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 7318U 74039A 23082.85894626 .00000031 00000-0 00000+0 0 9998
2 7318 4.9081 277.0592 0025855 292.8238 268.9564 1.01976543110080
Epoch (UTC): | 23 March 2023 20:36:52 |
Eccentricity: | 0.0025855 |
inclination: | 4.9081° |
perigee height: | 35207 km |
apogee height: | 35423 km |
right ascension of ascending node: | 277.0592° |
argument of perigee: | 292.8238° |
revolutions per day: | 1.01976543 |
mean anomaly at epoch: | 268.9564° |
orbit number at epoch: | 11008 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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