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 23705U 95058B 23155.40914697 .00000166 00000-0 10981-3 0 9995
2 23705 71.0206 138.7630 0013966 224.8140 135.1856 14.15234892425042
Epoch (UTC): | 04 June 2023 09:49:10 |
Eccentricity: | 0.0013966 |
inclination: | 71.0206° |
perigee height: | 831 km |
apogee height: | 851 km |
right ascension of ascending node: | 138.7630° |
argument of perigee: | 224.8140° |
revolutions per day: | 14.15234892 |
mean anomaly at epoch: | 135.1856° |
orbit number at epoch: | 42504 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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