SAKURA-3A (CS-3A) (18877)

COSPAR: 1988-012A | Alt Name: Sakura 3A

Image
SAKURA-3A (CS-3A) Satellite Image
Additional Sources
Launch Details

Launch Date

February 19, 1988

Launch Site

TANSC

Launch Pad

N

Launch Vehicle

H-1

Orbital Elements

NORAD ID

18877

International Designator

1988-012A

Epoch

Fri, 03 Jul 2026 18:08:32 GMT

Apogee

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Perigee

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Inclination

15.22°

Right Ascension

351.58°

Eccentricity

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Argument of Perigee

331.91°

Period

1467.32 min

Mean Motion

0.98 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

SAKURA-3A (CS-3A)

Alternative Name

Sakura 3A

Type

Payload

Status

Non-operational

Owner

NASDA/TSCJ

Country

Japan

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 18877U 88012A   26184.75593022 -.00000210  00000-0  00000-0 0  9998
2 18877  15.2201 351.5827 0008276 331.9061  35.9805  0.98137851127834

Source: Celestrak

Summary
The SAKURA-3A (CS-3A) satellite was launched on February 19, 1988, from Tanegashima Space Center using an H-1 launch vehicle for a communication mission by NASDA/TSCJ. It has dimensions of 3.6 meters in length and 2.2 meters in diameter with the same span measurement. The satellite's dry mass is 455 kg, while its launch mass was 565 kg. It carries 2 C-band transponders (with an additional one) and 10 Ka-band transponders (with a potential of five more), equipped with solar cells and batteries for power supply. The satellite’s operational lifespan is expected to be seven years, manufactured by MELCO under the CS-3 bus configuration.
Physical Characteristics

Length

3.6

Diameter

2.2

Span

3.6

Dry Mass

455

Launch Mass

565

Shape

Cyl + Ant

Radar Cross Section

6.1699

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

CS-3A

Purpose

Communication

Mission

Communication

Manufacturer

MELCO

Life Expectancy

7 years

Bus

CS 3

Configuration

Unknown

Motor

TE-M-700-5

Equipment

2 (+1) C-band transponders 4W TWTA, 180 MHz bandwidth, EIRP max 29 dBW 10 (+5) Ka-band transponders 4.2W TWTA, 100 MHz bandwidth, EIRP max 37 dBW

Power System

Solar cells, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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