INTELSAT 33E, 41748
Orbit data source: Space-Track
INTELSAT 33E, 41748 is a payload satellite owned by Intelsat SA (US) (US) in GEO that was launched on Wed, 24 Aug 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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41748 intel report (Beta)
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Identifier
Orbit
Country
US / ITSORelated business
Manufacturer
Boeing/ES
Mission
Non-operational Commercial Communications
Bus & Motor
BSS-702MP, LEROS-2B
Mass
6,552 kg wet, ~2,946 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 22.0 m
Radar Cross Section
59.953 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 INTELSAT 33E
1 41748U 16053B 26307.68518753 .00000106 00000-0 00000-0 0 9997
2 41748 1.9315 82.1300 0024975 192.6440 32.9607 1.00244644 37644Epoch: 2026-11-03T16:26Z
TLE epoch observation values (Epoch: 2026-11-03T16:26:40.202Z)
Latitude
-1.36862°
Longitude
18.242°
Altitude
35,705.947 km
Speed
3.081 km/s
True Right ascension
20h 31m 24s
True Declination
-1° 22' 02"
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
01:53:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,900.602 km
Perigee altitude
35,689.946 km
Semi-major axis
42,173.411 km
Eccentricity
0.0025
Inclination
1.9315°
RAAN
82.13°
Arg. of periapsis
192.644°
True anomaly
33.11682°
Mean anomaly
32.9607°
Eccentric anomaly
33.03872°
Mean motion
0.2506 °/min
Orbital period
1,436.54 mins
BSTAR
0
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Other satellites on launch #53 in the year 2016 (2016-08-24 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 33E Visibility
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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. |
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| INTELSAT 33E is likely not visible in the next few days. |
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41748 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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