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 24278U 96046B 24316.25620682 .00000049 00000-0 84369-4 0 9992
2 24278 98.5848 231.6471 0350250 167.1744 193.8596 13.53221105394321
Epoch (UTC): | 11 November 2024 06:08:56 |
Eccentricity: | 0.0350250 |
inclination: | 98.5848° |
perigee height: | 800 km |
apogee height: | 1321 km |
right ascension of ascending node: | 231.6471° |
argument of perigee: | 167.1744° |
revolutions per day: | 13.53221105 |
mean anomaly at epoch: | 193.8596° |
orbit number at epoch: | 39432 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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