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 18096U 87049B 24358.08184360 .00000433 00000-0 15273-3 0 9995
2 18096 74.0401 221.0700 0020362 77.7314 282.6119 14.37576074966336
Epoch (UTC): | 23 December 2024 01:57:51 |
Eccentricity: | 0.0020362 |
inclination: | 74.0401° |
perigee height: | 752 km |
apogee height: | 781 km |
right ascension of ascending node: | 221.0700° |
argument of perigee: | 77.7314° |
revolutions per day: | 14.37576074 |
mean anomaly at epoch: | 282.6119° |
orbit number at epoch: | 96633 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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