OCO 2 (40059)

COSPAR: 2014-035A | Alt Name: OCO-2

Image
OCO 2 Satellite Image
Additional Sources
Launch Details

Launch Date

July 2, 2014

Launch Site

AFWTR

Launch Pad

SLC2W

Launch Vehicle

Delta 7320-10C

Orbital Elements

NORAD ID

40059

International Designator

2014-035A

Epoch

Sat, 04 Jul 2026 06:05:56 GMT

Apogee

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Perigee

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Inclination

98.20°

Right Ascension

126.29°

Eccentricity

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Argument of Perigee

81.55°

Period

98.82 min

Mean Motion

14.57 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

OCO 2

Alternative Name

OCO-2

Type

Payload

Status

Operational

Owner

GSFC

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 40059U 14035A   26185.25412764  .00000490  00000-0  11877-3 0  9994
2 40059  98.2019 126.2875 0001480  81.5490 278.5876 14.57125666638531

Source: Celestrak

Summary
The OCO 2 (OCO-2) satellite, designated by NORAD CAT ID 40059 and OBJECT ID 2014-035A, is a LEOStar-2 configuration satellite built in the United States by OSCD for Earth Science missions. Launched on July 2, 2014, from AFWTR SLC2W using a Delta 7320-10C launch vehicle, it operates under the ownership of GSFC with an orbital lifetime of two years. The satellite measures 2.1 meters in length and has a diameter of 0.94 meters, spanning 9 meters when fully deployed. It carries three grating spectrometers as its primary equipment for conducting Earth science observations, specifically focusing on carbon dioxide measurements through its Orbiting Carbon Observatory payload. OCO 2 is powered by two deployable solar arrays and batteries. Its dry mass is 409 kg with a launch mass of 454 kg, and it features an AOCS motor system for attitude control. The satellite's shape consists of a hexagonal cylindrical body plus two panels.
Physical Characteristics

Length

2.1

Diameter

0.94

Span

9

Dry Mass

409

Launch Mass

454

Shape

Hex Cyl + 2 Pan

Radar Cross Section

1.154

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Orbiting Carbon Observatory

Purpose

Earth Science

Mission

Earth Science

Manufacturer

OSCD

Life Expectancy

2 years

Bus

Leostar-2

Configuration

LEOStar-2

Motor

AOCS

Equipment

3 grating spectrometers

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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