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GLOBALSTAR M076 (37190)
COSPAR: 2010-054C | Alt Name: Globalstar M076
Image
Additional Sources
Launch Details
Launch Date
October 19, 2010
Launch Site
Launch Pad
LC31
Launch Vehicle
Soyuz-2-1A
Orbital Elements
NORAD ID
37190
International Designator
2010-054C
Epoch
Sat, 04 Jul 2026 01:52:12 GMT
Apogee
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Perigee
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Inclination
52.00°
Right Ascension
56.72°
Eccentricity
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Argument of Perigee
71.34°
Period
114.08 min
Mean Motion
12.62 rev/day
Latitude
Calculating...
Longitude
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Altitude
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Velocity
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Polar Plot
3D Visualization
Basic Satellite Info
Name
GLOBALSTAR M076
Alternative Name
Globalstar M076
Type
Payload
Status
Operational
Owner
GLOB
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 37190U 10054C 26185.07792245 -.00000085 00000-0 10241-3 0 9993
2 37190 52.0037 56.7198 0001030 71.3395 92.9312 12.62262034725005
Source: Celestrak
Summary
GLOBALSTAR M076 (OBJECT_ID: 2010-054C) is a communication satellite manufactured by THALR and owned by GLOB. Launched on October 19, 2010, from TYMSC LC31 using a Soyuz-2-1A launch vehicle, the satellite has a bus configuration of ELiTeBus-1000. It measures 4 meters in length, with a diameter of 2 meters and a span of 12 meters. The dry mass is 500 kg, while its launch mass was 715 kg. Equipped with 16 C-to-S-band transponders and 16 L-to-C-band transponders, it provides communication services. Power is supplied by two deployable solar arrays generating up to 2.4 kW (bol) or 1.7 kW (eol), along with batteries. The satellite's shape is a trapezoidal cylinder with two panels and has an RCS of 4.5767. It was designed for a 15-year lifetime, stabilized using the LS-400 AOCS motor system.
Physical Characteristics
Length
4
Diameter
2
Span
12
Dry Mass
500
Launch Mass
715
Shape
Trap Cyl + 2 Pan
Radar Cross Section
4.5767
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Globalstar-2 FM5
Purpose
Communication
Mission
Communication
Manufacturer
THALR
Life Expectancy
15 years
Bus
Prisma
Configuration
ELiTeBus-1000
Motor
LS-400 AOCS
Equipment
16 C-to-S-band transponders, 16 L-to-C-band transponders
Power System
2 deployable solar arrays, 2.4 kW (bol), 1.7 kW (eol), 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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