INTELSAT 29E, 41308
Orbit data source: Space-Track
INTELSAT 29E, 41308 is a payload satellite owned by Intelsat SA (US) (US) in GEO that was launched on Wed, 27 Jan 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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41308 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
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: 9 hours ago
TLE from 9 hours ago
0 INTELSAT 29E
1 41308U 16004A 26078.10982330 -.00000085 00000-0 00000-0 0 9990
2 41308 6.2731 71.3925 0000750 247.1500 144.5289 1.00630724 37371Epoch: 2026-03-19T02:38Z
TLE epoch observation values (Epoch: 2026-03-19T02:38:08.733Z)
Latitude
3.26726°
Longitude
-113.27695°
Altitude
35,687.976 km
Speed
3.078 km/s
True Right ascension
06h 51m 41s
True Declination
3° 15' 50"
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
16:06:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,690.48 km
Perigee altitude
35,684.17 km
Semi-major axis
42,065.462 km
Eccentricity
0.00008
Inclination
6.2731°
RAAN
71.3925°
Arg. of periapsis
247.15°
True anomaly
144.53389°
Mean anomaly
144.5289°
Eccentric anomaly
144.53139°
Mean motion
0.25157 °/min
Orbital period
1,431.03 mins
BSTAR
0
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Other satellites on launch #4 in the year 2016 (2016-01-27 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 29E 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 | 2026-03-19 11:18:51.665Z | 191.986° SSW | 2026-03-20 06:28:51.665Z | 191.572° SSW | 37.573° | 2026-03-20 11:18:51.665Z | 189.902° SSW |
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41308 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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