Resurs-P No.2

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Resurs-P No.2
MAKS Airshow 2013 (Ramenskoye Airport, Russia) (525-06).jpg
Mission type Earth observation
Operator Roskosmos
COSPAR ID 2014-087A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 40360
Website
Mission durationPlanned: 5 years
Elapsed: 8 years, 10 months, 4 days
Spacecraft properties
Spacecraft type Resurs-P
Bus Yantar
Manufacturer TsSKB Progress
Launch mass6,392 kilograms (14,092 lb)
Dimensions7.93 by 2.72 metres (26.0 ft × 8.9 ft)
Start of mission
Launch date26 December 2014, 18:55:50 (2014-12-26UTC18:55:50Z) UTC
Rocket Soyuz-2.1b
Launch site Baikonur Cosmodrome Site 31/6
Orbital parameters
Reference system Geocentric
Regime Sun-synchronous
Perigee altitude 468 kilometres (291 mi) [1]
Apogee altitude 477 kilometres (296 mi) [1]
Inclination 97.29 degrees [1]
Period 93.91 minutes [1]
Epoch 25 January 2015, 06:03:01 UTC [1]
Instruments
Geoton-L1, GSA, ShMSA, Koronas-Nuklon
 

Resurs-P No.2 [2] is a Russian commercial Earth observation satellite capable of acquiring high-resolution imagery (resolution up to 1.0 m). The spacecraft will be operated by Roscosmos along with the Resurs-P No.1 satellite.

Contents

The satellite is designed for multi-spectral remote sensing of the Earth's surface aimed at acquiring high-quality visible images in near real-time as well as on-line data delivery via radio link and providing a wide range of consumers with value-added processed data.

Additionally the satellite carries the Nuklon high-energy particle detector developed by the Moscow State University for detecting cosmic radiation. [2]

See also

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References

  1. 1 2 3 4 5 "RESURS P2 Satellite details 2014-087A NORAD 40360". N2YO. 25 January 2015. Retrieved 25 January 2015.
  2. 1 2 Zak, Anatoly. "Resurs-P remote-sensing satellite". RussianSpaceWeb. Retrieved 26 December 2014.