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 22178.55673089 .00010058 00000-0 29884-3 0 9996
2 41557 97.3886 276.2714 0009944 349.5743 129.5188 15.34921307338930
Epoch (UTC): | 27 June 2022 13:21:41 |
Eccentricity: | 0.0009944 |
inclination: | 97.3886° |
perigee height: | 454 km |
apogee height: | 468 km |
right ascension of ascending node: | 276.2714° |
argument of perigee: | 349.5743° |
revolutions per day: | 15.34921307 |
mean anomaly at epoch: | 129.5188° |
orbit number at epoch: | 33893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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