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DOVE 2

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DOVE 2 is classified as:


NORAD ID: 39132
Int'l Code: 2013-015C
Perigee: 474.0 km
Apogee: 503.7 km
Inclination: 64.9 °
Period: 94.2 minutes
Semi major axis: 6859 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   24289.66904670  .00028625  00000-0  10384-2 0  9992
2 39132  64.8715  16.4171 0021580 296.4617  63.4301 15.28027141632258
Source of the keplerian elements: AFSPC