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 15333U 84106A 22230.33722979 -.00000226 00000-0 -93540-4 0 9992
2 15333 71.0254 98.3718 0020973 217.4222 142.5441 14.14145806954949
Epoch (UTC): | 18 August 2022 08:05:36 |
Eccentricity: | 0.0020973 |
inclination: | 71.0254° |
perigee height: | 830 km |
apogee height: | 860 km |
right ascension of ascending node: | 98.3718° |
argument of perigee: | 217.4222° |
revolutions per day: | 14.14145806 |
mean anomaly at epoch: | 142.5441° |
orbit number at epoch: | 95494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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