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 22178.75964735 .00005533 00000-0 22704-3 0 9991
2 47311 60.6857 323.4449 0018040 344.7235 15.3306 15.25445163 80035
Epoch (UTC): | 27 June 2022 18:13:53 |
Eccentricity: | 0.0018040 |
inclination: | 60.6857° |
perigee height: | 477 km |
apogee height: | 502 km |
right ascension of ascending node: | 323.4449° |
argument of perigee: | 344.7235° |
revolutions per day: | 15.25445163 |
mean anomaly at epoch: | 15.3306° |
orbit number at epoch: | 8003 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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