INTELSAT 23 (IS-23) (38867)

COSPAR: 2012-057A | Alt Name: Intelsat IS-23

Image
INTELSAT 23 (IS-23) Satellite Image
Additional Sources
Launch Details

Launch Date

October 14, 2012

Launch Pad

LC81/24

Launch Vehicle

Proton-M/Briz-M

Orbital Elements

NORAD ID

38867

International Designator

2012-057A

Epoch

Sat, 04 Jul 2026 05:57:28 GMT

Apogee

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Perigee

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Inclination

0.02°

Right Ascension

22.92°

Eccentricity

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Argument of Perigee

190.62°

Period

1436.17 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

INTELSAT 23 (IS-23)

Alternative Name

Intelsat IS-23

Type

Payload

Status

Operational

Owner

INTELU

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 38867U 12057A   26185.24824108 -.00000273  00000-0  00000-0 0  9991
2 38867   0.0169  22.9185 0000490 190.6238 105.0391  1.00266443 50122

Source: Celestrak

Summary
INTELSAT 23 (IS-23) is a communication satellite operated by INTELU and was launched on October 14, 2012, from the TYMSC launch site using a Proton-M/Briz-M launch vehicle from LC81/24. The spacecraft has dimensions of 5.5 meters in length, 2.3 meters in diameter, and spans 22.4 meters when its solar arrays are deployed. It weighs 3200 kilograms at launch and carries a dry mass of 1440 kilograms. Equipped with 24 C-band transponders and 15 Ku-band transponders, the satellite uses a Star-2.4E Bus configuration manufactured by OSCD. Its power supply consists of two deployable solar arrays and batteries. The expected lifetime is 15 years, and its shape can be described as box-like with two panels for solar arrays.
Physical Characteristics

Length

5.5

Diameter

2.3

Span

22.4

Dry Mass

1440

Launch Mass

3200

Shape

Box + 2 pan

Radar Cross Section

113.2145

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Intelsat IS-23

Purpose

Communication

Mission

Communication

Manufacturer

OSCD

Life Expectancy

15 years

Bus

OSC Star 2

Configuration

Star-2.4E Bus

Motor

BT-4

Equipment

24 C-band transponders, 15 Ku-band transponders

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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