We are excited to inform you of our upcoming relocation from Bandar Saujana Putra to a new and improved location at

Unit B2-20-1, Space U8 Mall,

Persiaran Pasak Bumi,

40150 Shah Alam,

Selangor Darul Ehsan,

Malaysia

This move is part of our ongoing commitment to enhancing the customer experience, offering improved accessibility and facilities. The effective date of this relocation is 1 November 2023, and our contact information, including updated phone numbers and email addresses, will remain unchanged. We appreciate your continued support and look forward to serving you from our new Shah Alam location. Should you have any questions or require further information, please don’t hesitate to contact our customer service team. Thank you for your cooperation, and we look forward to welcoming you at our new premises.

We are proudly inform that we are the authorized distributor for Göktürk-1 Image over Malaysia. Launched in December 2016, Göktürk-1 is a high-resolution optical satellite built by Telespazio for the Turkish Ministry of National Defense. The satellite has a wide range of military and civilian applications including reconnaissance, environmental monitoring, crop management, cadastral surveys, natural disaster damage assessment, and management of natural resources.

Mission Capabilities

Göktürk-1’s payload is HiRI (High Resolution Imager) of CNES (Centre National D’Etudes Spatiales), developed by Thales Alenia Space (TAS). The instrument is a pushbroom imager within the panchromatic and multispectral range with a high geo-location accuracy which has been developed from its use in the Pleiades satellite. HiRI onboard Göktürk-1 provides Turkey with high resolution optical reconnaissance as well as a wide range of civilian applications.

Performance Specifications

HiRI features a spatial resolution of 0.7 m and 2.8 m for the panchromatic (PAN) and multispectral (MS) bands, respectively. The imager has a swath width of 29 km at nadir with a 60° Field of Regard (FOR), and it is accurate to ±1 m with ground control points (GCP) and ±20 m without. Thanks to the satellite’s capability of imaging at angles of 30° to each side, a repeat cycle of approximately two days can be achieved over Turkish territory.

Göktürk-1 was launched into a sun-synchronous orbit at an altitude of 695 km at separation, inclined at 98.11°.

Space and Hardware Components

The satellite is based on the Proteus satellite bus developed by TAS and CNES, providing Göktürk-1 with a mass of 1060 kg and a design life of seven years. The Proteus satellite bus consists of an aluminium chassis with honeycomb panels mounted for the satellite’s subsystems. The spacecraft is three-axis stabilised, controlled by the ADCS (Attitude Determination and Control Subsystem), which includes star trackers, eight coarse sun sensors and two three-axis magnetometers; actuated by reaction wheels.

The communications subsystem is operated with S-band transceivers for data handling, which is then downlinked in X-band frequency.