TDRS 4 (19883)

COSPAR: 1989-021B | Alt Name: TDRS 4

Image
TDRS 4 Satellite Image
Additional Sources
Launch Details

Launch Date

March 13, 1989

Launch Pad

LC39B

Launch Vehicle

Space Shuttle

Orbital Elements

NORAD ID

19883

International Designator

1989-021B

Epoch

Sat, 04 Jul 2026 04:26:28 GMT

Apogee

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Perigee

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Inclination

12.81°

Right Ascension

354.93°

Eccentricity

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Argument of Perigee

317.25°

Period

1462.16 min

Mean Motion

0.98 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

TDRS 4

Alternative Name

TDRS 4

Type

Payload

Status

Non-operational

Owner

GSFC

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 19883U 89021B   26185.18505675 -.00000214  00000-0  00000-0 0  9996
2 19883  12.8094 354.9320 0015859 317.2480 209.4505  0.98484590308210

Source: Celestrak

Summary
TDRS 4, also known as TDRS D, is a communication and data relay satellite managed by GSFC (Goddard Space Flight Center) and manufactured by TRW. Launched on March 13, 1989, from Launch Pad LC39B at AFETR using the Space Shuttle launch vehicle, it achieved stable orbit status on March 14, 1989. The satellite has dimensions of 1.3 meters in length, 2.4 meters in diameter, and a span of 17.4 meters. Its dry mass is 1673 kg, with an initial launch mass of 2245 kg. TDRS 4 features deployable solar arrays for power generation and batteries as backup power sources. The satellite's equipment includes various Ku-band and S-band Traveling Wave Tube Amplifiers (TWTAs) and Solid State Power Amplifiers (SSPAs) used for communication in different bands, including intersatellite links. It has a designed lifetime of 10 years and is equipped with an Attitude and Orbit Control System (AOCS). TDRS 4's shape consists of a box structure with dishes and two panels. The satellite operates primarily for providing communication and data relay services.
Physical Characteristics

Length

1.3

Diameter

2.4

Span

17.4

Dry Mass

1673

Launch Mass

2245

Shape

Box + Dish + 2 Pan

Radar Cross Section

20.9264

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

TDRS D

Purpose

Communication, data relay

Mission

Communication, data relay

Manufacturer

TRW

Life Expectancy

10 years (design)

Bus

TDRS

Configuration

Unknown

Motor

AOCS

Equipment

4 (+2) 25W Ku-band TWTAs for LP (linearly polarized) zone coverage 2 (+2) 1.5W Ku-band TWTAs for CP (circularly polarized) spot coverage 2 (+4) 25W Ku-band TWTAs for LP zone coverage 2 (+2) 1.5W Ku-band TWTAs for CP spot coverage 12 5W TWTAs for LP C-Band up/down 2 (+2) 26W S-band SSPAs (used for intersatellite links) 8 (+4) 3.5W S-band SSPAs (used for intersatellite links)

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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