Image Band | VIS | WV | IR |
---|---|---|---|
spectral range | 0.45-1.0 µm | 5.7-7.1 µm | 10.5-12.5 µm |
resolution at nadir | 2.5 km | 5.0 km | 5.0 km |
In 1995, EUMETSAT began encrypting digital images and selling commercial licenses to receive METEOSAT real time broadcasts. EUMETSAT has made an international arrangement for METEOSAT encrypted data distribution via NOAA. Non-commercial users can arrange to get it from NOAA - contact John Pacquette at NESDIS. Fortunately, the METEOSAT-7 WEFAX images are still available in real time from EUMETSAT and from other sites in Europe, such as Nottingham, England. EUMETSAT posts a dissemination schedule. Radiometric calibration of the first-generation METEOSATs is indirect, through calculations and secondary earth-targets. METEOSAT navigation can be estimated using geometry and FORTRAN code.
An American site at UCSD describes the INDOEX science.
METEOSAT-5 has been re-located to a position around 63E. The re-location lasted from 14 January until 18 May 1998. The routine INDOEX mission started in July 1998.Only high resolution image formats will be disseminated on channel A2. There are AIVH and AW formats during daylight and AIW during night. PDUS reception coverage is possible from about 135E to 4W. A subset of the images taken by Meteosat-5 will be disseminated as hourly X-formats (XI, XVH) via the prime mission satellite at 0E. Additionally some reduced image formats are made available via the Internet at 3-hourly intervals.
Due to the high orbit inclination of METEOSAT-5, users may require a special PDUS set-up:
Use of a smaller diameter antenna or
Defocusing of the antenna feed.PDUS users will require two separate reception systems for direct reception of image data from 0E and 63E simultaneously. MKU's are required for other than 6-hourly image intervals.
Users who receive the HRI images from Meteosat-5 either directly or via the prime mission spacecraft, should note that these images can be easily distinguished from the other Meteosat images by checking the parameters in the identification field of the dissemination formats, i.e. the satellite identifier (bytes 1 and 2) and the longitude of the sub-satellite point (bytes 25 and 26).
INDOEX satellite images are on-line at EUMETSAT.
Data Policy for INDOEX
Below is a brief description of EUMETSAT's Data Policy for INDOEX. In view of the short term experimental nature of this activity, this deviates from EUMETSAT's standard Data Policy.INDOEX real time data are available free of charge to all users for any type of use. Access to encrypted real time data will be subject to a license agreement, in order to ensure the protection of EUMETSAT's Intellectual Property Rights. The necessary decryption key unit (MKU) will be provided to users at the currently applicable cost (700 ECU).
Access to INDOEX data archived in the MARF is also free of charge except for the payment of marginal costs of delivery as currently applicable. Again, access to MARF data will be subject to a simplified license agreement, in order to ensure the protection of EUMETSAT's Intellectual Property Rights. The Data Policy for INDOEX will apply only for the duration of the INDOEX activity, as agreed at the 34th EUMETSAT Council, i.e. until the end of 1999.
EUMETSAT's MSG satellite carries a 12-channel spinning Imager called SEVIRI, with a 1 km resolution visible band and 3 km resolution infrared bands, 8 of which are in the thermal infared.
Channel & wavelength (microns) |
Spectral Band upper-lower wavelengths (microns) |
Spatial Resolution (kilometers) |
Principal Sensitivity |
---|---|---|---|
HRV 0.75 | 0.6-0.9 | 1 km | cloud texture, winds |
VIS 0.64 | 0.56-0.71 | 3 km | cloud over land, winds |
VIS 0.81 | 0.74-0.88 | 3 km | cloud over water, vegetation |
NIR 1.6 | 1.50-1.78 | 3 km | cloud over snow |
MIR 3.8 | 3.48-4.36 | 3 km | low cloud |
IR 6.2 | 5.35-7.15 | 3 km | high water vapor |
IR 7.3 | 6.85-7.85 | 3 km | middle water vapor |
IR 8.7 | 8.30-9.10 | 3 km | total water vapor |
IR 9.7 | 9.38-9.94 | 3 km | total ozone |
IR 10.8 | 9.80-11.80 | 3 km | surface & cloud top temp., winds |
IR 12.0 | 11.00-13.00 | 3 km | surface temp. correction |
IR 13.4 | 12.40-13.40 | 3 km | higher clouds |
There is a MSG glossy brochure (2.5 MB PDF).
MSG is capable of full-disk images every 15 minutes. With a 60-cm aperture and a ton of spin-stabilized mass, imagery is sharp and stable.
Bandwidth limitations allow it to only downlink half of the 1 km resolution visible data (the left, middle, or right portion of the full-width scan).
MSG-1 was originally scheduled to launch in October 2000, but was delayed until July 2001 to deal with issues with the launch (moving from a dedicated launch on Ariane-4 to a rougher, shared launch on Ariane-5) and the ground segment. Further concerns about the ground system readiness delayed the launch schedule to August 2002. The MSG-1 satellite was successfully launched on 28 August 2002, and turned over to EUMETSAT on 25 September. First public imagery was due in late October 2002.
However, on 17 October 2002, a power supply switched off unexpectedly. Since then, the three remaining power supplies are being babied, preventing the global rebroadcast of the full resolution imagery, which will have to be routed through commercial communications satellites. As of November 2003, SEVERI HRIT and LRIT data is transmitted via EUMETCast, a satellite DVB broadcast system that provides coverage over Europe, Africa, the Middle East and parts of eastern North and South America.
The first official full-disk images were taken by MSG-1 on 28 November 2002.
After launch, there was one year of commissioning the ground system and validating calibrated imagery from MSG-1.
When MSG-1 became operational in 2004, it was renamed METEOSAT-8.
MSG-2 was originally scheduled for launch in 2002; it was eventually launched in 21 December 2005 on an Ariane-5 rocket. The first image was taken 24 January 2006.
MSG-3 was originally scheduled for launch in 2006; as of May 2003, it is scheduled for 7 years after the launch of MSG-1 (in 2009).
In spring 2003, EUMETSAT contracted for MSG-4 at a cost of 391 euros.
The total cost of MSG to EUMETSAT through 2015 will be 1,637 billion euros.
ESA has posted a Research Announcement of Opportunity (RAO) that solicits proposals to develop new and better satellite data products from MSG.
As of 2006, the next generation of EUMETSAT geosynchronous satellites will be named MTG: 3-axis stabilized, with a high resolution 5 channel imager and a lower resolution 22 channel full-disk imager. Hyperspectral infrared and UV/vis sounders are under consideration.
The address for Eumetsat is EUMETSAT Am Kavalleriesand 31 D-64295 Darmstadt Germany TEl. ++49 6151 8077 Fax ++49 6151 807555 Information about Meteosat can be obtained at the moment via an electronic bulletin board: telephone ++49 6151 807 620 / 621 The address for the Meteosat Data Service is Meteosat Data Service ESOC Robert Bosch Str. 5 D-6100 Darmstadt FR Germany PH: 06151 886, ext. 601 TELEX: 419 453
Date: Mon, 11 Nov 1996 Subject: GMS-5 data archive Dear Sir, With reference to your mail dated 5 November 1996 concerning GMS image, our office, Japan Weather Association (JWA) can provide you an analog VHS video tape of image titled "Time Lapse Cloud Movie" or a photographic print. Any other media including digital form for images is not available. Our e-mail address is kokusai@jwa.go.jp.
MTSAT is Jpanese weather satellite for geosynchronous orbit. MTSAT is a three-axis stabilized spacecraft and carries both a meteorological mission and an aeronautical communications mission. The Japan Meteorological Agency (JMA). contracted for MTSAT as a successor to GMS-5, in cooperation with the Civil Aviation Bureau (CAB), of the Ministry of Transport of Japan. The Japanese weather satellites are operated by JMA's Meteorological Satellite Center.
MTSAT SPECIFICATIONS | |
Design Life | more than 5 years for the meteorological mission,
more than 10 years for the air traffic control mission |
Survival Probability (Estimated) | 0.89 or greater for 5 years for the
meteorological mission
0.81 or greater for 10 years for the air-traffic control mission |
Orbital Position | +/- 0.1 degrees north-south and east-west, from its nominal position of 140E longitude |
Imaging period | Full earth disc within 27.5 minutes |
Imager characteristics |
Visible 0.55 - 0.80 micron
IR1 10.3 - 11.3 micron IR2 11.5 - 12.5 micron IR3 6.5 - 7.0 micron IR4 3.5 - 4.0 micron |
Signal quantisation | 10 bits for both Visible and IR |
Resolution (at the sub-satellite point) | 1 km for Visible, 4 km for IR |
Imager Data Transmission Rate | 2.62 Mbps |
Telecommunications | Transmission of raw image data |
Functions | Relay of High REsolution imager data (HiRED)
Relay of WEFAX and LRIT signals Relay of DCP reports Relay of DCP interrogation messages |
In the late 1990's, MTSAT-1 was constructed by Space Systems/Loral, and integrated with an Imager by ITT/fort Wayne, and shipped to Japan in March 1999. Unfortunately, the Japanese H-2 rocket launch failed in mid-November 1999.
The MTSAT-1 replacement is called MTSAT-1R. In March 2000, the contract for MTSAT-1R was awarded to SS/Loral. Launch was originally scheduled for March 2003. In November 2001, the MTSAT-1R launch was rescheduled to mid-summer 2003, due to delays created by US technology transfer restrictions. In the spring of 2003, launch was rescheduled to early 2004, due to problems during thermal-vacuum testing of the MTSAT Imager. In the fall of 2003, SS/Loral went bankrupt, temporarily delaying the shipment of MTSAT-1R. MTSAT-1R was successfully launched on 26 February 2005. MTSAT-1R became operational in mid-2005.
On MTSAT-1R, a Japanese Advanced Meteorological Imager (JAMI) will be supplied by Raytheon/Santa Barbara Research Systems (SBRS), not by ITT/Fort Wayne. The imaging schedule calls for one full-disk and one northern hemisphere scan per hour for cloud-tracked wind estimation.
MTSAT-1R's first published full-disk images were taken at midday on 23 March 2005. After becoming operational in mid-2005, the MTSAT-1R images are being published on the web.
MTSAT-1 is similar to the GOES-I/M Satellites, but carrying more communications gear and no Sounder. The MTSAT-1 5-band Imager by ITT had performance improvements over the GOES-I/M Imagers by ITT:
MTSAT-2 was launched on 24 February 2006. MTSAT-2 will be left in cold storage on-orbit until it is needed to replace MTSAT-1R, circa 2010. The MTSAT-2 spacecraft contract was awarded late in 2000 to MELCO, also known as Mitsubishi Electric Space Systems, with MTSAT-2's Imager to be supplied again by ITT/Fort Wayne. The major improvement in the ITT Imager is the noise performance of the infrared channels. MTSAT-2 will be the first to employ Mitsubishi's new communciations bus.
MTSAT-1 | MTSAT-2 | |
---|---|---|
IR1 | 0.20K @300K | 0.10K @300K |
0.55K @220K | 0.25K @220K | |
IR2 | 0.22K @300K | 0.10K @300K |
0.55K @220K | 0.25K @220K | |
IR3 | 0.15K @300K | 0.10K @300K |
0.85K @220K | 0.65K @220K | |
IR4 | 0.35K @300K | 0.10K @300K |
---------- | 2.50K @220K |
FY-2 Spacecraft | |||
---|---|---|---|
Attitude Stability | Spin stabilized (100 rotation/min) | ||
Orbital Altitude | 35800km | ||
Services | S-VISSR, L-Fax, etc. | ||
Scan Radiometer | |||
Channel | Waveband | Nadir Resolution | Temporal Resolution |
Visible | 0.55-1.05 micron | 1.25 x 1.25 (km x km) | 1 hour |
Water Vapour | 6.2 - 7.6 micron | 5 x 5 (km x km) | 1 hour |
IR | 10.5-12.5 micron | 5 x 5 (km x km) | 1 hour |
NASA requested and obtained permission to receive and share FY-2 data. This satellite will provide much needed coverage of the central Asian Hemisphere on an hourly basis. NASA has arranged to receive the data in Adelaide, Australia at the University of Southern Australia, and to transmit some full-resolution data, as well as calculated real-time products and localized sectors, over the Internet through Hawaii to NASA's Ames Research Center and Goddard Space Flight Center. There, the data will join similar data already being provided for GOES-8/9 and GMS-5. The data will be a short-term archive of infrared-resolution images, on-line for perhaps a week. Long-term archiving of the data will be performed by anyone willing to download the images using anonymous FTP from the NASA sites.
X-Sender: jdodge@mail.hq.nasa.gov Date: Mon, 11 Aug 1997 17:21:34 -0400 Subject: Real-Time FY-2 Data Dear Colleagues: Many of you have expressed an interest in receiving geostationary meteorological satellite data over the Asian Hemisphere. As you know the Chinese have recently launched a successful geostationary satellite and placed it at 105 deg E. Highly-compressed samples of their three channels (VIS, IR, and WV) are provided as attachments to this e-mail. Direct broadcast of the FY-2 data will begin in Oct., 1997. NASA has located a ground station for direct reception of the data at the Univ. of Southern Australia in Adelaide. The antenna has been erected, and the receiver, built in Hawaii and tested on GMS, will be installed before reception begins. Since any geostationary satellite produces large volumes of data, and FY-2, with its three bands, and hourly observations is no exception, we plan to place a computer at the reception site to generate segmented or subsampled files for reduced-volume transmission of the key data sets for real-time projects. We ask that you consider your real-time data requests carefully and plan a regular downloading of the requested products before their residence on the temporary storage site expires. Currently, we are planning a two-week residence time for the data. The data will be mirrored through Ames Research Center, and the Goddard Space Flight Center. We ask that you submit your requests for various areas and/or formats of real-time data so that we may attempt to consolidate the requests into reasonable sets of data that may satisfy the needs of several users and thereby save storage space and processing time. Please send your requests for real-time data processing to Pat Coronado at the Goddard Space Flight Center (Tel.(301)286-9323) or e-mail him at: cwifs@suzieq.gsfc.nasa.gov and please copy me at jdodge@hq.nasa.gov Those persons responding with descriptions of their real-time data requirements will be sent instructions concerning the procedure and scheduling of data access. Also don't forget to check out the Chinese Web site for higher resolution versions of their first images: http://www.cma.go.cn/fy2/fy2.htm It would also help if you would give me a brief description of the research that your are planning to do with the data. While we have heard of the desires to study the diurnal variabilities of various cloud regimes, and the interactions among atmospheric layers, as well as the evolution of large-scale storm systems, we are also interested to learn of the many possible atmospheric radiation interpretations, boundary layer-ocean interactions, multiple satellite analyses, latent heat exchange estimations, wind-wave relationships, rainfall estimation, and possible bioproductivity implications. Thanks for helping us to provide an efficient data access and delivery system for what promises to be a great new source of environmental satellite data. Jim Dodge *************************************************************** Dr. James C. Dodge Global Data Integration and Validation Program Science Division - Code YS Office of Mission to Planet Earth NASA Headquarters Washington, DC 20546 Tel. (202)358-0763 Fax (202)358-2770 Email: James.Dodge@hq.nasa.gov ***************************************************************
The spectral channels of VISSR on FY-2
Channel |
Wavelength (μm) |
||
FY-2 A,B |
FY-2 C,D,E |
||
VIS |
0.50-1.05 |
0.50-0.75 |
|
IR1 |
10.5-12.5 |
10.3-11.3 |
|
IR2 |
11.5-12.5 |
||
IR3 |
3.5-4.0 |
||
WV |
6.3-7.6 |
6.3-7.6 |
The characteristics of VIS channels of VISSR
Item |
Characteristics |
|
FY-2 A,B |
FY-2 C,D,E |
|
Wavelength (μm) |
0.50-1.05 |
0.50-0.75 |
FOV(μr) |
40 |
35 |
Space resolution (km) |
1.44 |
1.25 |
Dynamic range |
0-95% |
0-98% |
S/N |
6.5 (2.5%) |
1.5 (0.5%) |
43 (95%) |
50 (95%) |
|
Number of detectors |
4 (main) + 4 (alternate) |
4 (main) + 4 (alternate) |
Quantization level |
64 |
64 |
Calibration |
Cool-space images and solar image to realize in-orbit calibration |
Same as FY-2 A,B |
The characteristics of IR, WV channels of VISSR
FY-2 A,B |
FY-2 C,D,E |
||||||
IR |
WV |
IR1 |
IR2 |
IR3 |
WV |
||
Wavelength (μm) |
10.5-12.5 |
6.3-7.6 |
10.3-11.3 |
11.5-12.5 |
3.5-4.0 |
6.3-7.6 |
|
FOV (μr) |
160 |
160 |
140 |
140 |
140 |
140 |
|
Space resolution (km) |
5.76 |
5.76 |
5 |
5 |
5 |
5 |
|
Dynamic range |
180-330K |
190-290K |
180-330K |
180-280K |
|||
Temperature resolution |
0.6K |
1.0K |
0.4-0.2K |
0.4-0.2K |
0.5-0.3K |
0.6-0.5K |
|
Number of detectors |
1(main)+1 (alternate) |
1(main)+1 (alternate) |
1(main)+1 (alternate) |
1(main)+1 (alternate) |
1(main)+1 (alternate) |
1(main)+1 (alternate) |
|
Quantization level |
256 |
256 |
1024 |
1024 |
1024 |
1024 |
|
Calibration |
On board blackbody calibration, once every 3 disks |
The ground calibration accuracy is 1K. Cool space and planet calibration is used for on-board calibration, once every 2 disks. |
Subject: Re: Fengyun-2 downlink freq From: mdk@bom.gov.au (Mike Kenny) Date: Wed, 5 Feb 97 10:29:04 EST The GMS SV downlink frequency is 1687.1 MHz The Feng Yun 2B (FY-2B) meteorological satellite is offically due for launch sometime in 1997 and will be located at 105 degrees East. The FY-2B satellite will be operationally similar to GMS with high resolution stretched VISSR data (5km IR, 5km WV, 1.25km VIS), low resolution Wefax (analog), DCP capability and a new digital S-band fax service (CCITT G3) for domestic distribution of charts and imagery. FY-2B downlink characteristics Channel Freq Mod Power BW S.VISSR 1687.5 MHz BPSK NRZ-M +57 dBm 2 MHz LR-FAX 1691.0 MHz AM/FM +57 dBm 260 KHz S-FAX 1699.5 MHz AM/FM +46 dBm 26 KHz The Australian Bureau of Meteorology (BOM) is working with the China Meteorological Administration (CMA) on the Feng Yun 2B satellite and is providing a Turn Around Ranging Station (TARS) to support FY2AB operations as it does for the Japanese GMS satellite. --- Mike Kenny Satellite Engineering, Bureau of Meteorology, Melbourne, Australia.
By the way, the Chinese name all their weather satellites "Feng-Yun". They originally planned to use odd numbers for the low-earth orbiting birds (FY-1, FY-3, etc.), and even numbers for the geosynchronous birds (FY-2, FY-4, etc.). But then naming conventions changed in the late 1990's, so that now the first-generation geosynchronous series are all called FY-2. For some years, their first geosynchronous satellite to be constructed (and destroyed in a fueling accident) was called "FY-2A", and the first satellite to be launched successfully was called "FY-2B". By the year 2000, the unsuccessful satellite was no longer given any alphabetical designation, and the first geo-satellite in space was being called "FY-2A". By the year 2006, the decommissioned FY-2A and -2B satellites were declared "experimental", and FY-2C was declared "operational" at 105E.
The second generation of geosynchronous satellites to be launched by China will be designated FY-4, with plans for 3-axis stabilization, 12 channel imagery, passively cooled infrared detectors, 5-minute scans of China, and a FTIR sounder. As of 2006, the first two "experimental" satellites will be FY-4A/B launched in 2012/14, with four "operational" satellites to follow every two years starting in 2016.
The Scanning Television Radiometer (STR) on GOMS-1 has two spectral channels:
GOMS-1 initially had serious problems after launch on 31 October 1994, but the controllers eventually managed to bring it on-line. Despite the problems, GOMS-1 has become operational for the Eastern Hemisphere, but visible imagery can't be broadcast because of problems with the sensor package.
GOMS-1 infrared data became operational in June 1996. GOMS IR images are posted on-line, and a GOMS data archive is also on-line.
26 June 1996 GOMS/ELEKTRO WEFAX FORMAT as for METEOSAT WEFAX 3 second 300Hz Start signal 5 seconds phasing signal 5% black, 95% white lines about 800 lines of image each with line start signal (7 cycles of 840 Hz in blanking period) Image content : GOMS IR full earth disk + 4 quadrants : METEOSAT IR full earth disk : GMS IR 4 quadrants : meteorological charts (not seen here, see note) 3 seconds 450 Hz stop signal. RF characteristics Frequency : 1691.0 MHz EIRP: +? dBW Modulation: AM/FM Baseband video frequency : ? 1600 Hz Mod index: ? 80% Sub-carrier freq : 2400 Hz Freq Dev : ? 9 KHz RF bandwidth : 26 KHz Position : 76 degrees East ? is best guess or unknown, can anyone fill in the blanks ? GOMS DIGITAL DATA FORMAT Date rate : 1200 bps Modulation ? (PCM(SPILT PHASE-LEVEL)/PM) Mod index : ? (1.2 radian) RF bandwidth : ? Data Format : ? Note : See "06Z 23/6/96 surface analysis chart" at URL "http://www.drig.com/~johnb/gomsfax.gif " but beware, it is big (424 Kbytes !!!) (Credit : Chris van Lint and John Boyer) -- Mike Kenny (m.kenny@bom.gov.au) Satellite Engingeering, Bureau of Meteorology, Melbourne, Australia.
Subject: GOMS Schedule From: "Donald E. Hinsman" <hinsman@www.wmo.ch> Date: Wed, 03 Jul 1996 14:27:06 +0100 The following information was provided to WMO by the Russian Federation at the 48th WMO Executive Council. The following is the satellite data broadcasting schedule for GOMS N-1 WEFAX channel No. 1 via the Obninsk information reception and transmission station (on 1691 MHz) (Time in UTC) (SSP 76 degrees east longitude) Certified by Mr A. B. Uspensky, May 1996 Director-General of Planeta, a scientific production company Hour 03.00 04.00 15.00 16.00 17.00 Comments Min. :02 W0 W0 M4 Retransmission of other Meteosat WEFAX formats is possible :06 W1 W1 :10 W2 W2 :14 DTOT W3 W3 M5 :18 ETOT W4 DTOT W4 :22 CTOT :26 GMSA M1 GMSA M1 M6 :30 :34 :38 M2 M2 W0 :42 W1 :46 W2 :50 GMSB M3 M3 W3 :54 W4 :58 Where DTOT Standard Meteosat WEFAX format ETOT Standard Meteosat WEFAX format CTOT Standard Meteosat WEFAX format GMSA Standard Meteosat WEFAX format GMSB Standard Meteosat WEFAX format W0 Standard GOMS N-1 WEFAX format W1 Standard GOMS N-1 WEFAX format W2 Standard GOMS N-1 WEFAX format W3 Standard GOMS N-1 WEFAX format W4 Standard GOMS N-1 WEFAX format Mn Frames with Meteor TV information M1 Part of Europe sector (direct transmission mode) M2 Parts of the western Indian Ocean and Africa M3 Parts of the western Indian Ocean and Africa M4 Parts of the western Indian Ocean and Africa M5 Parts of the Arctic Eurasian coast (the Northern Passage - Sevmorput) M6 Parts of the Arctic Eurasian coast (the Northern Passage - Sevmorput) and W0 Full disk IR W1 NW quadrant IR W2 NE quadrant IR W3 SW quadrant IR W4 SE quadrant IR _________________________________________________ Dr Donald Hinsman tel: + 41 22 730 8285 41, av Giuseppe-Motta fax: + 41 22 734 2326 PO Box 2300 email: hinsman@www.wmo.ch CH-1211 Geneva 2, Switzerland _________________________________________________
Channel |
Spectral band (microns) |
Application |
---|---|---|
Visible | 0.675 |
Daytime cloud imagery Detection of special event (yellow dust, fire, haze, etc.) Atmospheric motion vector |
Shortwave IR | 3.75 |
Nighttime fog/stratus Fire detection Surface temperature |
Water Vapor | 6.75 |
Upper atmospheric water vapor Upper atmospheric motion |
Longwave Window 1 | 10.8 |
Standard IR split window channel (Cloud, Sea surface temperature, Yellow sand detection) |
Longwave Window 2 | 12.0 |
Standard IR split window channel (Cloud, Sea surface temperature, Yellow sand detection) |
Band center (nm) |
Band width (nm) |
Nominal radiance (Wm-2μm-1sr-1) |
Maximum radiance (Wm-2μm-1sr-1) |
NEdL (Wm-2μm-1sr-1) |
Signal/Noise ratio |
---|---|---|---|---|---|
412 | 20 | 100.0 | 150.0 | 0.100 | 1000 |
443 | 20 | 92.5 | 145.8 | 0.085 | 1090 |
490 | 20 | 72.2 | 115.5 | 0.067 | 1170 |
555 | 20 | 55.3 | 85.2 | 0.056 | 1070 |
660 | 20 | 32.0 | 58.3 | 0.032 | 1010 |
680 | 10 | 27.1 | 46.2 | 0.031 | 870 |
745 | 20 | 17.7 | 33.0 | 0.020 | 860 |
865 | 40 | 12.0 | 23.4 | 0.016 | 750 |