DOVE 2

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10-day predictions
DOVE 2 is classified as:

Experimental

NORAD ID: 39132

Int'l Code: 2013-015C

Perigee: 391.9 km

Apogee: 424.5 km

Inclination: 64.9 °

Period: 92.6 minutes

Semi major axis: 6779 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.

1 39132U 13015C   25338.65011720  .00080802  00000-0  11580-2 0  9996
2 39132  64.8624  69.2160 0024055 269.0011  90.8378 15.55369503696186

Source of the keplerian elements: AFSPC