Official name RUBIN 9.1/RUBIN 9.2/PSLV
Alternative name PSLV fourth stage (PS4) (PSLV-CA)
Cospar ID 2009-051F
Norad ID 35936
Launch date 2009-09-23
Launch site SRI
Launch vehicle PSLV-CA
Country/Organization Germany, Luxembourg
Type application Technology, traffic monitoring
Operator LuxSpace (#9.1), OHB-System (#9.2)
RCS size LARGE
Decay date ON ORBIT
Period (min) 99.82
Inclination (deg) 98.27
Perigee (km) 712
Apogee (km) 788
Eccentricity 0.0506666666666667
Mean motion (revs. per day) 14.4259667401322
Semi-Major axis (km) 7128.135
Raan (deg) 62.3258
Arg of perigee (deg) 229.9484
Shape Cyl + Cyl + 2 Nozzle
Mass (kg) 920
Span (m^2) 3.238
Contractors LuxSpace (#9.1), OHB-System (#9.2)
Equipment 2 AIS-receivers
Configuration 2 payload modules bolted to PSLV upper stage
Power Solar cells, batteries

Rubin 9 consists of two payloads Rubin-9.1 and Rubin-9.2 weighing 8 kg each and will primarily be used for the Automatic Identification System (AIS) for Maritime applications. These are non-separable payloads that are mounted at an angle of 45° to the PSLV EB deck.

Rubin-9.1 (AIS-Pathfinder 2) is developed by LuxSpace, a daughter of OHB-System, and has a mission objective of providing an insight into the issue of message collisions that limit detection in areas of dense shipping.

The main purpose of the OHB-System developed Rubin-9.2 payload is to test and qualify nano technologies from Angstrom company Sweden and to continue space based maritime Automatic Identification System (AIS) receiver experiments (started with Rubin-7 and Rubin-8 missions). Rubin-9.2 is similar to the Rubin-8 launched on PSLV-C9 in April 2008.

Rubin-9 was successfully launched on 23 September 2009 on a PSLV-CA from India.

Satellite COSPAR Date LS Launch Vehicle Remarks
RUBIN 9.1/RUBIN 9.2/PSLV 2009-051F 2009-09-23 SRI PSLV-CA with Oceansat 2, BeeSat 1, SwissCube 1, UWE 2, ITÜ-pSat 1