CartoSat 2A, AAUsat 2, CanX-2, CanX-6 (NTS), Compass 1, CUTE-1.7+APD II, Delfi-C3, IMS-1, RUBIN-8, SEEDS 2


Launched: 28 April 2008
Site: Satish Dhawan Space Centre, Sriharikota, India
Launcher: PSLV-C

Name: CartoSat 2A
Orbit: LEO, apogee: 637 km, perigee: 637 km: polar orbit
International Number: 2008-021A
Owner: ISRO
Contractor: ISRO

Name: CanX-6 (NTS)
Orbit: LEO, apogee: 637 km, perigee: 637 km: polar orbit
International Number: 2008-021B
Owner: Com Dev
Contractor: University of Toronto Institute for Aerospace Studies Space Flight Laboratory (UTIAS/SFL)

Name: CUTE-1.7+APD II
Orbit: LEO, apogee: 637 km, perigee: 637 km: polar orbit
International Number: 2008-021C

Name: IMS-1
Orbit: LEO, apogee: 637 km, perigee: 637 km: polar orbit
International Number: 2008-021D
Owner: ISRO
Contractor: ISRO

Name: CanX-2
Orbit: LEO, apogee: 637 km, perigee: 637 km: polar orbit
International Number: 2008-021E

Name: AAUsat 2
Orbit: LEO, apogee: 637 km, perigee: 637 km: polar orbit
International Number: 2008-021F

Name: SEEDS 2
Orbit: LEO, apogee: 637 km, perigee: 637 km: polar orbit
International Number: 2008-021G

Name: Delfi-C3
Orbit: LEO, apogee: 637 km, perigee: 637 km: polar orbit
International Number: 2008-021H

Name: Compass 1
Orbit: LEO, apogee: 637 km, perigee: 637 km: polar orbit
International Number: 2008-021I

Name: RUBIN-8
Orbit: LEO, apogee: 637 km, perigee: 637 km: polar orbit
International Number: 2008-021J
Owner: Cosmos International
Contractor: Cosmos International

CartoSat 2A

CartoSat 2A is an Indian Earth observation satellite owned and operated by ISRO.

CartoSat 2A is a state-of-the art remote sensing satellite with a spatial resolution of about one metre and swath of 9.6 km. The satellite carries a panchromatic camera (PAN) capable of taking black-and-white pictures in the visible region of electromagnetic spectrum. The highly agile CartoSat 2A is steerable along as well as across the direction of its movement to facilitate imaging of any area more frequently.

High-resolution data from CartoSat 2A will be invaluable in urban and rural development applications calling for large scale mapping.

CanX-6 (NTS)

CanX-6 is a Canadian experimental satellite which will verify the performance of key elements of Com Dev's advanced space-based Automatic Identification System (AIS) systems solution which will be used to track ships across the world.

The mission will collect data that will validate key technology and performance characteristics of the AIS system, enabling design improvements to be incorporated into the final product. The mission will also provide information related to maritime vessel densities and distribution, which will be used to optimise any future constellation system design.

Com Dev remains on track to provide an advanced space-based AIS capability that exceeds the performance of any other commercial system. This capability will enhance maritime safety and security on a global scale. The AIS data transmitted by over 68,000 ships world-wide is now collected primarily from other ships and land-based receivers with a limited range of approximately 50 nautical miles. Com Dev has developed satellite payload technology to solve the traditional challenges associated with space-based collection of AIS data, and is committed to commercialising it following a series of tests.

IMS-1

IMS-1 is an Indian Earth observation satellite owned and operated by ISRO.

Indian Mini Satellite (IMS-1)was developed by ISRO for remote sensing applications. Weighing 83 kg at lift-off, IMS-1 carries two remote sensing payloads - A Multi-spectral camera (Mx Payload) and a Hyper-spectral camera (HySI Payload), operating in the visible and near infrared regions of the electromagnetic spectrum. The spatial resolution of Mx camera is 37 metre with a swath of 151 km while that of HySI is about 506 metre with a swath of about 130 km.

The data from this mission will be made available to interested space agencies and student community from developing countries to provide necessary impetus to capacity building in using satellite data. The versatile IMS-1 has been specifically developed to carry different payloads in future without significant changes in it and has a design life time of two years.

RUBIN-8

RUBIN-8 is a German experimental payload which remains attached to the upper stage of the launcher. It will test the communications systems for a maritime navigation system which will relay information via the Orbcomm system of satellites.

Nanosatellites

The remaining satellites placed in orbit were nanosatellites built mainly by universities as technology demonstrators.

(source: Com Dev, ISRO)




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