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 23149.84473986 .00012497 00000-0 29432-3 0 9991
2 13552 82.5678 279.0346 0020886 304.8528 55.0754 15.41558756 85926
Epoch (UTC): | 29 May 2023 20:16:25 |
Eccentricity: | 0.0020886 |
inclination: | 82.5678° |
perigee height: | 427 km |
apogee height: | 456 km |
right ascension of ascending node: | 279.0346° |
argument of perigee: | 304.8528° |
revolutions per day: | 15.41558756 |
mean anomaly at epoch: | 55.0754° |
orbit number at epoch: | 8592 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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