Showing default

GLOBALSTAR M080, 38041

Orbit data source: Space-Track

GLOBALSTAR M080, 38041 is a payload satellite owned by Globalstar (US) in LEO that was launched on Wed, 28 Dec 2011 UTC via a SOYUZ-2-1A launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...
Identifier
38041, 2011-080B
Orbit
LEO
Country
Flag of UnknownUnknown / GLOB
Related business
Manufacturer
Thales Alenia
Mission
Operational Commercial Communications
Bus & Motor
PRISMA?, LS-400 AOCS?
Mass
715 kg wet, ~500 kg dry
Launch date (UTC)
2011-12-28 (14 years ago)
Launch vehicle
SOYUZ-2-1A
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Trap Cyl + 2 Pan, 6.0 m
Radar Cross Section
20.931 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 GLOBALSTAR M080
1 38041U 11080B   26041.48954852 -.00000091  00000-0  73395-4 0  9996
2 38041  52.0070  44.6695 0000421  35.1146 132.9246 12.62266238652887
Epoch: 2026-02-10T11:44Z
TLE epoch observation values (Epoch: 2026-02-10T11:44:56.992Z)
Latitude
9.38047°
Longitude
-99.51425°
Altitude
1,413.788 km
Speed
7.155 km/s
True Right ascension
14h 29m 10s
True Declination
9° 19' 48"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
19:05:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.324 km
Perigee altitude
1,413.668 km
Semi-major axis
7,792.133 km
Eccentricity
0.00004
Inclination
52.007°
RAAN
44.6695°
Arg. of periapsis
35.1146°
True anomaly
132.92813°
Mean anomaly
132.9246°
Eccentric anomaly
132.92637°
Mean motion
3.15543 °/min
Orbital period
114.09 mins
BSTAR
0.000073395
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|