OCS (26062)

COSPAR: 2000-004B | Alt Name: OCS
DECAYED

Image
OCS Satellite Image
Additional Sources
Launch Details

Launch Date

January 27, 2000

Launch Site

AFWTR

Launch Pad

SLC8

Launch Vehicle

Minotaur I

Orbital Elements

NORAD ID

26062

International Designator

2000-004B

Decay Date

3/5/2001

Basic Satellite Info

Name

OCS

Alternative Name

OCS

Type

Payload

Status

Decayed

Owner

SOR

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
The OCS (Objective-Cued System) satellite, designated NORAD_CAT_ID 26062 and OBJECT_ID 2000-004B, was launched on January 27, 2000, from AFWTR SLC8 using the Minotaur I launch vehicle. It is an experimental satellite designed by LGAR for the US Space Operations Research (SOR) with a configuration of a 3.5 meter diameter kapton/aluminum balloon shaped as a sphere plus cylinder. The satellite's dry mass and launch mass are both 23 kg, with no onboard motor or power system. Its reflective surface area is 5.2361 square meters, making it visible from Earth. OCS was intended for experimental purposes only and had an operational lifetime of approximately one year post-launch.
Physical Characteristics

Length

3.5

Diameter

3.5

Span

3.5

Dry Mass

23

Launch Mass

23

Shape

Sphere + Cyl

Radar Cross Section

5.2361

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

OCS

Purpose

Experimental

Mission

Experimental

Manufacturer

LGAR

Life Expectancy

1 year

Bus

OCSE

Configuration

3.5 meter diameter kapton / aluminum balloon

Motor

None

Equipment

?

Power System

None

ADCS

Unknown

Transmitter Frequency

Unknown

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