INTELSAT 36, 41747
Orbit data source: Space-Track
INTELSAT 36, 41747 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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41747 intel report (Beta)
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Identifier
Orbit
Country
US / ITSORelated business
Manufacturer
SS/Loral (MDA)
Mission
Operational Commercial Communications
Bus & Motor
LS-1300, R-4D
Mass
3,253 kg wet, ~1,800 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 12.4 m
Radar Cross Section
38.748 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 INTELSAT 36
1 41747U 16053A 26266.14207181 .00000000 00000-0 00000-0 0 9994
2 41747 0.0150 159.2526 0001757 191.9093 130.4816 1.00268694 36944Epoch: 2026-09-23T03:24Z
TLE epoch observation values (Epoch: 2026-09-23T03:24:35.004Z)
Latitude
-0.02567°
Longitude
68.49964°
Altitude
35,791.784 km
Speed
3.074 km/s
True Right ascension
08h 06m 34s
True Declination
0° 01' 32"
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
19:46:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,795.941 km
Perigee altitude
35,781.123 km
Semi-major axis
42,166.669 km
Eccentricity
0.00018
Inclination
0.015°
RAAN
159.2526°
Arg. of periapsis
191.9093°
True anomaly
130.49691°
Mean anomaly
130.4816°
Eccentric anomaly
130.48926°
Mean motion
0.25066 °/min
Orbital period
1,436.19 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 36 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 36 is likely not visible in the next few days. |
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41747 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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