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 19257U 88053B 24310.42374281 .00001534 00000-0 50975-3 0 9991
2 19257 74.0462 293.9943 0021384 238.4866 233.9638 14.38446120906230
Epoch (UTC): | 05 November 2024 10:10:11 |
Eccentricity: | 0.0021384 |
inclination: | 74.0462° |
perigee height: | 748 km |
apogee height: | 779 km |
right ascension of ascending node: | 293.9943° |
argument of perigee: | 238.4866° |
revolutions per day: | 14.38446120 |
mean anomaly at epoch: | 233.9638° |
orbit number at epoch: | 90623 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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