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 23029.29542616 .00006299 00000-0 30958-3 0 9995
2 53807 53.2054 347.9491 0012887 356.4982 3.5923 15.19247872 21320
Epoch (UTC): | 29 January 2023 07:05:24 |
Eccentricity: | 0.0012887 |
inclination: | 53.2054° |
perigee height: | 499 km |
apogee height: | 517 km |
right ascension of ascending node: | 347.9491° |
argument of perigee: | 356.4982° |
revolutions per day: | 15.19247872 |
mean anomaly at epoch: | 3.5923° |
orbit number at epoch: | 2132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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