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 41459U 16025D 23083.51605120 .00038048 00000-0 12535-2 0 9994
2 41459 98.1927 276.5424 0117660 33.0738 327.7848 15.24854915379974
Epoch (UTC): | 24 March 2023 12:23:06 |
Eccentricity: | 0.0117660 |
inclination: | 98.1927° |
perigee height: | 410 km |
apogee height: | 572 km |
right ascension of ascending node: | 276.5424° |
argument of perigee: | 33.0738° |
revolutions per day: | 15.24854915 |
mean anomaly at epoch: | 327.7848° |
orbit number at epoch: | 37997 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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