SEDSAT 1 (SO-33) (25509)

COSPAR: 1998-061B | Alt Name: SEDSAT-OSCAR-33

Image
SEDSAT 1 (SO-33) Satellite Image
Additional Sources
Launch Details

Launch Date

October 24, 1998

Launch Pad

SLC17A

Launch Vehicle

Delta 7326-9.5

Orbital Elements

NORAD ID

25509

International Designator

1998-061B

Epoch

Sat, 04 Jul 2026 04:46:08 GMT

Apogee

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Perigee

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Inclination

31.43°

Right Ascension

17.70°

Eccentricity

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Argument of Perigee

224.26°

Period

100.46 min

Mean Motion

14.33 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

SEDSAT 1 (SO-33)

Alternative Name

SEDSAT-OSCAR-33

Type

Payload

Status

Non-operational

Owner

SEDSH

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 25509U 98061B   26185.19870638  .00000530  00000-0  85857-4 0  9994
2 25509  31.4331  17.7004 0336276 224.2589 133.0678 14.33402843448271

Source: Celestrak

Summary
SEDSAT 1 (SO-33), also known as SEDSAT-OSCAR-33, is a technology satellite launched by the US on October 24, 1998, from Cape Canaveral Air Force Station's Launch Complex 17A using a Delta 7326-9.5 launch vehicle. The spacecraft has dimensions of 32.13 cm x 32.13 cm x 35.43 cm and is designed to have a lifetime of 5 years. It was manufactured by SEDSH (Student Explorer Demonstration Satellite Program Headquarters) with a dry mass of 36 kg, identical to its launch mass. The satellite features solar cells and batteries for power supply and carries SEASIS equipment on board. Its shape is cubic with a span, length, and diameter all measuring 0.4 meters. SEDSAT 1 serves technology-related purposes as part of the SEDSAT mission under the ownership of SEDSH.
Physical Characteristics

Length

0.4

Diameter

0.4

Span

0.4

Dry Mass

36

Launch Mass

36

Shape

Cube

Radar Cross Section

0.2922

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

SEDSAT

Purpose

Technology

Mission

Technology

Manufacturer

SEDSH

Life Expectancy

5 years (design)

Bus

SEDSAT

Configuration

32.13 cm x 32.13 cm x 35.43 cm structure

Motor

?

Equipment

SEASIS

Power System

Solar cells, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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