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 24298U 96051B 24310.57968474 -.00000004 00000-0 24407-4 0 9992
2 24298 70.7869 130.0223 0013987 141.1039 219.1090 14.12456256452584
Epoch (UTC): | 05 November 2024 13:54:44 |
Eccentricity: | 0.0013987 |
inclination: | 70.7869° |
perigee height: | 841 km |
apogee height: | 861 km |
right ascension of ascending node: | 130.0223° |
argument of perigee: | 141.1039° |
revolutions per day: | 14.12456256 |
mean anomaly at epoch: | 219.1090° |
orbit number at epoch: | 45258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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