RazakSAT
Specifications
The major specification of RazakSAT, as provided by the satellites' builder and operator (ATSB) in February 2010, are:

RazakSAT

Section Title: Specifications
Table Section Text: The major specification of RazakSAT, as provided by the satellites' builder and operator (ATSB) in February 2010, are:

Subsystems	Specifications

Altitude	685 km

Inclination	9°

Payload (MAC)	GSD : 2.5 m (PAN), 5 m (MS) Swathwidth : 20 km @ 685 km

Attitude Determination & Control Subsystem (ADCS)	Three-axis stabilization based on four reaction wheels Pointing Accuracy : < 0.2° (2 s) Pointing Knowledge : 1 arcmin (2 s)

Electrical Power Subsystem (EPS)	GaAs/Ge solar cells on honeycomb substrate NiCd batteries (18 Ahr) Peak Power Tracking (PPT) & constant current control Solar Power : >300 W @ EOL

Command & 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)	9,600 bit/s / 1,200 bit/s S-band TT&C uplink 38.4 kbs / 9,600 bit/s / 1,200 bit/s S-band TT&C downlink

Payload Data Management	32 Gbit On-board solid-state memory 30 Mbit/s X band payload data downlink

Structure & Thermal	Ø1,200 × 1,200 mm Hexagonal shape Mass : 180 kg Modular structure Passive & Active thermal control

Mission Lifetime	3 Years

Sentence(s)

The altitude of RazakSAT is 685 km and has an inclination of 9 degrees.

final_sentence: The altitude of RazakSAT is 685 km and has an inclination of 9 degrees.