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 25732U 99025C 19348.87674535 -.00000037 +00000-0 +40640-5 0 9994
2 25732 098.9634 011.1448 0037659 020.8074 155.8703 14.17671023065529
Epoch (UTC): | 14 December 2019 21:02:30 |
Eccentricity: | 0.0037659 |
inclination: | 98.9634° |
perigee height: | 806 km |
apogee height: | 860 km |
right ascension of ascending node: | 11.1448° |
argument of perigee: | 20.8074° |
revolutions per day: | 14.17671023 |
mean anomaly at epoch: | 155.8703° |
orbit number at epoch: | 6552 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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