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 23318U 94066B 23159.46916869 .00000489 00000-0 62407-4 0 9995
2 23318 82.5402 304.4558 0022044 292.9417 66.9469 14.79357004544929
Epoch (UTC): | 08 June 2023 11:15:36 |
Eccentricity: | 0.0022044 |
inclination: | 82.5402° |
perigee height: | 616 km |
apogee height: | 647 km |
right ascension of ascending node: | 304.4558° |
argument of perigee: | 292.9417° |
revolutions per day: | 14.79357004 |
mean anomaly at epoch: | 66.9469° |
orbit number at epoch: | 54492 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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