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 20571U 90034B 24287.56790666 .00008935 00000-0 12411-2 0 9995
2 20571 22.7493 9.0996 0483087 211.8992 145.1327 14.18404369770938
Epoch (UTC): | 13 October 2024 13:37:47 |
Eccentricity: | 0.0483087 |
inclination: | 22.7493° |
perigee height: | 482 km |
apogee height: | 1179 km |
right ascension of ascending node: | 9.0996° |
argument of perigee: | 211.8992° |
revolutions per day: | 14.18404369 |
mean anomaly at epoch: | 145.1327° |
orbit number at epoch: | 77093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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