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METOP-B (38771)
COSPAR: 2012-049A | Alt Name: METOP B
Image
Additional Sources
Launch Details
Launch Date
September 17, 2012
Launch Site
Launch Pad
LC31
Launch Vehicle
Soyuz-2-1A
Orbital Elements
NORAD ID
38771
International Designator
2012-049A
Epoch
Sat, 04 Jul 2026 03:41:31 GMT
Apogee
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Perigee
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Inclination
98.65°
Right Ascension
236.31°
Eccentricity
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Argument of Perigee
320.46°
Period
101.31 min
Mean Motion
14.21 rev/day
Latitude
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Longitude
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Altitude
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Velocity
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Polar Plot
3D Visualization
Basic Satellite Info
Name
METOP-B
Alternative Name
METOP B
Type
Payload
Status
Operational
Owner
EUMET
Country
EUMETSAT
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 38771U 12049A 26185.15384021 .00000113 00000-0 71615-4 0 9997
2 38771 98.6495 236.3139 0001242 320.4603 39.6484 14.21444055715673
Source: Celestrak
Summary
METOP-B is a meteorology satellite identified by NORAD_CAT_ID 38771 and OBJECT_ID 2012-049A. It was launched on September 17, 2012, from the TYMSC launch site using Soyuz-2-1A as its launch vehicle. The satellite has dimensions of 6.3 meters in length, a diameter of 3.4 meters, and spans 17.6 meters with its equipment deployed. METOP-B has a dry mass of 3,769 kg and launched at a total mass of 4,086 kg. It is equipped with an array of instruments including A/DCS, AMSU, ASCAT, AVHRR/3, GOME-2, GRAS, HIRS/4, IASI, MHS, SARP/3, SARR, and SEM-2 for meteorological observations. The satellite's power system consists of a deployable solar array and batteries. It is owned by EUMET and was manufactured by EADSB with the mission to conduct meteorology studies. METOP-B has an expected lifetime of 5 years.
Physical Characteristics
Length
6.3
Diameter
3.4
Span
17.6
Dry Mass
3769
Launch Mass
4086
Shape
Box + panel
Radar Cross Section
13.648
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
METOP B
Purpose
Meteorology
Mission
Meteorology
Manufacturer
EADSB
Life Expectancy
5 years
Bus
Metop
Configuration
PPF/SPOT Mk.3
Motor
AOCS
Equipment
A/DCS, AMSU, ASCAT, AVHRR/3, GOME-2, GRAS, HIRS/4, IASI, MHS, SARP/3, SARR, SEM-2
Power System
Deployable solar array, batteries
ADCS
Unknown
Transmitter Frequency
Unknown
Map
Next Pass
Azimuth Elevation Time (Local)
Start Azimuth
Max Elevation
Stop Azimuth
Time Until
Pass Duration
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