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 40354U 14084B 23271.51517121 .00022135 00000-0 31060-3 0 9997
2 40354 74.7326 53.8766 0025518 356.9560 3.1501 15.56246563493466
Epoch (UTC): | 28 September 2023 12:21:50 |
Eccentricity: | 0.0025518 |
inclination: | 74.7326° |
perigee height: | 381 km |
apogee height: | 416 km |
right ascension of ascending node: | 53.8766° |
argument of perigee: | 356.9560° |
revolutions per day: | 15.56246563 |
mean anomaly at epoch: | 3.1501° |
orbit number at epoch: | 49346 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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