SWAS (25560)

COSPAR: 1998-071A | Alt Name: SWAS

Image
SWAS Satellite Image
Additional Sources
Launch Details

Launch Date

December 6, 1998

Launch Site

WRAS

Launch Pad

RW30/12

Launch Vehicle

Pegasus XL

Orbital Elements

NORAD ID

25560

International Designator

1998-071A

Epoch

Sat, 04 Jul 2026 05:49:52 GMT

Apogee

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Perigee

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Inclination

69.89°

Right Ascension

183.53°

Eccentricity

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Argument of Perigee

242.69°

Period

95.38 min

Mean Motion

15.10 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

SWAS

Alternative Name

SWAS

Type

Payload

Status

Backup

Owner

GSFC

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 25560U 98071A   26185.24297071  .00002799  00000-0  17967-3 0  9997
2 25560  69.8939 183.5320 0008275 242.6949 117.3373 15.09703087499843

Source: Celestrak

Summary
The Satellite with Autonomous Weights in Space (SWAS) is an astronomy satellite, specifically designed for sub-millimeter wave observations, launched on December 6, 1998, from the Wallops Flight Facility using a Pegasus XL launch vehicle. It has a NORAD catalog ID of 25560 and an object ID of 1998-071A. The satellite is owned by GSFC (Goddard Space Flight Center) and was manufactured by the same entity. Its dimensions are 1.7 meters in length, 1 meter in diameter, and it has a span of 2 meters with a dry mass of 282 kilograms. SWAS is equipped with a 55 x 71 cm elliptical off-axis Cassegrain telescope and submillimeter radiometers for its mission purposes. The satellite's configuration includes three-axis stabilization and two deployable fixed solar panels, complemented by body-mounted solar arrays and batteries for power generation. Its shape consists of a cylinder with two panels, and it has an RCS (Reflective Cross Section) value of 1.8056 square meters.
Physical Characteristics

Length

1.7

Diameter

1

Span

2

Dry Mass

282

Launch Mass

282

Shape

Cyl+2 Pan

Radar Cross Section

1.8056

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

SWAS

Purpose

Astronomy, sub-mm wave

Mission

Astronomy, sub-mm wave

Manufacturer

GSFC

Life Expectancy

Unknown

Bus

SMEX

Configuration

3 axis stabilized, 4 deployable, fixed solar panels and one body-mounted

Motor

?

Equipment

55 x 71 cm elliptical off-axis Cassegrain telescope, submillimeter radiometers

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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