LANDSAT 5 (14780)

COSPAR: 1984-021A | Alt Name: Landsat 5

Image
LANDSAT 5 Satellite Image
Additional Sources
Launch Details

Launch Date

March 1, 1984

Launch Site

AFWTR

Launch Pad

SLC2W

Launch Vehicle

Delta 3920

Orbital Elements

NORAD ID

14780

International Designator

1984-021A

Epoch

Sat, 04 Jul 2026 01:16:37 GMT

Apogee

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Perigee

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Inclination

98.07°

Right Ascension

105.00°

Eccentricity

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Argument of Perigee

60.64°

Period

95.71 min

Mean Motion

15.05 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

LANDSAT 5

Alternative Name

Landsat 5

Type

Payload

Status

Non-operational

Owner

NOAA

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 14780U 84021A   26185.05321513  .00003823  00000-0  26320-3 0  9999
2 14780  98.0685 105.0040 0069927  60.6366 300.1819 15.04548179793924

Source: Celestrak

Summary
Landsat 5 was an Earth observation satellite launched on March 1, 1984, from Vandenberg Air Force Base using a Delta 3920 launch vehicle. The spacecraft measured 4.3 meters in length and had a diameter of 2.1 meters with a span of 6 meters due to its solar arrays. It weighed approximately 1863 kg dry and was designed for a three-year mission but operated for nearly 29 years. Landsat 5 was equipped with TM (Thematic Mapper) and MSS (Multispectral Scanner) sensors, providing critical data for Earth observation missions. The satellite's power came from deployable solar arrays and batteries, and it was stabilized using an MMS-AOCS motor system. Managed by NOAA, Landsat 5 played a vital role in environmental monitoring and geospatial analysis throughout its extended operational lifetime.
Physical Characteristics

Length

4.3

Diameter

2.1

Span

6

Dry Mass

1863

Launch Mass

1938

Shape

Box + 2 Pan

Radar Cross Section

8.406

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Landsat D'

Purpose

Earth observation

Mission

Earth observation

Manufacturer

GEVF/FAIR

Life Expectancy

3 years design; 28.8 years reached (#5)

Bus

MMS

Configuration

MMS

Motor

MMS-AOCS

Equipment

TM, MSS

Power System

Deployable solar array, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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