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 44767C 19074BG 21025.35301537 .00007966 00000-0 53372-3 0 257
2 44767 53.0583 338.3814 0002323 62.1263 346.9818 15.06388404 13
Epoch (UTC): | 25 January 2021 08:28:20 |
Eccentricity: | 0.0002323 |
inclination: | 53.0583° |
perigee height: | 545 km |
apogee height: | 549 km |
right ascension of ascending node: | 338.3814° |
argument of perigee: | 62.1263° |
revolutions per day: | 15.06388404 |
mean anomaly at epoch: | 346.9818° |
orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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