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 38341U 12025E 22145.15626234 .00001701 00000-0 20296-3 0 9993
2 38341 98.5078 358.8758 0055808 120.9456 239.7258 14.84677403542275
Epoch (UTC): | 25 May 2022 03:45:01 |
Eccentricity: | 0.0055808 |
inclination: | 98.5078° |
perigee height: | 575 km |
apogee height: | 653 km |
right ascension of ascending node: | 358.8758° |
argument of perigee: | 120.9456° |
revolutions per day: | 14.84677403 |
mean anomaly at epoch: | 239.7258° |
orbit number at epoch: | 54227 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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