NAVSTAR 36 (USA 100) (23027)

COSPAR: 1994-016A | Alt Name: GPS IIA-15

Image
NAVSTAR 36 (USA 100) Satellite Image
Additional Sources
Launch Details

Launch Date

March 10, 1994

Launch Pad

LC17A

Launch Vehicle

Delta 7925

Orbital Elements

NORAD ID

23027

International Designator

1994-016A

Epoch

Thu, 02 Jul 2026 12:13:38 GMT

Apogee

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Perigee

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Inclination

53.09°

Right Ascension

273.46°

Eccentricity

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Argument of Perigee

218.24°

Period

771.39 min

Mean Motion

1.87 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

NAVSTAR 36 (USA 100)

Alternative Name

GPS IIA-15

Type

Payload

Status

Non-operational

Owner

AFSMC

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 23027U 94016A   26183.50947441 -.00000020  00000-0  00000+0 0  9990
2 23027  53.0935 273.4632 0034525 218.2355 142.5508  1.86675120233518

Source: Celestrak

Summary
NAVSTAR 36 (USA 100), also known as GPS IIA-15, is a navigation satellite that was launched on March 10, 1994, from Launch Complex 17A at Cape Canaveral Air Force Station using the Delta 7925 launch vehicle. Manufactured by RWISB for AFSMC, this GPS satellite has dimensions of 2.4 meters in length and a diameter of 1.8 meters, with solar arrays spanning 5.3 meters when deployed. It has a dry mass of 860 kg and is equipped with two deployable solar arrays and batteries for power generation. The satellite's configuration includes a box shape with two panels and uses 3-axis stabilization to maintain its orientation in space. Its mission lifespan was projected to be 7.5 years, serving as part of the GPS constellation to provide navigation services globally.
Physical Characteristics

Length

2.4

Diameter

1.8

Span

5.3

Dry Mass

860

Launch Mass

860

Shape

Box + 2 Pan

Radar Cross Section

1.9565

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

GPS SVN 36

Purpose

Navigation

Mission

Navigation

Manufacturer

RWISB

Life Expectancy

7.5 years

Bus

GPS

Configuration

3-Axis stabilized

Motor

Star 37XFP

Equipment

?

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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