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 22176.47229279 .00011151 00000-0 33139-3 0 9996
2 41557 97.3879 274.1823 0010113 357.7186 130.9901 15.34884196338610
Epoch (UTC): | 25 June 2022 11:20:06 |
Eccentricity: | 0.0010113 |
inclination: | 97.3879° |
perigee height: | 454 km |
apogee height: | 468 km |
right ascension of ascending node: | 274.1823° |
argument of perigee: | 357.7186° |
revolutions per day: | 15.34884196 |
mean anomaly at epoch: | 130.9901° |
orbit number at epoch: | 33861 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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