Showing default

EUTE 9B, 41310

Orbit data source: Space-Track

EUTE 9B, 41310 is a payload satellite owned by EutelsatSA (FR) in GEO that was launched on Fri, 29 Jan 2016 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 9B details

Identifier	41310, 2016-005A
Orbit	GEO
Last TLE update	9 hours ago
Origin	EutelsatSA (FR / EUTE)
Manufacturer	Airbus/Toulouse
Mission	Operational Commercial Communications
Bus & Motor	EUROSTAR 3000, R-4D?
Mass	~5,162 kg wet, ~3,000 kg dry
Launch date (UTC)	2016-01-29 (9 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, 39 m
Radar Cross Section	46.485 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 9 hours ago

0 EUTE 9B
1 41310U 16005A   24339.80609774  .00000083  00000-0  00000-0 0  9994
2 41310   0.0677  75.3528 0004511 187.8398 110.1123  1.00271478 32505

Epoch: 2024-12-04T19:20Z

Definitive object data (Epoch: 2024-12-04T19:20:46.844Z)

Latitude	-0.04106°
Longitude	9.03821°
Altitude	35,792.765 km
Speed	3.074 km/s
True Right ascension	00h 53m 19s
True Declination	0° 02' 28"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	0.06475°
Longitude	141.61128°
Altitude	35,794.872 km
Speed	3.074 km/s
Apparent Right ascension	10h 06m 44s
Apparent Declination	-5° 10' 41"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	02:07:21
Azimuth	73.933° E
Elevation	-25.979°
Doppler factor	1

Orbital elements

Apogee altitude	35,806.772 km
Perigee altitude	35,768.73 km
Semi-major axis	42,165.888 km
Eccentricity	0.0004511
Inclination	0.0677°
RAAN	75.3528°
Arg. of periapsis	187.8398°
True anomaly	110.16083°
Mean anomaly	110.1123°
Eccentric anomaly	110.13657°
Mean motion	0.25067 °/min
BSTAR	Unknown
Orbital period	1436.15 mins