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 23152.43475365 .00000425 00000-0 53809-4 0 9992
2 23318 82.5396 310.9868 0022387 317.3089 42.6384 14.79350836543881
Epoch (UTC): | 01 June 2023 10:26:02 |
Eccentricity: | 0.0022387 |
inclination: | 82.5396° |
perigee height: | 615 km |
apogee height: | 647 km |
right ascension of ascending node: | 310.9868° |
argument of perigee: | 317.3089° |
revolutions per day: | 14.79350836 |
mean anomaly at epoch: | 42.6384° |
orbit number at epoch: | 54388 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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