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 22145.56063458 .00001771 00000-0 21091-3 0 9992
2 38341 98.5078 359.3072 0055813 119.6709 241.0077 14.84679335542251
Epoch (UTC): | 25 May 2022 13:27:18 |
Eccentricity: | 0.0055813 |
inclination: | 98.5078° |
perigee height: | 575 km |
apogee height: | 653 km |
right ascension of ascending node: | 359.3072° |
argument of perigee: | 119.6709° |
revolutions per day: | 14.84679335 |
mean anomaly at epoch: | 241.0077° |
orbit number at epoch: | 54225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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