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DOVE 2

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DOVE 2 is classified as:


NORAD ID: 39132
Int'l Code: 2013-015C
Perigee: 467.1 km
Apogee: 496.5 km
Inclination: 64.9 °
Period: 94.1 minutes
Semi major axis: 6852 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.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 39132U 13015C   24325.83423416  .00025225  00000-0  85252-3 0  9996
2 39132  64.8683 257.6319 0021409 294.2276  65.6619 15.30388084638343
Source of the keplerian elements: AFSPC