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 19419U 88074A 23084.38295156 .00000170 00000-0 27846-3 0 9995
2 19419 90.0151 18.0872 0095339 198.8246 276.8533 13.42345167693395
Epoch (UTC): | 25 March 2023 09:11:27 |
Eccentricity: | 0.0095339 |
inclination: | 90.0151° |
perigee height: | 1029 km |
apogee height: | 1172 km |
right ascension of ascending node: | 18.0872° |
argument of perigee: | 198.8246° |
revolutions per day: | 13.42345167 |
mean anomaly at epoch: | 276.8533° |
orbit number at epoch: | 69339 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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