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 41557U 16033B 22135.84198060 .00013958 00000-0 42794-3 0 9999
2 41557 97.3857 233.5059 0012695 131.9546 344.3279 15.33809848332382
Epoch (UTC): | 15 May 2022 20:12:27 |
Eccentricity: | 0.0012695 |
inclination: | 97.3857° |
perigee height: | 456 km |
apogee height: | 473 km |
right ascension of ascending node: | 233.5059° |
argument of perigee: | 131.9546° |
revolutions per day: | 15.33809848 |
mean anomaly at epoch: | 344.3279° |
orbit number at epoch: | 33238 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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