CHINASAT 16 (SJ-13) (42662)

COSPAR: 2017-018A | Alt Name: Shi Jian 13

Image
CHINASAT 16 (SJ-13) Satellite Image
Additional Sources
Launch Details

Launch Date

April 12, 2017

Launch Site

XICLF

Launch Pad

LC2

Launch Vehicle

Chang Zheng 3B

Orbital Elements

NORAD ID

42662

International Designator

2017-018A

Epoch

Fri, 03 Jul 2026 05:54:11 GMT

Apogee

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Perigee

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Inclination

0.10°

Right Ascension

89.14°

Eccentricity

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Argument of Perigee

130.60°

Period

1436.06 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

CHINASAT 16 (SJ-13)

Alternative Name

Shi Jian 13

Type

Payload

Status

Operational

Owner

CAST

Country

China

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 42662U 17018A   26184.24596696 -.00000341  00000-0  00000-0 0  9994
2 42662   0.0967  89.1400 0004432 130.5966 260.5869  1.00274596 33915

Source: Celestrak

Summary
CHINASAT 16 (SJ-13), also known as Shi Jian 13, is a communications and technology satellite launched by China on April 12, 2017, from Xichang Satellite Launch Center using the Chang Zheng 3B launch vehicle. The spacecraft has dimensions of approximately 5 meters in length with a diameter of 2.5 meters and spans about 30 meters when its solar arrays are deployed. It was manufactured by CAST and features a DFH-4S Bus configuration, equipped with high-throughput 26 Ka-band transponders and a Laser communication terminal for data transmission. The satellite has a dry mass of 2500 kg and had a launch mass of 4600 kg, powered by two deployable solar arrays and batteries. It is designed to operate in orbit for up to 15 years.
Physical Characteristics

Length

5

Diameter

2.5

Span

30

Dry Mass

2500

Launch Mass

4600

Shape

Box + 2 Pan

Radar Cross Section

12.3708

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Zhongxing 16

Purpose

Communications, technology

Mission

Communications, technology

Manufacturer

CAST

Life Expectancy

15 years

Bus

DFH-3B

Configuration

DFH-4S Bus

Motor

LIPS-200

Equipment

high-throughput 26 Ka-band transponders, Laser communication terminal

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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