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 34571U 93036VH 24276.41511822 .00031021 00000-0 10109-1 0 9995
2 34571 74.0455 273.5317 0079061 54.5117 306.3379 14.36749636809963
Epoch (UTC): | 02 October 2024 09:57:46 |
Eccentricity: | 0.0079061 |
inclination: | 74.0455° |
perigee height: | 713 km |
apogee height: | 826 km |
right ascension of ascending node: | 273.5317° |
argument of perigee: | 54.5117° |
revolutions per day: | 14.36749636 |
mean anomaly at epoch: | 306.3379° |
orbit number at epoch: | 80996 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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