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 10961U 78063A 24357.46258820 .00000426 00000-0 15126-3 0 9997
2 10961 74.0764 2.7391 0017531 296.6137 63.3220 14.37280202435096
Epoch (UTC): | 22 December 2024 11:06:07 |
Eccentricity: | 0.0017531 |
inclination: | 74.0764° |
perigee height: | 755 km |
apogee height: | 780 km |
right ascension of ascending node: | 2.7391° |
argument of perigee: | 296.6137° |
revolutions per day: | 14.37280202 |
mean anomaly at epoch: | 63.3220° |
orbit number at epoch: | 43509 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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