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 29047U 06011A 19053.31823326 -.00000026 00000-0 60085-5 0 9999
2 29047 71.9803 11.9387 0050383 174.3153 185.8566 14.28665287672625
Epoch (UTC): | 22 February 2019 07:38:15 |
Eccentricity: | 0.0050383 |
inclination: | 71.9803° |
perigee height: | 760 km |
apogee height: | 832 km |
right ascension of ascending node: | 11.9387° |
argument of perigee: | 174.3153° |
revolutions per day: | 14.28665287 |
mean anomaly at epoch: | 185.8566° |
orbit number at epoch: | 67262 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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