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DOVE 2

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DOVE 2 is classified as:


NORAD ID: 39132
Int'l Code: 2013-015C
Perigee: 549.1 km
Apogee: 554.8 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   19018.82238965  .00000069  00000-0  16288-4 0  9994
2 39132  64.8758 233.8684 0004134 306.6300 139.6458 15.07180249315981
Source of the keplerian elements: AFSPC