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 25338U 98030A 23151.39102422 .00000242 00000-0 11898-3 0 9994
2 25338 98.6064 180.7344 0010402 10.0441 350.0945 14.26323889302861
Epoch (UTC): | 31 May 2023 09:23:04 |
Eccentricity: | 0.0010402 |
inclination: | 98.6064° |
perigee height: | 796 km |
apogee height: | 811 km |
right ascension of ascending node: | 180.7344° |
argument of perigee: | 10.0441° |
revolutions per day: | 14.26323889 |
mean anomaly at epoch: | 350.0945° |
orbit number at epoch: | 30286 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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