GEOEYE 1 (33331)

COSPAR: 2008-042A | Alt Name: GeoEye-1

Image
GEOEYE 1 Satellite Image
Additional Sources
Launch Details

Launch Date

September 6, 2008

Launch Site

AFWTR

Launch Pad

SLC2W

Launch Vehicle

Delta 7420-10C

Orbital Elements

NORAD ID

33331

International Designator

2008-042A

Epoch

Sat, 04 Jul 2026 03:53:43 GMT

Apogee

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Perigee

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Inclination

98.13°

Right Ascension

258.89°

Eccentricity

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Argument of Perigee

21.43°

Period

98.32 min

Mean Motion

14.65 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

GEOEYE 1

Alternative Name

GeoEye-1

Type

Payload

Status

Operational

Owner

GEYE

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 33331U 08042A   26185.16230333  .00000551  00000-0  11270-3 0  9995
2 33331  98.1332 258.8871 0004764  21.4273 338.7129 14.64642299952635

Source: Celestrak

Summary
GEOEYE 1, also known as GeoEye-1, is an Earth observation satellite with a NORAD ID of 33331 and designated object ID of 2008-042A. It was manufactured by GDG for GEYE (GeoEye) and launched on September 6, 2008, from AFWTR's SLC2W launch pad using a Delta 7420-10C launch vehicle. The satellite has dimensions of 4.4 meters in length, 2.7 meters in diameter, and a span of 5 meters. It features a high-resolution panchromatic/multispectral camera, terabit recorder, and an X-band downlink for data transmission. Equipped with deployable fixed solar arrays and batteries, GEOEYE 1 has a dry mass of 1779 kg and was launched with a total mass of 1923 kg. The satellite's design includes an AOCS motor for attitude control and is expected to have a lifetime of over seven years with fuel for up to fifteen years. Its shape consists of a hexagonal cylinder with a panoramic section, and it has a radar cross-section (RCS) value of 4.937 square meters.
Physical Characteristics

Length

4.4

Diameter

2.7

Span

5

Dry Mass

1779

Launch Mass

1923

Shape

Hex Cyl + Pan

Radar Cross Section

4.937

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

GeoEye-1

Purpose

Earth observation

Mission

Earth observation

Manufacturer

GDG

Life Expectancy

7+ year design life; fuel for 15 years

Bus

SA-200HP

Configuration

SA-200HP

Motor

AOCS

Equipment

High resolution panchromatic/multispectral camera, terabit recorder; X-band downlink

Power System

Deployable fixed solar array, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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