SUPERBIRD-A2 (28218)

COSPAR: 2004-011A | Alt Name: Superbird A2

Image
SUPERBIRD-A2 Satellite Image
Additional Sources
Launch Details

Launch Date

April 16, 2004

Launch Pad

SLC36A

Launch Vehicle

Atlas IIAS

Orbital Elements

NORAD ID

28218

International Designator

2004-011A

Epoch

Sat, 04 Jul 2026 04:33:13 GMT

Apogee

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Perigee

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Inclination

13.47°

Right Ascension

17.48°

Eccentricity

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Argument of Perigee

45.52°

Period

1447.76 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

SUPERBIRD-A2

Alternative Name

Superbird A2

Type

Payload

Status

Non-operational

Owner

SCC

Country

Japan

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 28218U 04011A   26185.18973676 -.00000007  00000-0  00000-0 0  9994
2 28218  13.4687  17.4831 0028999  45.5190 122.8650  0.99463828 80615

Source: Celestrak

Summary
SUPERBIRD-A2, also known as Superbird A2, is a communication satellite identified by NORAD CAT ID 28218 and OBJECT ID 2004-011A. Launched on April 16, 2004, from the Air Force Eastern Test Range (AFETR) at SLC36A using an Atlas IIAS launch vehicle, it was manufactured by BOHB for SCC, with a configuration of HS-601 and BSS-601. The satellite measures 4.5 meters in length, 3.5 meters in diameter, and has a span of 26.2 meters. It carries 23 active Ku-Band transponders and 4 active Ka-Band transponders for its communication mission. At launch, the satellite had a mass of 3100 kilograms and a dry mass of 1477 kilograms. Its power system includes two deployable solar arrays and batteries. The satellite has an operational lifetime of 13 years and is equipped with R-4D-11-300 motors for maneuvering, featuring a box shape with two panels.
Physical Characteristics

Length

4.5

Diameter

3.5

Span

26.2

Dry Mass

1477

Launch Mass

3100

Shape

Box + 2 Pan

Radar Cross Section

5.0118

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Superbird 6

Purpose

Communication

Mission

Communication

Manufacturer

BOHB

Life Expectancy

13 years

Bus

HS-601

Configuration

BSS-601

Motor

R-4D-11-300

Equipment

23 active Ku-Band transponders, 4 active Ka-Band transponders.

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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