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 23035.21605223 .00004269 00000-0 21441-3 0 9990
2 53807 53.2065 320.9331 0013209 14.1668 345.9696 15.19302099 22227
Epoch (UTC): | 04 February 2023 05:11:06 |
Eccentricity: | 0.0013209 |
inclination: | 53.2065° |
perigee height: | 499 km |
apogee height: | 517 km |
right ascension of ascending node: | 320.9331° |
argument of perigee: | 14.1668° |
revolutions per day: | 15.19302099 |
mean anomaly at epoch: | 345.9696° |
orbit number at epoch: | 2222 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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