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 24305U 96052B 24256.89469004 .00000223 00000-0 22179-3 0 9996
2 24305 82.9396 195.5879 0028719 239.2920 120.5405 13.73980513404411
Epoch (UTC): | 12 September 2024 21:28:21 |
Eccentricity: | 0.0028719 |
inclination: | 82.9396° |
perigee height: | 964 km |
apogee height: | 1006 km |
right ascension of ascending node: | 195.5879° |
argument of perigee: | 239.2920° |
revolutions per day: | 13.73980513 |
mean anomaly at epoch: | 120.5405° |
orbit number at epoch: | 40441 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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