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 44255U 19029W 19341.25001157 -.00027949 00000-0 -15925-2 0 9997
2 44255 53.0031 6.4468 0000822 151.0987 155.2983 15.12130796 29813
Epoch (UTC): | 07 December 2019 06:00:01 |
Eccentricity: | 0.0000822 |
inclination: | 53.0031° |
perigee height: | 529 km |
apogee height: | 530 km |
right ascension of ascending node: | 6.4468° |
argument of perigee: | 151.0987° |
revolutions per day: | 15.12130796 |
mean anomaly at epoch: | 155.2983° |
orbit number at epoch: | 2981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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