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 UnknownUnknown / 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 (10 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: 10 hours ago

TLE from 10 hours ago
0 EUTE 9B
1 41310U 16005A   26002.74934175  .00000067  00000-0  00000+0 0  9993
2 41310   0.0475  65.3997 0005021 215.1316 100.5923  1.00271872 36459
Epoch: 2026-01-02T17:59Z
TLE epoch observation values (Epoch: 2026-01-02T17:59:03.127Z)
Latitude
-0.03357°
Longitude
9.04406°
Altitude
35,790 km
Speed
3.074 km/s
True Right ascension
01h 24m 46s
True Declination
0° 02' 01"
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
03:53:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,808.812 km
Perigee altitude
35,766.47 km
Semi-major axis
42,165.778 km
Eccentricity
0.0005
Inclination
0.0475°
RAAN
65.3997°
Arg. of periapsis
215.1316°
True anomaly
100.64885°
Mean anomaly
100.5923°
Eccentric anomaly
100.62058°
Mean motion
0.25067 °/min
Orbital period
1,436.15 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
|