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 19548U 88091B 18112.50303264 -.00000314 00000-0 00000+0 0 9997
2 19548 14.4383 4.8417 0038292 318.1712 6.2915 1.00276618 95506
Epoch (UTC): | 22 April 2018 12:04:22 |
Eccentricity: | 0.0038292 |
inclination: | 14.4383° |
perigee height: | 35623 km |
apogee height: | 35946 km |
right ascension of ascending node: | 4.8417° |
argument of perigee: | 318.1712° |
revolutions per day: | 1.00276618 |
mean anomaly at epoch: | 6.2915° |
orbit number at epoch: | 9550 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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