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 22179.54619317 .00004493 00000-0 18645-3 0 9995
2 47311 60.6859 320.4831 0018215 345.6741 14.3828 15.25452348 80159
Epoch (UTC): | 28 June 2022 13:06:31 |
Eccentricity: | 0.0018215 |
inclination: | 60.6859° |
perigee height: | 477 km |
apogee height: | 502 km |
right ascension of ascending node: | 320.4831° |
argument of perigee: | 345.6741° |
revolutions per day: | 15.25452348 |
mean anomaly at epoch: | 14.3828° |
orbit number at epoch: | 8015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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