CCE 1 Rocket - 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 15202U 84088D   13167.97479632  .00000133  00000-0  37769-4 0  4889
2 15202 028.9212 333.9484 1993882 268.3758 292.3189 10.79875920135718
Epoch (UTC): 16 June 2013 23:23:42
Eccentricity: 0.1993882
inclination: 28.9212°
perigee height: 544 km
apogee height: 3992 km
right ascension of ascending node: 333.9484°
argument of perigee: 268.3758°
revolutions per day: 10.79875920
mean anomaly at epoch: 292.3189°
orbit number at epoch: 13571

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

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