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

0