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DOVE 2

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DOVE 2 is classified as:


NORAD ID: 39132
Int'l Code: 2013-015C
Perigee: 539.3 km
Apogee: 564.0 km
Inclination: 64.9 °
Period: 95.5 minutes
Semi major axis: 6922 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   19143.62830186  .00000292  00000-0  31114-4 0  9997
2 39132  64.8766 197.6558 0017798 321.4800 118.5562 15.07285285334795
Source of the keplerian elements: AFSPC