TDRS 6 (22314)

COSPAR: 1993-003B | Alt Name: TDRS-6

Image
TDRS 6 Satellite Image
Additional Sources
Launch Details

Launch Date

January 13, 1993

Launch Pad

LC39B

Launch Vehicle

Space Shuttle

Orbital Elements

NORAD ID

22314

International Designator

1993-003B

Epoch

Sat, 04 Jul 2026 04:38:57 GMT

Apogee

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Perigee

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Inclination

14.18°

Right Ascension

356.93°

Eccentricity

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Argument of Perigee

180.23°

Period

1436.19 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

TDRS 6

Alternative Name

TDRS-6

Type

Payload

Status

Operational

Owner

GSFC

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 22314U 93003B   26185.19372596 -.00000289  00000-0  00000-0 0  9991
2 22314  14.1830 356.9318 0008851 180.2345 128.7025  1.00265147122579

Source: Celestrak

Summary
TDRS 6, also known as TDRS-6, is a communication and data relay satellite launched on January 13, 1993, from Launch Pad LC39B at AFETR using the Space Shuttle as its launch vehicle. Built by TRW for the GSFC (Goddard Space Flight Center), it has dimensions of 1.3 meters in length, 2.4 meters in diameter, and a span of 17.4 meters. The satellite carries a dry mass of 1673 kilograms and had a launch mass of 2534 kilograms. It is equipped with deployable solar arrays for power and batteries as backup. Its primary mission includes communication and data relay services, using various Ku-band and S-band TWTAs (Traveling Wave Tube Amplifiers) and SSPAs (Solid State Power Amplifiers). The satellite was designed to operate for 10 years and has a shape described as Box + Dish + 2 Pan with an RCS of 28.6701.
Physical Characteristics

Length

1.3

Diameter

2.4

Span

17.4

Dry Mass

1673

Launch Mass

2534

Shape

Box + Dish + 2 Pan

Radar Cross Section

28.6701

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

TDRS F

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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