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 47311U 21002C 23081.18579507 .00032874 00000-0 98230-3 0 9996
2 47311 60.6838 31.8364 0031039 127.8718 232.5190 15.33951916120923
Epoch (UTC): | 22 March 2023 04:27:32 |
Eccentricity: | 0.0031039 |
inclination: | 60.6838° |
perigee height: | 443 km |
apogee height: | 485 km |
right ascension of ascending node: | 31.8364° |
argument of perigee: | 127.8718° |
revolutions per day: | 15.33951916 |
mean anomaly at epoch: | 232.5190° |
orbit number at epoch: | 12092 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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