Showing default

EUTE 36B (EUTE W7), 36101

Orbit data source: Space-Track

EUTE 36B (EUTE W7), 36101 is a payload satellite owned by EutelsatSA (FR) in GEO that was launched on Tue, 24 Nov 2009 UTC via a PROTON-M/BRIZ-M 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.

Not visible in the next 10 days
Identifier
36101, 2009-065A
Orbit
GEO
Country
Flag of UnknownUnknown / EUTE
Related business
Manufacturer
Thales Alenia
Mission
Operational Commercial Communications
Bus & Motor
SPACEBUS 4000C4, S400
Mass
5,627 kg wet, ~2,800 kg dry
Launch date (UTC)
2009-11-24 (16 years ago)
Launch vehicle
PROTON-M/BRIZ-M
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan + 1 Dish, 17.0 m
Radar Cross Section
44.769 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 EUTE 36B (EUTE W7)
1 36101U 09065A   25258.59454266  .00000096  00000-0  00000-0 0  9999
2 36101   0.0600 344.9959 0005736 195.6897  78.6324  1.00270618 57959
Epoch: 2025-09-15T14:16Z
TLE epoch observation values (Epoch: 2025-09-15T14:16:08.485Z)
Latitude
-0.04077°
Longitude
50.54904°
Altitude
35,781.687 km
Speed
3.075 km/s
True Right ascension
17h 17m 31s
True Declination
0° 02' 27"
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
16:40:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,812.179 km
Perigee altitude
35,763.806 km
Semi-major axis
42,166.129 km
Eccentricity
0.00057
Inclination
0.06°
RAAN
344.9959°
Arg. of periapsis
195.6897°
True anomaly
78.69685°
Mean anomaly
78.6324°
Eccentric anomaly
78.66462°
Mean motion
0.25067 °/min
Orbital period
1,436.17 mins
BSTAR
0
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...
Other satellites on launch #65 in the year 2009 (2009-11-24 UTC)

Documentation

Showing up to 5 results
|