DOVE 2

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10-day predictions
DOVE 2 is classified as:

Experimental

NORAD ID: 39132

Int'l Code: 2013-015C

Perigee: 499.6 km

Apogee: 516.0 km

Inclination: 64.9 °

Period: 94.6 minutes

Semi major axis: 6878 km

RCS: 0.053 m² (small)

Launch date: April 19, 2013
Source: United States (US)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)

The DOVE 2 mission is a technology demonstration nanosatellite for Cosmogia Inc. for remote sensing purposes based on the triple CubeSat form factor.

1 39132U 13015C   24139.75083299  .00020712  00000-0  91445-3 0  9998
2 39132  64.8692 145.0963 0011940 292.6968  67.2898 15.21726364609406

Source of the keplerian elements: AFSPC