METSAT Systems Status

NOAA/POES / METOP DMSP

METEOSAT 6/7/8/9MTSAT-1R

GOES

NASA EOS (Aqua, etc.)

MARCH 24 UPDATE

DMSP OPSCAPFLIGHT

#LAUNCH

DATELTAN REMARKS

PRIMARY

F17 Nov 06 1728 Full mission capability

F16 Oct 03 1937SGYRO provides reduced pointing accuracy

SECONDARYF15 Dec 99 1827

SGYRO provides reduced pointing accuracy

F13 Mar 95 1825One of two operational recorders is degraded

TACTICAL F14 Apr 97 1630Unable to provide global smooth data

Tactical Ops OnlyTactical Ops Only

- FULLY MISSION CAPABLE- PARTIALLY MISSION CAPABLE- NOT MISSION CAPABLE

FOUO/UCI

DMSP OPSCAP CriteriaFOUO/UCI

MAJOR SUBSYSTEMS

FMC PMC NMC

Primary Sensor (OLS) Operational Line Scan

Fully operational and calibrated

Loss of calibration or otherwise degraded capability

Not operational

Command & Control

Fully capable of using commands and data from ground stations and other spacecraft subsystems to control attitude and operating modes

Degraded capability to use commands and data from ground stations and other spacecraft subsystems to control attitude and operating modes

Inability to use commands and data from ground stations and other spacecraft subsystems to control attitude and operating modes

Data Recorders Fully capable of collecting and disseminating worldwide smooth data (2 or more fully functional recorders delivering clean data)

Degraded capability to collect and disseminate worldwide smooth data (one recorder delivering clean data, or one of 2 recorders degraded)

Inability to collect and disseminate worldwide smooth data (0 recorders). ***Tactical Operations Satellite – able to provide real-time operational data to direct readout users

Electrical Power Fully capable of performing collection, storage, control and distribution of electrical power

Degraded capability to perform collection, storage, control and distribution of electrical power

Inability to perform collection, storage, control and distribution of electrical power

Communications Fully capable of receiving commands and transmitting telemetry and transmitting mission data

Degraded capability to receive commands, transmit telemetry or transmit mission data

Inability to receive commands, transmit telemetry or transmit mission data

Attitude Control Maintain positional pointing w/in .01 deg

Maintain positional pointing w/in .12 deg

Below User Thresholds

Color Key: CAL/VAL Nominal - G Loss of Redundancy/Degraded - Y Loss of Mission Capability - RFOUO/UCI* - Denotes Solid State Recorder (SSR) POC: Watch Officer (301-693-3196)

Flight Number (Overall)Operations NumberLTAN (+/- 5 Mins)Mission Data CategoryLaunch DateOn-Orbit (Months)SC/OLS Probable Life (Months)(per CSAT 04/23/08)

Earth Weather SensorsVisible/IR Imager (OLS)Microwave Imager/Sounder (SSMI/SSMIS)Microwave Temp Sounder(SSMT1)Microwave Water Vapor Sounder(SSMT2)

Space Weather SensorsX/Gamma Ray Detector(SSB-X family)Magnetometer (SSM)Ionosphere (SSI-ES2/-ES3)Electron/Proton (SSJ4/SSJ5)UV Limb Imager (SSULI)UV Spectrographic Imager (SSUSI)

Spacecraft SubsystemsCommand & ControlPowerAttitude ControlCommunications

RecordersOverall Recorder StatusIndividual Recorder Status 1 2 1 2 1 2* 1* 2* 1* 2*

3 4 3 4 3 4* 3* 4* 3* 4*

NA

Y

NANA

NA

F-1751

1728PRI

11/4/200628

42/139

F-1549

1820SEC

12/12/1999110

<6/57

YY

NANA

NAY

R

3/24/1995 4/4/1997 10/18/2003

1824SEC

1626TAC

166

NA

167

NA

Y

143<6/24

Y

Y

NA

Y

NA

R Y NA

R

NA

F-1347

1934PRI

6418/103

Y

F-1448

RY

Y

Y

F-1654

NA

FOUO/UCI

DMSP Spacecraft Status

SENSORS

Earth Weather Sensors

Visible/IR Image (OLS) Microwave Imager/Sounder (SSMI - SSMIS) GREEN YELLOW RED Temperature Sounder (SSMT1) Water Vapor Profiler (SSMT2) Fully Operational Degraded, but Useable Loss of Usefulness to User

Space Weather Sensors X/Gamma Ray Detector (SSB/X-M or X-2) Definition: Definition: Definition: Magnetometer (SSM) Meets all mission Does not meet specifications, Does not meet mission Ionsphere (SSI-ES or ES-2 or ES-3) requirements and however does meet some requirements. Electron/Proton (SSJ or SSJ/4 or SSJ/5) specifications. mission requirements. UV Limb Imager (SSULI) UV Spectographic Imager (SSUSI)

SUBSYSTEMS Nominal Loss of Redundancy/Degraded Loss of Capability

Spacecraft

Command & Control 2 SCP 1 SCP 0 SCP Power 2 Batteries 2 Batteries (1 Degraded) <1 Battery Attitude Control (Pointing Precision) Maintain positional pointing

within .01 deg Maintain positional pointing within .12 deg

Below User Thresholds

Communications All transmitters operational Loss of 1 transmitter Loss of EDT1&2, PDT1&2 or loss of DDT

Recorders Digital or Solid State Recorders (Numbers) 3 or 4 of 4 Operational 2 of 4 Operational <1 of 4 Operational (Does not

meet world-wide smooth requirement)

(Quality) Clean Noisy Unusable

FOUO/UCI

DMSP Spacecraft Status CriteriaFOUO/UCI

NOAA POES STATUSSTATUS FLIGHT #

LAUNCH DATE LTAN REMARKS

PRIMARY(AM) METOP A Oct 06 0930

NOMINAL: All sensors “GREEN”

PRIMARY(PM) NOAA 18 May 05 1341 HIRS IR channels degradation

increased (HIRS in “Red” Status)

BACKUP(AM) NOAA 17 Jun 02 2134

AMSU-A1 inoperative.AVHRR LACs will be discontinued as of 31 Mar 2009

On-Orbit Verification

NOAA 19

(N-PRIME)Feb 09 1358

On-orbit verification (OV) is in progress until futher notice.

SECONDARY

NOAA 15

(AM)May 98 1650

AMSU-A1 channels 11/14 are inoperative.

NOAA 16

(PM)Sept 00 1731

AMSU-A1 channel 4 is inoperative. AVHRR Scan Motor suffering degradation.

- FULLY MISSION CAPABLE- PARTIALLY MISSION CAPABLE- NOT MISSION CAPABLE

AMSU-A: Channel 7 noise exceeds specifications

FOUO/UCI

Flight Number (Overall)Operations Number (NORAD ID) IMPACTS LTAN (+/- 5 Mins)

Mission Data Category

Launch Date

On-Orbit (Months)

AVHRR Probable Life (Months)

Earth Weather Sensors Adv. Very High Resol. Radiometer (AVHRR) C M N S T

Adv. Microwave Sounding Unit -A1 (AMSU-A1) C N T

Adv. Microwave Sounding Unit -A2 (AMSU-A2) C N T

Adv. Microwave Sounding Unit -B (AMSU-B) C N T

High Resol. Infrared Radiation Sounder (HIRS) R C N

Microwave Humidity Sounder (MHS) C N T

Space Weather Sensors Solar Backscatter Ultraviolet Radiometer (SBUV)

Space Environment Monitor (SEM)

Spacecraft Subsystems Command & Control

Power

Attitude Control

Communications

Recorders Overall Recorder Status Individual Recorder Status 1* 2* 1* 2* 1 2* 1* 2* 1* 2* 1* 2* 1*

3* 4* 3* 4* 3 4* 3* 4* 3* 4* 3* 4* 3*

Y

NA

Y

Y

5/13/1998

142

N1525338

1650

SEC-AM

Green/Cal

Green/Cal

N1828654

METOP-A29499

No HRPT

N19 (N') 33591

Green/Cal

6/24/2002

N17274532134

BACKUP-AM

1358

CAL/VAL

1

2/6/2009

81

R

Green/Cal

NA

0930

PRI-AM

1341

PRI-PM

10/19/2006 5/20/2005

29 46

9/21/2000

102

N16265361731

SEC-PM

Y

NA

Green/Cal Y

Y

ASCAT NA

Y

Y

NA

Y

NA

Y

NA

Green/Cal

Green/Cal

Y

FOUO/UCINOAA Spacecraft Status

Color Key: CAL/VAL Nominal - G Loss of Redundancy/Degraded - Y Loss of Mission Capability - R

* - Denotes Solid State Recorder (SSR) POC: Mr. McCrone (831-656-4403)IMPACTS: C- COAMPS, M – MCSST/SST, N-NOGAPS, S-SATFOCUS, T-TCWEB

GEOSTATIONARY STATUSSTATUS FLIGHT # LAUNCHED Long. REMARKS

South America GOES 10 Apr 97 60W Imager: Green --- Sounder: Red

Primary GOES West GOES 11 May 00 75W All Earth Sensors: ‘G’. Space: ‘Y’

Primary GOES East GOES 12 Jul 01 135W All Earth Sensors: ‘G’. Space: ‘R’

On-Orbit / Storage GOES 13 May 06 105W All Earth Sensors: ‘G’. Space: ‘Y’

INDOEX-B/U METEOSAT 6 Nov 93 67E Backup only

INDOEX-Primary METEOSAT 7 Sep 97 57E All Earth Sensors: ‘G’.

On-Orbit / Storage METEOSAT 8 Aug 02 9.5E All Earth Sensors: ‘G’.

PRIMARY - Europe METEOSAT 9 Dec 05 0 All Earth Sensors: ‘G’.

China FY-2D Dec 06 105E All Earth Sensors: ‘G’.

West Pacific/Japan MTSAT-1R Feb 05 140E All Earth Sensors: ‘G’.

On-Orbit / Storage MTSAT-2 Feb 06 145E All Earth Sensors: ‘G’.

- FULLY MISSION CAPABLE- PARTIALLY MISSION CAPABLE- NOT MISSION CAPABLE

GEOSTATIONARY STATUSSTATUS FLIGHT # The Latest info {Sources}

South America GOES 10 http://www.oso.noaa.gov/goesstatus/spacecraftStatusSummary.asp?spacecraft=10

Primary GOES West GOES 11http://www.oso.noaa.gov/goesstatus/spacecraftStatusSummary.asp?spacecraft=11

Primary GOES East GOES 12http://www.oso.noaa.gov/goesstatus/spacecraftStatusSummary.asp?spacecraft=12

On-Orbit / Storage GOES 13 http://www.oso.noaa.gov/goesstatus/

INDOEX-B/U METEOSAT 6http://www.eumetsat.int/Home/Main/Access_to_Data/Meteosat_Image_Services/SP_1119363946419

INDOEX-Primary METEOSAT 7 “Same as Above”

On-Orbit / Storage METEOSAT 8 http://www.eumetsat.int/Home/index.htm

PRIMARY - Europe METEOSAT 9 http://www.eumetsat.int/Home/index.htm

China FY-2D http://nsmc.cma.gov.cn/fy2e.html

West Pacific/Japan MTSAT-1R http://www.jma.go.jp/jma/jma-eng/satellite/

On-Orbit / Storage MTSAT-2 http://www.jma.go.jp/jma/jma-eng/satellite/

- FULLY MISSION CAPABLE- PARTIALLY MISSION CAPABLE- NOT MISSION CAPABLE

FOUO/UCI

Flight Number (Overall)Operations Number (NORAD ID) Longitude Mission Data Category Launch Date On-Orbit (Months) Initial Operating Date Earth Sensor Probable Life (Months)

Earth Weather Sensors GOES IMAGER GOES SOUNDER INR (Image Navigation & Registation)

Spin Enhncd Vis & IR Imager (SEVIRI)

SOUNDER Capability Japan Adv Meteorological Imager (JAMI)

Space Weather Sensors Solar X-Ray Imager (SXI) R R Y

Space Environment Monitor (SEM) R R Y R Y

Spacecraft Subsystems Command & Control Power Attitude Control Communications

This means "Past it's Normal Life expectancy"Past

4/1/2003 STANDBY 9/3/1997

Y

Y

12/21/2005

NA

NA

NA

2/26/200548

8

MET9

1/26/2006 6/28/2005

MTSAT1R28622140EWPAC

NA

NANA

NANA

28912MET827509

9.5EEUROPE

12/21/200539

21

NA

NA

NA

NA

NA

NA

NA

GOES1126352

GOES1024786

GOES1329155

7/23/2001

GOES1226871135WGOESE

105WSTORAGE

32

60

5/24/2006

NA

91

Past

NA

NANA

NA

NARNA

NA

60WS.Amer.

75WGOESW

4/25/1997 5/3/2000141

Past

105

174/25/1997 6/21/2006

9/3/1997136

Past

MET724932

57EINDOEX

NAY

NA

NA

NA

R

NA

0EUROPE

12/12/200528

NANA

NA

12

NANA

NA

FOUO/UCI

Color Key: CAL/VAL Nominal - G Loss of Redundancy/Degraded - Y Loss of Mission Capability - R

POC: Mr. McCrone (831-656-4403)IMPACTS: C- COAMPS, M – MCSST/SST, N-NOGAPS, S-SATFOCUS, T-TCWEB“Past” This means "Past it's Normal Life expectancy"

GEOSTATIONARY STATUS

NASA EOS STATUSNORAD I.D. FLIGHT #

LAUNCH DATE LTAN REMARKS

25063 TRMM Nov 1997 N/A TROPICAL COVERAGE

25994 TERRA Dec 1999 1030 Nominal: LEAD EOS

27424 AQUA May 2002 1330 Nominal: “A Train” Lead

6 years

28376 AURA July 2004 1345Nominal: “A Train” Final

25789 QUIKSCAT Jun 1999 0600 Nominal: SeaWinds: 2 years

23560 ERS-2 Apr 1995 1000Nominal: Ocean winds

26997 JASON-1 Dec 2001 N/A Nominal Altimeter

33105 JASON-2 Jun 2008 N/A Nominal Altimeter

- FULLY MISSION CAPABLE- PARTIALLY MISSION CAPABLE- NOT MISSION CAPABLE

Subsystem Description

AMSU-A1 Advanced Microwave Sounding Unit -A1

AMSU-A2 Advanced Microwave Sounding Unit -A2

AMSU-B Advanced Microwave Sounding Unit -B

AVHRR Advanced Very High Resolution Radiometer

CCS Command and Control System

COMM Communications

DCS Data Collection System

DHS Data Handling System

DPLY Deployment Subsystem

EPS Electrical Power System

HIRS High Resolution Infrared Radiation Sounder

MHS Microwave Humidity Sounder

SBUV Solar Backscatter Ultraviolet Radiometer

SEM Space Environment Monitor

THERM Thermal Control System

NOAA Sensor Acronyms