|
NORAD ID: 31789
Int'l Code: 2007-028A
Perigee: 525.8 km
Apogee: 570.5 km
Inclination: 64.5 °
Period: 95.5 minutes
Semi major axis: 6919 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 13342.11005770 .00004631 00000-0 30460-3 0 7885
2 31789 064.5080 184.6353 0032233 218.3138 291.3211 15.08425608354147
Source: AFSPC
NASA's NSSDC Master Catalog entry for GENESIS 2
|
