
CRS-1 successful, but the secondary payload was inserted into abnormally low orbit and lost due to Falcon 9 boost stage engine failure, ISS visiting vehicle safety rules, and the primary payload owner's contractual right to decline a second ignition of the second stage under some conditions.
Payloads
CRS-1
Type:
Dragon 1.0
Mass:
400 kg
Inclination Degree:
51.6539°
Customers:
NASA (CRS)
Manufacturers:
SpaceX
Nationalities:
United States
Orbcomm-OG2
Type:
Dragon 1.0
Mass:
400 kg
Inclination Degree:
45°
Customers:
Orbcomm