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: 10 hours ago
TLE from 10 hours ago
0 INTELSAT 32E
1 41945U 17007B 25243.51678513 -.00000265 00000-0 00000-0 0 9994
2 41945 0.0146 104.9478 0000420 322.6723 55.1839 1.00271698 31324Epoch: 2025-08-31T12:24Z
TLE epoch observation values (Epoch: 2025-08-31T12:24:10.235Z)
Latitude
0.00425°
Longitude
-43.1752°
Altitude
35,785.102 km
Speed
3.075 km/s
True Right ascension
08h 11m 12s
True Declination
0° 00' 15"
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
14:13:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,789.461 km
Perigee altitude
35,785.919 km
Semi-major axis
42,165.827 km
Eccentricity
0.00004
Inclination
0.0146°
RAAN
104.9478°
Arg. of periapsis
322.6723°
True anomaly
55.18785°
Mean anomaly
55.1839°
Eccentric anomaly
55.18588°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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Other satellites on launch #7 in the year 2017 (2017-02-14 UTC)
INTELSAT 32E Visibility forecast
Observer location: undefined°, undefined°
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 | 2025-08-31 22:33:03.380Z | 108.863° ESE | 2025-09-01 19:25:03.380Z | 108.844° ESE | 12.392° | 2025-09-01 22:33:03.380Z | 108.864° 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
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