DOVE 2

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10-day predictions
DOVE 2 is classified as:

Experimental

NORAD ID: 39132

Int'l Code: 2013-015C

Perigee: 500.2 km

Apogee: 516.6 km

Inclination: 64.9 °

Period: 94.6 minutes

Semi major axis: 6879 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   24134.42716471  .00017405  00000-0  77487-3 0  9997
2 39132  64.8693 162.3789 0011896 292.2086  67.7780 15.21521466608592

Source of the keplerian elements: AFSPC