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 35824U 93036ASW 24355.27563158 .00003032 00000-0 20371-2 0 9992
2 35824 73.8457 302.4556 0254640 91.4797 271.5511 13.86562230792692
Epoch (UTC): | 20 December 2024 06:36:54 |
Eccentricity: | 0.0254640 |
inclination: | 73.8457° |
perigee height: | 754 km |
apogee height: | 1127 km |
right ascension of ascending node: | 302.4556° |
argument of perigee: | 91.4797° |
revolutions per day: | 13.86562230 |
mean anomaly at epoch: | 271.5511° |
orbit number at epoch: | 79269 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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