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DOVE 2

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DOVE 2 is classified as:


NORAD ID: 39132
Int'l Code: 2013-015C
Perigee: 522.0 km
Apogee: 567.6 km
Inclination: 64.9 °
Period: 95.4 minutes
Semi major axis: 6915 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   22185.46588826  .00001336  00000-0  93495-4 0  9990
2 39132  64.8727 181.6138 0033000 294.2011 225.7966 15.09517175506354
Source of the keplerian elements: AFSPC