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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). Payloads include a variety of satellites, spacecraft, and rockets 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

EUTE 36B (EUTE W7) details

Identifier	36101, 2009-065A
Orbit	GEO
Last TLE update	1 day ago
Origin	EutelsatSA (FR / EUTE)
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 (15 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, 34 m
Radar Cross Section	44.769 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 EUTE 36B (EUTE W7)
1 36101U 09065A   24347.84632605  .00000126  00000-0  00000-0 0  9994
2 36101   0.0638   4.7051 0005693 269.6995 162.7938  1.00270410 55186

Epoch: 2024-12-12T20:18Z

Definitive object data (Epoch: 2024-12-12T20:18:42.57Z)

Latitude	0.08375°
Longitude	50.50665°
Altitude	35,809.503 km
Speed	3.073 km/s
True Right ascension	05h 08m 49s
True Declination	0° 05' 01"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	0.08727°
Longitude	68.41353°
Altitude	35,810.45 km
Speed	3.073 km/s
Apparent Right ascension	06h 30m 22s
Apparent Declination	-4° 54' 16"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	19:58:01
Azimuth	35.176° NE
Elevation	-49.803°
Doppler factor	1

Orbital elements

Apogee altitude	35,812.056 km
Perigee altitude	35,764.046 km
Semi-major axis	42,166.188 km
Eccentricity	0.0005693
Inclination	0.0638°
RAAN	4.7051°
Arg. of periapsis	269.6995°
True anomaly	162.81308°
Mean anomaly	162.7938°
Eccentric anomaly	162.80344°
Mean motion	0.25067 °/min
BSTAR	Unknown
Orbital period	1436.17 mins