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 36470U 93036BBV 24357.41265552 .00028855 00000-0 38388-2 0 9992
2 36470 73.8546 255.5628 0042359 156.4301 203.8828 14.78959964607951
Epoch (UTC): | 22 December 2024 09:54:13 |
Eccentricity: | 0.0042359 |
inclination: | 73.8546° |
perigee height: | 603 km |
apogee height: | 662 km |
right ascension of ascending node: | 255.5628° |
argument of perigee: | 156.4301° |
revolutions per day: | 14.78959964 |
mean anomaly at epoch: | 203.8828° |
orbit number at epoch: | 60795 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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