NIGCOMSAT 1R (38014)

COSPAR: 2011-077A | Alt Name: Nigcomsat 1R

Image
NIGCOMSAT 1R Satellite Image
Additional Sources
Launch Details

Launch Date

December 19, 2011

Launch Site

XICLF

Launch Pad

LC2

Launch Vehicle

Chang Zheng 3B

Orbital Elements

NORAD ID

38014

International Designator

2011-077A

Epoch

Sat, 04 Jul 2026 05:32:09 GMT

Apogee

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Perigee

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Inclination

0.01°

Right Ascension

279.88°

Eccentricity

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Argument of Perigee

75.51°

Period

1436.09 min

Mean Motion

1.00 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

NIGCOMSAT 1R

Alternative Name

Nigcomsat 1R

Type

Payload

Status

Operational

Owner

NGCOM

Country

Nigeria

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 38014U 11077A   26185.23066405  .00000157  00000-0  00000-0 0  9993
2 38014   0.0053 279.8835 0002557  75.5074  52.3696  1.00272357 53124

Source: Celestrak

Summary
NIGCOMSAT 1R, also known as Nigcomsat 1R, is a communication satellite operated by NGCOM and manufactured by CAST using the DFH-4 bus configuration. Launched on December 19, 2011, from Xichang Satellite Launch Center (XICLF), it utilized the Chang Zheng 3B launch vehicle. The satellite has dimensions of 5 meters in length, 2.5 meters in diameter, and a span of 30 meters with deployable solar arrays for power generation along with batteries. It carries a payload including 4 C-band, 14 Ku-band, 8 Ka-band, and 2 L-band transponders. The satellite has a dry mass of 2,500 kilograms and was launched with a total mass of 5,086 kilograms. NIGCOMSAT 1R is intended for communication purposes and features the DFH-4 LAE motor system. Its operational lifetime is expected to be 15 years.
Physical Characteristics

Length

5

Diameter

2.5

Span

30

Dry Mass

2500

Launch Mass

5086

Shape

Box + 2 Pan

Radar Cross Section

18.4944

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Nigcomsat 1R

Purpose

Communication

Mission

Communication

Manufacturer

CAST

Life Expectancy

15 years

Bus

DFH-4

Configuration

DFH-4 bus

Motor

DFH-4 LAE

Equipment

4 C-band, 14 Ku-band, 8 Ka-band, 2 L-band transponders

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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