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 24318.06578838 .00000955 00000-0 32065-3 0 9999
2 19257 74.0466 279.9172 0021125 223.0980 207.3283 14.38466288907613
Epoch (UTC): | 13 November 2024 01:34:44 |
Eccentricity: | 0.0021125 |
inclination: | 74.0466° |
perigee height: | 748 km |
apogee height: | 778 km |
right ascension of ascending node: | 279.9172° |
argument of perigee: | 223.0980° |
revolutions per day: | 14.38466288 |
mean anomaly at epoch: | 207.3283° |
orbit number at epoch: | 90761 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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