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 15331U 84105A 22140.52288318 .00005399 00000-0 28127-3 0 9996
2 15331 82.5380 0.8500 0013672 183.6912 176.4222 15.15716476 53648
Epoch (UTC): | 20 May 2022 12:32:57 |
Eccentricity: | 0.0013672 |
inclination: | 82.5380° |
perigee height: | 509 km |
apogee height: | 528 km |
right ascension of ascending node: | 0.8500° |
argument of perigee: | 183.6912° |
revolutions per day: | 15.15716476 |
mean anomaly at epoch: | 176.4222° |
orbit number at epoch: | 5364 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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