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 23337.39461807 .00008026 00000-0 34927-3 0 9990
2 53807 53.2383 18.2062 0009968 205.2835 154.7677 15.23101058 68215
Epoch (UTC): | 03 December 2023 09:28:15 |
Eccentricity: | 0.0009968 |
inclination: | 53.2383° |
perigee height: | 489 km |
apogee height: | 503 km |
right ascension of ascending node: | 18.2062° |
argument of perigee: | 205.2835° |
revolutions per day: | 15.23101058 |
mean anomaly at epoch: | 154.7677° |
orbit number at epoch: | 6821 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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