THAICOM 2 (23314)

COSPAR: 1994-065B | Alt Name: Thaicom 2

Image
THAICOM 2 Satellite Image
Additional Sources
Launch Details

Launch Date

October 8, 1994

Launch Site

FRGUI

Launch Pad

ELA2

Launch Vehicle

Ariane 44L

Orbital Elements

NORAD ID

23314

International Designator

1994-065B

Epoch

Sat, 04 Jul 2026 03:52:14 GMT

Apogee

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Perigee

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Inclination

11.51°

Right Ascension

38.44°

Eccentricity

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Argument of Perigee

178.40°

Period

1445.98 min

Mean Motion

1.00 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

THAICOM 2

Alternative Name

Thaicom 2

Type

Payload

Status

Non-operational

Owner

SHINW

Country

Thailand

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 23314U 94065B   26185.16127712  .00000117  00000-0  00000-0 0  9995
2 23314  11.5061  38.4391 0001993 178.4030 175.4664  0.99586747 46538

Source: Celestrak

Summary
THAICOM 2 is a communication satellite with a NORAD catalog ID of 23314 and an object ID of 1994-065B. Launched on October 8, 1994, from the ELA2 launch pad at Kourou, French Guiana, using an Ariane 44L rocket, THAICOM 2 has a bus configuration and body of HS-376L. The satellite measures 6.7 meters in length with a diameter of 2.2 meters and a span of 6.7 meters. It has a dry mass of 402 kilograms and a launch mass of 596 kilograms, powered by solar cells and batteries. THAICOM 2's payload includes 2 (+1) Ku-band transponders and 10 (+2) C-band transponders for communication purposes. The satellite was manufactured by HSES with a planned lifetime of 13.5 years but reached an operational life of 16 years. Its shape is cylindrical, and it belongs to SHINW (Thaicom Public Company Limited).
Physical Characteristics

Length

6.7

Diameter

2.2

Span

6.7

Dry Mass

402

Launch Mass

596

Shape

Cyl

Radar Cross Section

1.3162

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Thaicom 2

Purpose

Communication

Mission

Communication

Manufacturer

HSES

Life Expectancy

13.5 years (planned), 16 years reached

Bus

HS-376L

Configuration

HS-376L

Motor

Star 30

Equipment

2 (+1) Ku-band transponders, 10 (+2) C-band transponders

Power System

Solar cells (body mounted and drop-skirt), batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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