Official name STUDSAT
Alternative name Studsat
Cospar ID 2010-035B
Norad ID 36796
Launch date 2010-07-12
Launch site SRI
Launch vehicle PSLV-CA
Country/Organization India
Type application Technology
Operator Team STUDSAT
RCS size SMALL
Decay date ON ORBIT
Period (min) 96.37
Inclination (deg) 98.17
Perigee (km) 576
Apogee (km) 593
Eccentricity 0.0145423438836612
Mean motion (revs. per day) 14.942409463526
Semi-Major axis (km) 6962.635
Raan (deg) 353.4254
Arg of perigee (deg) 34.2814
Shape Box
Mass (kg) 1
Height (m) 0.135
Width (m) 0.1
Depth (m) 0.135
Span (m^2) 0.135
Lifetime 6 months
Contractors Team STUDSAT
Equipment CMOS camera
Propulsion None
Configuration CubeSat (1U)
Power Solar cells, batteries

STUDSAT (Student Satellite) is a pico satellite conceptualized and currently being designed by undergraduate students across India. The mission is experimental in nature and the major objective is for the students to have a hands on experience on the design, fabrication and realization of a space mission at a minimum cost. The mission life is to be six months.

The uniqueness of this project is it has been initiated by students and managed mostly by students with support from Indian Space Research Organization and the Studsat consortium, which consists of seven Engineering colleges from Hyderabad and Bangalore, who formed as a team and signed an MOU among themselves in order to sponsor the project financially.

STUDSAT is built on a CubeSat 1U structure. The payload consists of a CMOS camera. The objective of this system is to obtain monochrome images of the Earth with resolution of 94 meters.

The satellite was successfully deployed in orbit, but no signals were received.

Satellite COSPAR Date LS Launch Vehicle Remarks
STUDSAT 2010-035B 2010-07-12 SRI PSLV-CA with Cartosat 2B, AlSat 2A, AISSat 1, TIsat 1