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: 12 hours ago
TLE from 12 hours ago
0 EUTE 65W
1 41382U 16014A 25258.50024891 -.00000293 00000-0 00000-0 0 9996
2 41382 0.0757 43.2560 0002174 137.7260 288.6300 1.00272441 34789Epoch: 2025-09-15T12:00Z
TLE epoch observation values (Epoch: 2025-09-15T12:00:21.505Z)
Latitude
0.05212°
Longitude
-65.20711°
Altitude
35,782.943 km
Speed
3.075 km/s
True Right ascension
07h 18m 20s
True Declination
0° 03' 07"
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
16:50:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,796.648 km
Perigee altitude
35,778.315 km
Semi-major axis
42,165.618 km
Eccentricity
0.00022
Inclination
0.0757°
RAAN
43.256°
Arg. of periapsis
137.726°
True anomaly
288.60639°
Mean anomaly
288.63°
Eccentric anomaly
288.6182°
Mean motion
0.25067 °/min
Orbital period
1,436.14 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 | 2025-09-16 00:09:56.739Z | 127.471° SE | 2025-09-16 14:28:56.739Z | 127.412° SE | 25.472° | 2025-09-17 00:09:56.739Z | 127.469° 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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