HIMAWARI-9 (41836)

COSPAR: 2016-064A | Alt Name: Himawari-9

Image
HIMAWARI-9 Satellite Image
Additional Sources
Launch Details

Launch Date

November 2, 2016

Launch Site

TANSC

Launch Pad

Y

Launch Vehicle

H-IIA 202

Orbital Elements

NORAD ID

41836

International Designator

2016-064A

Epoch

Thu, 02 Jul 2026 16:41:28 GMT

Apogee

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Perigee

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Inclination

0.03°

Right Ascension

267.94°

Eccentricity

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Argument of Perigee

225.42°

Period

1436.15 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

HIMAWARI-9

Alternative Name

Himawari-9

Type

Payload

Status

Operational

Owner

JMA

Country

Japan

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 41836U 16064A   26183.69547150 -.00000265  00000-0  00000-0 0  9990
2 41836   0.0302 267.9360 0001438 225.4185 178.4790  1.00268231 35361

Source: Celestrak

Summary
HIMAWARI-9, also known as Himawari-9, is a communication and meteorology satellite operated by JMA (Japan Meteorological Agency). Launched on November 2, 2016, from Tanegashima Space Center using the H-IIA 202 launch vehicle, this DS-2000 bus configured satellite has dimensions of 8 meters in length, 4 meters in diameter, and a span of 30 meters. It carries payloads such as AHI (Advanced Himawari Imager), SEDA (Space Environment Data Acquisition Unit), and DCS (Data Collection System). With a launch mass of 3500 kg and a dry mass of 1300 kg, the satellite is powered by deployable solar arrays and batteries. It features an R-4D motor for propulsion and has a shape described as "Box +panel+boom" with a radar cross-section (RCS) of 38.791 square meters. The mission's planned lifetime includes a meteorological operation period of 8 years within a total duration of 15 years, and it was manufactured by MELCO (Mitsubishi Electric Corporation).
Physical Characteristics

Length

8

Diameter

4

Span

30

Dry Mass

1300

Launch Mass

3500

Shape

Box +panel+boom

Radar Cross Section

38.791

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Himawari 9

Purpose

Communication, Meteorology

Mission

Communication, Meteorology

Manufacturer

MELCO

Life Expectancy

15 years (meteorological mission 8 years)

Bus

DS-2000

Configuration

DS-2000

Motor

R-4D

Equipment

AHI, SEDA, DCS

Power System

Deployable solar array, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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