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 23156.89344361 .00000100 00000-0 76078-4 0 9992
2 23705 71.0208 135.6482 0013899 222.9506 137.0533 14.15235479425253
Epoch (UTC): | 05 June 2023 21:26:33 |
Eccentricity: | 0.0013899 |
inclination: | 71.0208° |
perigee height: | 831 km |
apogee height: | 851 km |
right ascension of ascending node: | 135.6482° |
argument of perigee: | 222.9506° |
revolutions per day: | 14.15235479 |
mean anomaly at epoch: | 137.0533° |
orbit number at epoch: | 42525 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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