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 39057U 13001A 23270.53234825 .00000066 00000-0 40595-3 0 9993
2 39057 82.4945 118.5549 0028227 33.3534 326.9317 12.42944103485269
Epoch (UTC): | 27 September 2023 12:46:34 |
Eccentricity: | 0.0028227 |
inclination: | 82.4945° |
perigee height: | 1472 km |
apogee height: | 1516 km |
right ascension of ascending node: | 118.5549° |
argument of perigee: | 33.3534° |
revolutions per day: | 12.42944103 |
mean anomaly at epoch: | 326.9317° |
orbit number at epoch: | 48526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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