INTELSAT 602 (IS-602) (20315)

COSPAR: 1989-087A | Alt Name: INTELSAT 602

Image
INTELSAT 602 (IS-602) Satellite Image
Additional Sources
Launch Details

Launch Date

October 27, 1989

Launch Site

FRGUI

Launch Pad

ELA2

Launch Vehicle

Ariane 44L

Orbital Elements

NORAD ID

20315

International Designator

1989-087A

Epoch

Sat, 04 Jul 2026 03:43:45 GMT

Apogee

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Perigee

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Inclination

14.33°

Right Ascension

7.42°

Eccentricity

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Argument of Perigee

220.90°

Period

1454.43 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

INTELSAT 602 (IS-602)

Alternative Name

INTELSAT 602

Type

Payload

Status

Non-operational

Owner

INTEL

Country

INTELSAT

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 20315U 89087A   26185.15538375 -.00000070  00000-0  00000-0 0  9990
2 20315  14.3298   7.4231 0005235 220.9000 132.1568  0.99007814131486

Source: Celestrak

Summary
INTELSAT 602 (IS-602) is a communication satellite launched on October 27, 1989, from Guiana Space Centre using an Ariane 44L launch vehicle. The spacecraft has a length of 11.8 meters and a diameter of 3.6 meters, with a dry mass of 1906 kilograms and a launch mass of 4286 kilograms. It is equipped with 38 C-band transponders and 10 Ku-band transponders for communication purposes. The satellite's power comes from solar cells mounted on the body and drop-skirt, along with batteries. INTELSAT 602 was manufactured by HSES and operated for a lifetime of 13 years. It is owned by INTEL and has an RCS of 12.6191. The satellite's shape is cylindrical.
Physical Characteristics

Length

11.8

Diameter

3.6

Span

11.8

Dry Mass

1906

Launch Mass

4286

Shape

Cyl

Radar Cross Section

12.6191

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

INTELSAT VI F-2

Purpose

Communication

Mission

Communication

Manufacturer

HSES

Life Expectancy

13 years

Bus

HS-389

Configuration

HS-389

Motor

R-4D-12 x2

Equipment

38 C-band transponders, 10 Ku-band transponders

Power System

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

ADCS

Unknown

Transmitter Frequency

Unknown

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