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). 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
41310, 2016-005A
Orbit
GEO
Country
Flag of FRFR / EUTE
Related business
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 (11 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, 19.5 m
Radar Cross Section
46.485 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 EUTE 9B
1 41310U 16005A   26296.20861396  .00000073  00000-0  00000-0 0  9991
2 41310   0.0725  68.6558 0003908 172.1067 235.0003  1.00272162 39407
Epoch: 2026-10-23T05:00Z
TLE epoch observation values (Epoch: 2026-10-23T05:00:24.246Z)
Latitude
0.02321°
Longitude
8.95447°
Altitude
35,795.396 km
Speed
3.074 km/s
True Right ascension
07h 42m 45s
True Declination
0° 01' 23"
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
13:17:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,804.038 km
Perigee altitude
35,771.081 km
Semi-major axis
42,165.697 km
Eccentricity
0.00039
Inclination
0.0725°
RAAN
68.6558°
Arg. of periapsis
172.1067°
True anomaly
234.96363°
Mean anomaly
235.0003°
Eccentric anomaly
234.98196°
Mean motion
0.25067 °/min
Orbital period
1,436.14 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 #5 in the year 2016 (2016-01-29 UTC)

Documentation

Showing up to 5 results
|