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 23090.17888692 .00040914 00000-0 11948-2 0 9997
2 47311 60.6839 357.5130 0029596 133.7018 226.6534 15.34626160122308
Epoch (UTC): | 31 March 2023 04:17:35 |
Eccentricity: | 0.0029596 |
inclination: | 60.6839° |
perigee height: | 442 km |
apogee height: | 482 km |
right ascension of ascending node: | 357.5130° |
argument of perigee: | 133.7018° |
revolutions per day: | 15.34626160 |
mean anomaly at epoch: | 226.6534° |
orbit number at epoch: | 12230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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