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 20580U 90037B 23272.44218154 .00005751 00000-0 29673-3 0 9997
2 20580 28.4694 293.8532 0002616 74.0641 33.5155 15.14196740637274
Epoch (UTC): | 29 September 2023 10:36:44 |
Eccentricity: | 0.0002616 |
inclination: | 28.4694° |
perigee height: | 521 km |
apogee height: | 525 km |
right ascension of ascending node: | 293.8532° |
argument of perigee: | 74.0641° |
revolutions per day: | 15.14196740 |
mean anomaly at epoch: | 33.5155° |
orbit number at epoch: | 63727 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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