INTELSAT 32E, 41945
Orbit data source: Space-Track
INTELSAT 32E, 41945 is an American payload satellite in GEO that was launched on Tue, 14 Feb 2017 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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41945 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ITSORelated business
Manufacturer
Airbus/Toulouse
Mission
Operational Commercial Communications
Bus & Motor
EUROSTAR 3000X, R-4D?
Mass
~6,300 kg wet, ~3,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 19.5 m
Radar Cross Section
46.485 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 INTELSAT 32E
1 41945U 17007B 25295.32700272 -.00000260 00000-0 00000+0 0 9992
2 41945 0.0292 101.1606 0000782 277.3991 87.0123 1.00270619 31841Epoch: 2025-10-22T07:50Z
TLE epoch observation values (Epoch: 2025-10-22T07:50:53.035Z)
Latitude
-0.01074°
Longitude
-43.1745°
Altitude
35,786.232 km
Speed
3.075 km/s
True Right ascension
07h 02m 11s
True Declination
0° 00' 39"
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
18:11:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,791.29 km
Perigee altitude
35,784.695 km
Semi-major axis
42,166.129 km
Eccentricity
0.00008
Inclination
0.0292°
RAAN
101.1606°
Arg. of periapsis
277.3991°
True anomaly
87.02125°
Mean anomaly
87.0123°
Eccentric anomaly
87.01677°
Mean motion
0.25067 °/min
Orbital period
1,436.17 mins
BSTAR
0
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Other satellites on launch #7 in the year 2017 (2017-02-14 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.INTELSAT 32E 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 | 2025-10-22 23:05:40.417Z | 108.872° ESE | 2025-10-23 20:59:40.417Z | 108.875° ESE | 12.396° | 2025-10-23 23:05:40.417Z | 108.876° ESE |
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41945 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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