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 51839U 22019R 24358.18124595 .00031262 00000-0 10932-2 0 9998
2 51839 97.4153 70.9436 0004346 312.5713 47.5160 15.29471563156227
Epoch (UTC): | 23 December 2024 04:20:59 |
Eccentricity: | 0.0004346 |
inclination: | 97.4153° |
perigee height: | 474 km |
apogee height: | 480 km |
right ascension of ascending node: | 70.9436° |
argument of perigee: | 312.5713° |
revolutions per day: | 15.29471563 |
mean anomaly at epoch: | 47.5160° |
orbit number at epoch: | 15622 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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