INDOSTAR 1 (25050)

COSPAR: 1997-071B | Alt Name: Cakrawarta 1

Image
INDOSTAR 1 Satellite Image
Additional Sources
Launch Details

Launch Date

November 12, 1997

Launch Site

FRGUI

Launch Pad

ELA2

Launch Vehicle

Ariane 44L

Orbital Elements

NORAD ID

25050

International Designator

1997-071B

Epoch

Fri, 03 Jul 2026 15:24:07 GMT

Apogee

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Perigee

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Inclination

12.97°

Right Ascension

19.91°

Eccentricity

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Argument of Perigee

317.95°

Period

1435.31 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

INDOSTAR 1

Alternative Name

Cakrawarta 1

Type

Payload

Status

Non-operational

Owner

INDO

Country

Indonesia

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 25050U 97071B   26184.64174936  .00000126  00000-0  00000-0 0  9996
2 25050  12.9744  19.9139 0001901 317.9459 216.1856  1.00326430104960

Source: Celestrak

Summary
INDOSTAR 1 (also known as Cakrawarta 1) is a communication satellite launched on November 12, 1997, from ELA2 at the Kourou launch site in French Guiana using an Ariane 44L rocket. The spacecraft measures 3.8 meters in length with a diameter of 2 meters and a span of 16.1 meters due to its solar arrays. It has a dry mass of 643 kg and was launched with a total mass of 718 kg. The satellite is equipped with five active S-band transponders for communication purposes, powered by two deployable solar arrays and batteries. INDOSTAR 1 was manufactured by OSCM (Orbital Sciences Corporation Malaysia) under the configuration known as Star-1, designed to operate for a period of 14 years in its mission focused on communications services.
Physical Characteristics

Length

3.8

Diameter

2

Span

16.1

Dry Mass

643

Launch Mass

718

Shape

Box + 2 Pan

Radar Cross Section

15.8489

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Indostar 1

Purpose

Communication

Mission

Communication

Manufacturer

OSCM

Life Expectancy

14 years

Bus

OSC Star 1

Configuration

Star-1

Motor

Star 30E

Equipment

5 active S-band transponders

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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