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 13552U 82092A 23147.11839596 .00012170 00000-0 28721-3 0 9990
2 13552 82.5682 281.8096 0020998 315.2459 44.7092 15.41492060228729
Epoch (UTC): | 27 May 2023 02:50:29 |
Eccentricity: | 0.0020998 |
inclination: | 82.5682° |
perigee height: | 427 km |
apogee height: | 456 km |
right ascension of ascending node: | 281.8096° |
argument of perigee: | 315.2459° |
revolutions per day: | 15.41492060 |
mean anomaly at epoch: | 44.7092° |
orbit number at epoch: | 22872 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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