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 23035.80810273 .00004032 00000-0 20337-3 0 9999
2 53807 53.2061 318.2317 0013184 16.0465 344.0947 15.19307195 22316
Epoch (UTC): | 04 February 2023 19:23:40 |
Eccentricity: | 0.0013184 |
inclination: | 53.2061° |
perigee height: | 499 km |
apogee height: | 517 km |
right ascension of ascending node: | 318.2317° |
argument of perigee: | 16.0465° |
revolutions per day: | 15.19307195 |
mean anomaly at epoch: | 344.0947° |
orbit number at epoch: | 2231 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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