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 00020U 59007A 21022.69391846 .00000111 00000-0 43674-4 0 9997
2 00020 33.3461 120.9737 1666067 349.7577 7.2682 11.55793486255979
Epoch (UTC): | 22 January 2021 16:39:14 |
Eccentricity: | 0.1666067 |
inclination: | 33.3461° |
perigee height: | 508 km |
apogee height: | 3262 km |
right ascension of ascending node: | 120.9737° |
argument of perigee: | 349.7577° |
revolutions per day: | 11.55793486 |
mean anomaly at epoch: | 7.2682° |
orbit number at epoch: | 25597 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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