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 12835U 81091A 24358.14292427 .00000091 00000-0 78463-4 0 9993
2 12835 82.9190 217.1250 0027792 162.8342 311.9585 13.75583670171399
Epoch (UTC): | 23 December 2024 03:25:48 |
Eccentricity: | 0.0027792 |
inclination: | 82.9190° |
perigee height: | 959 km |
apogee height: | 1000 km |
right ascension of ascending node: | 217.1250° |
argument of perigee: | 162.8342° |
revolutions per day: | 13.75583670 |
mean anomaly at epoch: | 311.9585° |
orbit number at epoch: | 17139 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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