INSAT-2DT (ARABSAT-1C) (21894)

COSPAR: 1992-010B | Alt Name: Arabsat 1C

Image
INSAT-2DT (ARABSAT-1C) Satellite Image
Additional Sources
Launch Details

Launch Date

February 26, 1992

Launch Site

FRGUI

Launch Pad

ELA2

Launch Vehicle

Ariane 44L

Orbital Elements

NORAD ID

21894

International Designator

1992-010B

Epoch

Fri, 03 Jul 2026 22:05:30 GMT

Apogee

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Perigee

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Inclination

14.37°

Right Ascension

11.53°

Eccentricity

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Argument of Perigee

280.01°

Period

1459.17 min

Mean Motion

0.99 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

INSAT-2DT (ARABSAT-1C)

Alternative Name

Arabsat 1C

Type

Payload

Status

Non-operational

Owner

ARAB

Country

Arabsat

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 21894U 92010B   26184.92049162 -.00000259  00000-0  00000-0 0  9997
2 21894  14.3661  11.5291 0027487 280.0093 115.9203  0.98686455124410

Source: Celestrak

Summary
INSAT-2DT (ARABSAT-1C), also known as Arabsat 1C, is a communication satellite designed and built by AESPC/LOR. Launched on February 26, 1992, from the ELA2 launch pad at Guiana Space Centre using an Ariane 44L rocket, it reached stable orbit one day later on February 27, 1992. The satellite has a configuration based on the Spacebus-1000 platform and measures 2.3 meters in length, with a diameter of 1.5 meters and a span of 20.7 meters when its solar arrays are deployed. Equipped with 25 C-band transponders and 2 S-band transponders for communication services, it has a dry mass of 600 kilograms and launched with a total mass of 1310 kilograms. The satellite is powered by two deployable solar arrays and batteries, with its mission duration estimated at seven years. It was owned by ARAB and operated primarily for communication purposes.
Physical Characteristics

Length

2.3

Diameter

1.5

Span

20.7

Dry Mass

600

Launch Mass

1310

Shape

Box + 2 Pan

Radar Cross Section

2.5119

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Arabsat 1C

Purpose

Communication

Mission

Communication

Manufacturer

AESPC/LOR

Life Expectancy

7 years

Bus

Spacebus 100

Configuration

Spacebus-1000

Motor

R-4D-11

Equipment

25 C-band transponders, 2 S-band transponders

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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