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 19039U 88029B 24311.60309521 .00001391 00000-0 45302-3 0 9997
2 19039 74.0494 6.4154 0024238 232.5706 127.3243 14.39484342919032
Epoch (UTC): | 06 November 2024 14:28:27 |
Eccentricity: | 0.0024238 |
inclination: | 74.0494° |
perigee height: | 743 km |
apogee height: | 777 km |
right ascension of ascending node: | 6.4154° |
argument of perigee: | 232.5706° |
revolutions per day: | 14.39484342 |
mean anomaly at epoch: | 127.3243° |
orbit number at epoch: | 91903 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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