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 00005U 58002B 23087.84133674 .00000139 00000-0 14897-3 0 9991
2 00005 34.2614 342.9389 1846876 237.8293 102.9902 10.85075563315438
Epoch (UTC): | 28 March 2023 20:11:31 |
Eccentricity: | 0.1846876 |
inclination: | 34.2614° |
perigee height: | 648 km |
apogee height: | 3832 km |
right ascension of ascending node: | 342.9389° |
argument of perigee: | 237.8293° |
revolutions per day: | 10.85075563 |
mean anomaly at epoch: | 102.9902° |
orbit number at epoch: | 31543 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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