Resurs-P No.1
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| Mission type | Earth observation |
|---|---|
| Operator | Roskosmos |
| COSPAR ID | 2013-030A |
| SATCAT № | 39186 |
| Website | |
| Mission duration | 5 years (planned) |
| Spacecraft properties | |
| Spacecraft type | Resurs-P |
| Bus | Yantar |
| Manufacturer | TsSKB Progress |
| Launch mass | 6,570 kilograms (14,480 lb) |
| Dimensions | 7.93 by 2.72 metres (26.0 ft × 8.9 ft) |
| Start of mission | |
| Launch date | 25 June 2013, 17:28:48 UTC |
| Rocket | Soyuz-2-1b |
| Launch site | Baikonur Cosmodrome 31/6 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Sun-synchronous |
| Perigee | 470 kilometres (290 mi) |
| Apogee | 480 kilometres (300 mi) |
| Inclination | 97.28 degrees |
| Epoch | Planned |
| Instruments | |
| Geoton-L1, GSA, ShMSA | |
Resurs-P No.1[1] is a Russian commercial Earth observation satellite capable of acquiring high-resolution imagery (resolution up to 0.7 m). The spacecraft will be operated by Roscosmos as a replacement of the Resurs-DK No.1 satellite.
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.
Spacecraft
The Resurs-P spacecraft was built by the Russian space company TsSKB Progress in Samara, Russia. It is a modified version of the military reconnaissance satellite Yantar-4KS1 (Terilen).[2] The spacecraft is three-axis stabilized. The design lifetime is no less than five years. The ground location accuracy is 10 metres (33 ft). The maximum daily imaging area is 1,000,000 square kilometres (390,000 sq mi).
Resurs is Russian for "Resource". The letter P stands for prospecting.[3]
Optical subsystem
- Type: apochromatic telephoto
- Focal length: 4000 mm
- Objective diameter: 500 mm
- Relative aperture: 1:8
- Field of view: 5° 12'
Spectral Resolution
- 0.58-0.8 µm panchromatic
- 0.45-0.52 µm blue
- 0.52-0.6 µm green
- 0.61-0.68 µm red
- 0.72-0.8 µm visible/ near infrared
- 0.8-0.9 µm near infrared
Spatial resolution
Panchromatic
- At 475 km altitude: 3.0 - 4.0 m
Multispectral
- Monochromatic mode: 12 – 60 m
- Panchromatic mode: 24 – 120 m
Hyperspectral
Maximum 30 m
Temporal resolution
[4] The revisit rate is once every 3 days.
Imaging Swath
[4] Swath width at the altitude of 475 km:
- Panchromatic camera: 38 km
- Multispectral camera: 97 km (Monochromatic mode) / 441 km (Panchromatic mode)
- Hyper-spectral imager: 25 km
See also
References
- ↑ Zak, Anatoly. "Resurs-P remote-sensing satellite". RussianSpaceWeb. Retrieved 29 June 2013.
- ↑ "Yantar-4KS1". Astronautix.com. Retrieved 12 August 2011.
- ↑ ""TsSKB Progress" will make satellite "Resource-P-3" for sensing". RIA Novosti. Retrieved 24 June 2013.
- ↑ 4.0 4.1 4.2 4.3 4.4 "Remote sensing spacecraft "Resurs-P"". Roscosmos. Retrieved 24 June 2013.
External links
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