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 41334U 16010A 22127.25356700 0.00000000 00000-0 00000-0 0 08
2 41334 122.9964 225.0132 0004569 130.4891 229.5108 13.41448299 07
Epoch (UTC): | 07 May 2022 06:05:08 |
Eccentricity: | 0.0004569 |
inclination: | 122.9964° |
perigee height: | 1100 km |
apogee height: | 1107 km |
right ascension of ascending node: | 225.0132° |
argument of perigee: | 130.4891° |
revolutions per day: | 13.41448299 |
mean anomaly at epoch: | 229.5108° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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