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 4783U 70102A 22229.17671400 .00000021 00000-0 45781-4 0 9997
2 4783 74.0329 174.3693 0030037 142.0964 218.2279 13.74829797593893
Epoch (UTC): | 17 August 2022 04:14:28 |
Eccentricity: | 0.0030037 |
inclination: | 74.0329° |
perigee height: | 960 km |
apogee height: | 1004 km |
right ascension of ascending node: | 174.3693° |
argument of perigee: | 142.0964° |
revolutions per day: | 13.74829797 |
mean anomaly at epoch: | 218.2279° |
orbit number at epoch: | 59389 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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