ORBVIEW 1 (MICROLAB) (23547)

COSPAR: 1995-017C | Alt Name: OrbView-1

Image
ORBVIEW 1 (MICROLAB) Satellite Image
Additional Sources
Launch Details

Launch Date

April 3, 1995

Launch Site

WRAS

Launch Pad

RW30/12

Launch Vehicle

Pegasus H

Orbital Elements

NORAD ID

23547

International Designator

1995-017C

Epoch

Sat, 04 Jul 2026 06:30:42 GMT

Apogee

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Perigee

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Inclination

69.97°

Right Ascension

183.72°

Eccentricity

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Argument of Perigee

295.23°

Period

98.13 min

Mean Motion

14.67 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

ORBVIEW 1 (MICROLAB)

Alternative Name

OrbView-1

Type

Payload

Status

Unknown

Owner

ORBI

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 23547U 95017C   26185.27132500  .00001414  00000-0  26158-3 0  9990
2 23547  69.9741 183.7209 0012008 295.2287  64.7611 14.67483207660790

Source: Celestrak

Summary
ORBVIEW 1 (MICROLAB), also known as OrbView-1, is a MicroStar configuration satellite manufactured by OSCG and owned by ORBI. Launched on April 3, 1995, from the Wallops Flight Facility (WRAS) using a Pegasus H launch vehicle, this Earth observation satellite has dimensions of 0.2 meters in length, 1 meter in diameter, and spans 4.3 meters when its solar arrays are deployed. It carries equipment including the OTD (Optical Transient Detector) and GPS/MET instruments. The satellite’s dry mass is 42 kilograms, identical to its launch mass, and it uses two deployable solar arrays with batteries for power supply. Its shape consists of a cylinder with two panels and an antenna, and it has a radar cross-section area (RCS) of 0.7658 square meters.
Physical Characteristics

Length

0.2

Diameter

1

Span

4.3

Dry Mass

42

Launch Mass

42

Shape

Cyl + 2 Pan + Ant

Radar Cross Section

0.7658

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Microlab 1

Purpose

Earth observation

Mission

Earth observation

Manufacturer

OSCG

Life Expectancy

Unknown

Bus

Microstar

Configuration

MicroStar (double)

Motor

?

Equipment

OTD (Optical Transient Detector), GPS/MET

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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