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DOVE 2

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DOVE 2 is classified as:


NORAD ID: 39132
Int'l Code: 2013-015C
Perigee: 534.9 km
Apogee: 561.1 km
Inclination: 64.9 °
Period: 95.5 minutes
Semi major axis: 6919 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   22020.36029346  .00002566  00000-0  17490-3 0  9990
2 39132  64.8783 347.2020 0018923 318.7361 119.4501 15.08465520481444
Source of the keplerian elements: AFSPC