THEOS (33396)

COSPAR: 2008-049A | Alt Name: Thaichote

Image
THEOS Satellite Image
Additional Sources
Launch Details

Launch Date

October 1, 2008

Launch Site

DLS

Launch Pad

Sh370/13

Launch Vehicle

Dnepr

Orbital Elements

NORAD ID

33396

International Designator

2008-049A

Epoch

Sat, 04 Jul 2026 07:13:24 GMT

Apogee

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Perigee

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Inclination

98.56°

Right Ascension

242.03°

Eccentricity

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Argument of Perigee

84.13°

Period

101.40 min

Mean Motion

14.20 rev/day

Latitude

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Longitude

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Altitude

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Velocity

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Polar Plot
3D Visualization
Basic Satellite Info

Name

THEOS

Alternative Name

Thaichote

Type

Payload

Status

Operational

Owner

GISTDA

Country

Thailand

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 33396U 08049A   26185.30097606 -.00000015  00000-0  13029-4 0  9994
2 33396  98.5559 242.0286 0001150  84.1256 276.0052 14.20135053920393

Source: Celestrak

Summary
THEOS (Thaichote) is an Earth observation satellite with the NORAD catalog ID 33396 and OBJECT_ID 2008-049A. Launched on October 1, 2008, from Sh370/13 at DLS using a Dnepr launch vehicle, it was manufactured by ASTT for GISTDA. The satellite is equipped with a 2 m resolution black-and-white imager and a 15 m resolution panchromatic imager. It has dimensions of 2.4 meters in length, 2.1 meters in diameter, and spans 3 meters. Its dry mass is 670 kg, with a launch mass of 750 kg. THEOS uses hydrazine thrusters for propulsion and deployable fixed solar arrays along with batteries for power supply. The satellite’s configuration is Leostar-500-XO, and it has an estimated lifetime exceeding five years, with fuel allowing up to seven years of operation.
Physical Characteristics

Length

2.4

Diameter

2.1

Span

3

Dry Mass

670

Launch Mass

750

Shape

Hex Cyl + Pan

Radar Cross Section

2.8441

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

THEOS

Purpose

Earth observation

Mission

Earth observation

Manufacturer

ASTT

Life Expectancy

> 5 years; 7 years (fuel)

Bus

Astrosat-500

Configuration

Leostar-500-XO

Motor

Hydrazine thrusters

Equipment

2 m resolution black-and-white imager, 15 m resolution panchromatic imager

Power System

Deployable fixed solar array, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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