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 23160.74884814 .00013799 00000-0 32185-3 0 9994
2 13552 82.5689 267.9336 0020781 263.0324 96.8560 15.41857125 87604
Epoch (UTC): | 09 June 2023 17:58:20 |
Eccentricity: | 0.0020781 |
inclination: | 82.5689° |
perigee height: | 426 km |
apogee height: | 455 km |
right ascension of ascending node: | 267.9336° |
argument of perigee: | 263.0324° |
revolutions per day: | 15.41857125 |
mean anomaly at epoch: | 96.8560° |
orbit number at epoch: | 8760 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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