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 23157.39164737 .00024997 00000-0 65761-3 0 9998
2 47311 60.6811 100.0251 0014027 170.9721 189.1628 15.38434607132631
Epoch (UTC): | 06 June 2023 09:23:58 |
Eccentricity: | 0.0014027 |
inclination: | 60.6811° |
perigee height: | 441 km |
apogee height: | 460 km |
right ascension of ascending node: | 100.0251° |
argument of perigee: | 170.9721° |
revolutions per day: | 15.38434607 |
mean anomaly at epoch: | 189.1628° |
orbit number at epoch: | 13263 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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