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GENESIS 2

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    GENESIS 2 can be found in the following categories:
    Experimental

    NORAD ID: 31789
    Int'l Code: 2007-028A
    Perigee: 528.5 km
    Apogee: 548.8 km
    Inclination: 64.5 °
    Period: 95.3 minutes
    Semi major axis: 6909 km
    Launch date: June 28, 2007
    Source: United States (US)
    Comments: Genesis II is the second experimental pathfinder spacecraft designed to test and confirm systems for future manned commercial space modules planned by Las Vegas-based Bigelow Aerospace The privately-funded space station module was launched atop a Dnepr rocket at 8:02 a.m. PDT from the ISC Kosmotras Yasny Cosmodrome, located in the Orenburg region of Russia, and was inserted into orbit at 8:16 a.m. PDT at an inclination of 64 degrees.

    Two Line Element Set (TLE):

    1 31789U 07028A   14330.80883750  .00006483  00000-0  39072-3 0  1059
    2 31789 064.5074 121.5601 0014687 333.9263 026.1116 15.11527358407542
    
    
    Source: AFSPC

    NASA's NSSDC Master Catalog entry for GENESIS 2

     
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