RESURS-P 2 (40360)

COSPAR: 2014-087A | Alt Name: Resurs-P No. 2
DECAYED

Image
RESURS-P 2 Satellite Image
Additional Sources
Launch Details

Launch Date

December 26, 2014

Launch Pad

LC31

Launch Vehicle

Soyuz-2-1B

Orbital Elements

NORAD ID

40360

International Designator

2014-087A

Decay Date

2/11/2025

Basic Satellite Info

Name

RESURS-P 2

Alternative Name

Resurs-P No. 2

Type

Payload

Status

Decayed

Owner

TSSKBP

Country

Russia

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
RESURS-P 2, also known as Resurs-P No. 2, is an Earth observation satellite belonging to Russia (RU) and was launched on December 26, 2014, from the TYMSC launch site using a Soyuz-2-1B launch vehicle. The spacecraft uses the Yantar bus design with dimensions of 7.9 meters in length, 2.7 meters in diameter, and has a span of 13 meters. It weighs approximately 6392 kg at launch, with a dry mass of about 5900 kg. Powered by two deployable solar arrays and batteries, RESURS-P 2 is equipped for Earth observation and cosmic ray detection through the Nuklon particle detector. Its mission duration was planned for five years, but it may have lasted up to seven years. The satellite was built by TSSKBP and operates using instruments such as HGeoton-L1, KShMSA, and an AIS-receiver.
Physical Characteristics

Length

7.9

Diameter

2.7

Span

13

Dry Mass

5900

Launch Mass

6392

Shape

Cy+2 pan

Radar Cross Section

8.331

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Resurs-P No. 2

Purpose

Earth Observation (all), cosmic rays (#2)

Mission

Earth Observation (all), cosmic rays (#2)

Manufacturer

TSSKBP

Life Expectancy

5 years (#1, 2); 7 years (#3, 4, 5);

Bus

Resurs P

Configuration

Yantar bus

Motor

Unknown

Equipment

HGeoton-L1, KShMSA, AIS-receiver (all); Nuklon particle detector (#2)

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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