EUTE 65W, 41382
Orbit data source: Space-Track
EUTE 65W, 41382 is a payload satellite owned by EutelsatSA (FR) in GEO that was launched on Wed, 09 Mar 2016 UTC via an ARIANE 5ECA launch vehicle from the French Guiana (FRGUI). 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.
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41382 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / EUTERelated business
Manufacturer
SS/Loral (MDA)
Mission
Operational Commercial Communications
Bus & Motor
SSL-1300, R-4D?
Mass
6,564 kg wet, ~3,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 13.0 m
Radar Cross Section
49.949 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 EUTE 65W
1 41382U 16014A 25304.30946414 -.00000266 00000-0 00000-0 0 9990
2 41382 0.0725 46.2417 0002426 182.6735 217.2008 1.00271111 35242Epoch: 2025-10-31T07:25Z
TLE epoch observation values (Epoch: 2025-10-31T07:25:37.701Z)
Latitude
0.03987°
Longitude
-65.20031°
Altitude
35,794.439 km
Speed
3.074 km/s
True Right ascension
05h 44m 15s
True Declination
0° 02' 23"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
08:24:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,798.084 km
Perigee altitude
35,777.625 km
Semi-major axis
42,165.991 km
Eccentricity
0.00024
Inclination
0.0725°
RAAN
46.2417°
Arg. of periapsis
182.6735°
True anomaly
217.184°
Mean anomaly
217.2008°
Eccentric anomaly
217.1924°
Mean motion
0.25067 °/min
Orbital period
1,436.16 mins
BSTAR
0
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Other satellites on launch #14 in the year 2016 (2016-03-09 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.EUTE 65W Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-10-31 12:44:24.233Z | 127.448° SE | 2025-11-01 10:51:24.233Z | 127.447° SE | 25.474° | 2025-11-01 12:44:24.233Z | 127.453° SE |
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41382 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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