Similar to the process endured by Bigelow for
Genesis I, transporting
Genesis II to
Russia for launch was the end result of nearly a year of regulatory processes due to restrictions imposed by
International Traffic in Arms Regulations (ITAR) and other procedures, both in the
United States and abroad. After leaving
North Las Vegas, Nevada in the United States, the spacecraft made a stopover in
Luxembourg before being flown on an
Antonov An-124 to
Orsk, Russia, and transported over ground to the Dombarovskiy base.
Genesis II made its final move into the Assembly, Integration and Test Building on 29 March 2007. Originally slated for a 6 August 2006 launch,
ISC Kosmotras delayed the launch to 30 January 2007, due to the failure of a Dnepr rocket in July 2006. The launch was delayed an additional four times (1 April 2007, 19 April 2007, 26 April 2007, and 23 May 2007) due to technical and scheduling reasons before its eventual launch on 28 June 2007 at 15:02:20
UTC. As with
Genesis I, it was launched aboard an
ISC Kosmotras Dnepr rocket from
Dombarovsky Air Base near
Yasny, Orenburg Oblast, Russia. It successfully reached orbit after separation from the rocket at 15:16 UTC. Due to the mechanics of its orbit, first contact with the craft was established once it passed over
SpaceQuest, Ltd.'s
Fairfax, Virginia receiving station at 22:20 UTC, confirming that it was functioning nominally with power and air pressure at expected levels. Externally,
Genesis II is identical in size to
Genesis I; as such, it is a one-third scale of the full-size
BA 330 model, with on-orbit measurements of in length and in diameter, with an interior habitable volume of . As part of its inflatable design,
Genesis II launched with a diameter of , expanding to its full size after entering orbit. Within two days of launch, attitude control systems had damped all rotation and oriented antennae toward Earth. On 12 December 2007, Bigelow Aerospace provided an update indicating that
Genesis II was in good health. All cameras had been tested and more than 4,000 photographs had been taken. The craft was in a nearly circular orbit with an
eccentricity of 0.028, and had only lost from launch to that time.
Attitude control systems and all eight solar arrays were operational, and no damage to the outer surface of the craft was observed. Internal pressure was noted as holding between , with the variation caused by
Genesis II moving in and out of sunlight during its orbit. On 23 April 2009, Bigelow Aerospace announced that
Genesis II had surpassed the 10,000 orbit mark, having been in space for 665 days and travelling over . In February 2011, Bigelow reported that the vehicle had "performed flawlessly in terms of pressure maintenance and thermal control-environmental containment". Although the design life of the spacecraft avionics was only six months, the avionics systems worked flawlessly for over two and a half years before failure. The data received after the first six months was a re-verification of the validation test suite that was accomplished during the design life period. On 17 September 2019, an alert was generated by the
U.S. Air Force stating that there was a 5.6% chance that
Genesis II would collide with another
derelict satellite, the Soviet satellite
Kosmos 1300. == Systems ==