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 24310.60498270 .00008233 00000-0 73339-3 0 9993
2 60235 61.9949 112.0955 0026293 341.6744 18.3394 14.96443281 17761
Epoch (UTC): | 05 November 2024 14:31:10 |
Eccentricity: | 0.0026293 |
inclination: | 61.9949° |
perigee height: | 559 km |
apogee height: | 596 km |
right ascension of ascending node: | 112.0955° |
argument of perigee: | 341.6744° |
revolutions per day: | 14.96443281 |
mean anomaly at epoch: | 18.3394° |
orbit number at epoch: | 1776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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