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 23156.59514861 .00013775 00000-0 32258-3 0 9999
2 13552 82.5693 272.1619 0020714 278.9353 80.9549 15.41738687 86964
Epoch (UTC): | 05 June 2023 14:17:00 |
Eccentricity: | 0.0020714 |
inclination: | 82.5693° |
perigee height: | 427 km |
apogee height: | 455 km |
right ascension of ascending node: | 272.1619° |
argument of perigee: | 278.9353° |
revolutions per day: | 15.41738687 |
mean anomaly at epoch: | 80.9549° |
orbit number at epoch: | 8696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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