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 19210U 88050A 23089.64104917 .00006047 00000-0 37602-3 0 9996
2 19210 82.5129 142.0785 0015092 264.0224 95.9285 15.09376249874694
Epoch (UTC): | 30 March 2023 15:23:06 |
Eccentricity: | 0.0015092 |
inclination: | 82.5129° |
perigee height: | 527 km |
apogee height: | 548 km |
right ascension of ascending node: | 142.0785° |
argument of perigee: | 264.0224° |
revolutions per day: | 15.09376249 |
mean anomaly at epoch: | 95.9285° |
orbit number at epoch: | 87469 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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