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 23154.77780668 .00012494 00000-0 29299-3 0 9995
2 13552 82.5690 274.0120 0020725 285.9256 73.9707 15.41691313229906
Epoch (UTC): | 03 June 2023 18:40:02 |
Eccentricity: | 0.0020725 |
inclination: | 82.5690° |
perigee height: | 427 km |
apogee height: | 455 km |
right ascension of ascending node: | 274.0120° |
argument of perigee: | 285.9256° |
revolutions per day: | 15.41691313 |
mean anomaly at epoch: | 73.9707° |
orbit number at epoch: | 22990 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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