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Introduction to RazakSAT (Malaysia's remote sensing satellite)

This article was written in collaboration with the Astronautic Technology (M) Sdn Bhd (Dr. Tuan Hj Norhizam Hamzah and Dr. Rosymah) and APRSAF secretariat.

RazakSAT (Fig. 1) is scheduled to be launched from Kwajalein Atoll, an island located in the Republic of the Marshall Islands, U.S.A. on July 14, 2009 using a Falcon 1 launcher developed by SpaceX. RazakSAT is a small Low Equatorial Orbit (LEO) satellite that carries the electro-optical payload of a Medium-sized Aperture Camera (MAC) - a pushbroom camera with 5 linear detectors (1 panchromatic, 4 multi-spectral).

RazakSAT was named after the second prime minister of Malaysia, Tun Abdul Razak (known as the Father of Malaysian Development) a moniker given to him by the former prime minister of Malaysia, Tun Mahathir Mohamad.

In order to acquire the most number of images for Malaysia and other countries in the equatorial belt (Table 1), the satellite will be launched in Near Equatorial Orbit (NEqO) with an inclination of 9属 (Fig. 2) and will have up to six opportunities a day to take images and overcome the major obstacle to passive remote sensing, namely, cloud cover. Another requirement for most remote sensing applications is access to high spatial resolution data. Driven by these requirements, the mission of RazakSAT is to provide a satellite with high re-visits and high-resolution data.

The specifications of RazakSAT are shown in Table 2.

To handle mission operations, there will be a new ground station in Sg. Lang, Banting under the control of the Malaysian National Space Agency (ANGKASA) and it will consists of a Mission Control Station (MCS) and an Image Receiving and Processing Station (IRPS). MCS will perform mission planning, command generation, telemetry reception, archiving and analysis. IRPS will archive images together with data on attitude and ephemeris telemetry for post-processing and distribution.

The images and data from RazakSAT will be received and distributed by the Malaysian Remote Sensing Agency (ARSM) ground station located in Temerloh, Pahang. In addition, other ground stations located in the NEqO will also be able to receive the images.

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Fig. 1 RazakSAT

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Fig. 2 Near Equatorial Orbit

Table 1 List of Countries Covered by NEqO (9o inclination)

Continent Countries
Asia India, Indonesia, Malaysia, Maldives, Philippines, Sri Lanka, Thailand
Africa Angola, Benin, Burundi, Cameroon, Central African Republic, Chad, Cote d'Ivoire, Ethiopia, Gabon, Guinea, Kenya, Liberia, Nigeria, Rwanda, Sierra Leone, Somalia, Sudan, Tanzania, Uganda, Zaire
Latin America Brazil, Colombia, Ecuador, French Guiana, Guyana, Panama, Peru, Surinam, Venezuela

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Table 2 Key Technical Features of RazakSAT

Subsystems Key Features
Orbit 685 km Near Equatorial
Inclination 9 degrees
Payload (MAC) GSD: 2.5 m (PAN), 5 m (MS)
Swathwidth: 20 km
Electrical Power Subsystem
(EPS)
GaAs/Ge solar cells on honeycomb substrate
NiCd batteries (18 Ahr)
Constant current control
Solar Power: 330 W @ EOL
Command and Data Handling Subsystem (C&DH) Two on-board computers
Telemetry and command interface modules
Analog Telemetry channels: up to 90
Digital Telemetry channels: up to 120
Telecommunication Subsystem (TS) 9600 bps/1200 bps S-band TT&C uplink
38.4 kbps/9600 bps/1200 bps S-band TT&C downlink
Payload Data Management 32 Gbits On-board solid-state memory
30 Mbps X-band payload data downlink
Structure and Thermal Control F1200 ' 1200 mm Hexagonal shape
Mass: less than 200 kg
Modular structure
Passive and Active thermal control
Mission Life 3 years

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