198 00000-0 81902-3 0 9999
2 60235 61.9939 124.3231 0025626 339.9415 20.0663 14.96372586 17237
Epoch (UTC): | 02 November 2024 01:31:18 |
Eccentricity: | 0.0025626 |
inclination: | 61.9939° |
perigee height: | 560 km |
apogee height: | 596 km |
right ascension of ascending node: | 124.3231° |
argument of perigee: | 339.9415° |
revolutions per day: | 14.96372586 |
mean anomaly at epoch: | 20.0663° |
orbit number at epoch: | 1723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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