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 23345.20307307 .00004140 00000-0 18665-3 0 9997
2 53807 53.2417 342.3906 0008999 231.4171 128.6022 15.23187605 69406
Epoch (UTC): | 11 December 2023 04:52:25 |
Eccentricity: | 0.0008999 |
inclination: | 53.2417° |
perigee height: | 490 km |
apogee height: | 502 km |
right ascension of ascending node: | 342.3906° |
argument of perigee: | 231.4171° |
revolutions per day: | 15.23187605 |
mean anomaly at epoch: | 128.6022° |
orbit number at epoch: | 6940 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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