deb Chang Zheng 4 - Orbit

View from above orbital plane
View from above orbital plane
View from above satellite
View from above satellite

Ground track
Ground track

The orbit data is extracted from the following two-line orbital elements,

1 20847U 90081K   13145.47599485  .00005950  00000-0  12577-2 0  7704
2 20847 098.5408 290.7639 0028531 058.6562 341.9791 14.59451478187541
Epoch (UTC): 25 May 2013 11:25:25
Eccentricity: 0.0028531
inclination: 98.5408°
perigee height: 675 km
apogee height: 715 km
right ascension of ascending node: 290.7639°
argument of perigee: 58.6562°
revolutions per day: 14.59451478
mean anomaly at epoch: 341.9791°
orbit number at epoch: 18754

The dashed part of the orbit path shows where the satellite is in the earth's shadow,  

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