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 48244U 21031AL 24358.15438437 -.00000117 00000-0 -35077-3 0 9992
2 48244 87.8998 37.2820 0001714 102.9453 257.1868 13.14504791177166
Epoch (UTC): | 23 December 2024 03:42:18 |
Eccentricity: | 0.0001714 |
inclination: | 87.8998° |
perigee height: | 1204 km |
apogee height: | 1207 km |
right ascension of ascending node: | 37.2820° |
argument of perigee: | 102.9453° |
revolutions per day: | 13.14504791 |
mean anomaly at epoch: | 257.1868° |
orbit number at epoch: | 17716 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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