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 23159.38595012 .00014606 00000-0 34114-3 0 9993
2 13552 82.5692 269.3211 0020762 268.2502 91.6367 15.41818462 87395
Epoch (UTC): | 08 June 2023 09:15:46 |
Eccentricity: | 0.0020762 |
inclination: | 82.5692° |
perigee height: | 426 km |
apogee height: | 455 km |
right ascension of ascending node: | 269.3211° |
argument of perigee: | 268.2502° |
revolutions per day: | 15.41818462 |
mean anomaly at epoch: | 91.6367° |
orbit number at epoch: | 8739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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