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 53807U 22111AL 23332.47301643 .00008719 00000-0 37925-3 0 9995
2 53807 53.2353 40.7777 0010425 190.5145 169.5637 15.23002420 67464
Epoch (UTC): | 28 November 2023 11:21:08 |
Eccentricity: | 0.0010425 |
inclination: | 53.2353° |
perigee height: | 489 km |
apogee height: | 504 km |
right ascension of ascending node: | 40.7777° |
argument of perigee: | 190.5145° |
revolutions per day: | 15.23002420 |
mean anomaly at epoch: | 169.5637° |
orbit number at epoch: | 6746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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