LEMUR-2-JOBANPUTRA (41991)

COSPAR: 2017-008AV | Alt Name: Lemur-2-Jobanputra
DECAYED

Image
LEMUR-2-JOBANPUTRA Satellite Image
Additional Sources
Launch Details

Launch Date

February 15, 2017

Launch Site

SRILR

Launch Pad

FLP

Launch Vehicle

PSLV-XL

Orbital Elements

NORAD ID

41991

International Designator

2017-008AV

Decay Date

7/8/2023

Basic Satellite Info

Name

LEMUR-2-JOBANPUTRA

Alternative Name

Lemur-2-Jobanputra

Type

Payload

Status

Decayed

Owner

SPIRE

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
LEMUR-2-JOBANPUTRA is a 3U CubeSat satellite with dimensions 0.3m in length and width, and 0.1m in diameter. It was launched on February 15, 2017, from the Satish Dhawan Space Centre (SRILR) Launch Pad (FLP), using the PSLV-XL launch vehicle. The satellite, manufactured by SPIREG for the owner SPIRE, has a dry mass of 4.6 kg and is equipped with solar cells and batteries for power. Its equipment includes STRATOS (GPS radio occultation payload), SENSE (AIS-receiver), and AirSafe (ASD-B payload). The satellite's shape is described as Box+2 pan, and it has a reflective surface area of 0.094 square meters.
Physical Characteristics

Length

0.3

Diameter

0.1

Span

0.3

Dry Mass

4.6

Launch Mass

4.6

Shape

Box+2 pan

Radar Cross Section

0.094

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Lemur FM29

Purpose

Unknown

Mission

Unknown

Manufacturer

SPIREG

Life Expectancy

Unknown

Bus

Cubesat 3U

Configuration

CubeSat (3U)

Motor

None

Equipment

STRATOS (GPS radio occultation payload), SENSE (AIS-receiver), AirSafe (ASD-B payload, #78 and later)

Power System

Solar cells, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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