INTELSAT 512 (16101)

COSPAR: 1985-087A | Alt Name: INTELSAT 512

Image
INTELSAT 512 Satellite Image
Additional Sources
Launch Details

Launch Date

September 28, 1985

Launch Pad

LC36B

Launch Vehicle

Atlas G Centaur

Orbital Elements

NORAD ID

16101

International Designator

1985-087A

Epoch

Fri, 03 Jul 2026 21:45:37 GMT

Apogee

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Perigee

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Inclination

14.09°

Right Ascension

343.63°

Eccentricity

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Argument of Perigee

324.11°

Period

1452.85 min

Mean Motion

0.99 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 512

Alternative Name

INTELSAT 512

Type

Payload

Status

Non-operational

Owner

INTEL

Country

INTELSAT

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 16101U 85087A   26184.90668152 -.00000231  00000-0  00000-0 0  9992
2 16101  14.0863 343.6271 0009969 324.1057  60.4570  0.99115609130493

Source: Celestrak

Summary
INTELSAT 512 is a communication satellite with the NORAD identification number 16101 and object ID 1985-087A. It was launched on September 28, 1985, from Launch Complex 36B at Cape Canaveral using an Atlas G Centaur launch vehicle. The spacecraft has a configuration based on the Intelsat-5 bus with dimensions of 6.4 meters in length and a diameter of 2 meters, with a span of 15.6 meters due to its solar arrays. It was equipped with 26 C-band transponders and 6 Ku-band transponders for communication purposes. The satellite has a dry mass of 922 kg and a launch mass of 1092 kg, powered by two deployable solar arrays and batteries. Its mission lasted for approximately 9 years, operated by INTEL and manufactured by FORDA.
Physical Characteristics

Length

6.4

Diameter

2

Span

15.6

Dry Mass

922

Launch Mass

1092

Shape

Box + 2 Pan

Radar Cross Section

6.0376

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

INTELSAT VA F12

Purpose

Communication

Mission

Communication

Manufacturer

FORDA

Life Expectancy

9 years

Bus

FS INTELSAT 5

Configuration

Intelsat-5 bus

Motor

Star 37XF

Equipment

26 C-band transponders, 6 Ku-band transponders

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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