EUTE 117W B, 41589
Orbit data source: Space-Track
EUTE 117W B, 41589 is a payload satellite owned by Eutelsat Americas (FR) in GEO that was launched on Wed, 15 Jun 2016 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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41589 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / EUTERelated business
Manufacturer
Airbus/Toulouse
Mission
Operational Commercial Communications
Bus & Motor
BSS-702SP, XIPS-25
Mass
1,963 kg wet, ~1,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 16.3 m
Radar Cross Section
29.478 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 EUTE 117W B
1 41589U 16038B 25355.18933575 .00000011 00000-0 00000+0 0 9997
2 41589 0.0136 151.8440 0000344 158.1973 91.1465 1.00270361 34875Epoch: 2025-12-21T04:32Z
TLE epoch observation values (Epoch: 2025-12-21T04:32:38.608Z)
Latitude
-0.00808°
Longitude
-116.98334°
Altitude
35,786.522 km
Speed
3.075 km/s
True Right ascension
02h 44m 43s
True Declination
0° 00' 29"
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
12:15:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,789.515 km
Perigee altitude
35,786.614 km
Semi-major axis
42,166.202 km
Eccentricity
0.00003
Inclination
0.0136°
RAAN
151.844°
Arg. of periapsis
158.1973°
True anomaly
91.15044°
Mean anomaly
91.1465°
Eccentric anomaly
91.14847°
Mean motion
0.25067 °/min
Orbital period
1,436.17 mins
BSTAR
0
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Other satellites on launch #38 in the year 2016 (2016-06-15 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 117W B 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 | 2025-12-21 13:14:29.329Z | 198.148° SSW | 2025-12-21 21:14:29.329Z | 198.15° SSW | 33.906° | 2025-12-22 13:14:29.329Z | 198.153° SSW |
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41589 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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