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: 22 hours ago
TLE from 22 hours ago
0 INTELSAT 29E
1 41308U 16004A 26284.17594455 -.00000156 00000-0 00000-0 0 9992
2 41308 6.7846 68.8598 0003927 137.8645 23.8606 1.00611564 39447Epoch: 2026-10-11T04:13Z
TLE epoch observation values (Epoch: 2026-10-11T04:13:21.609Z)
Latitude
2.12493°
Longitude
147.5891°
Altitude
35,675.685 km
Speed
3.079 km/s
True Right ascension
15h 22m 48s
True Declination
2° 07' 22"
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
21:02:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,709.183 km
Perigee altitude
35,676.14 km
Semi-major axis
42,070.799 km
Eccentricity
0.00039
Inclination
6.7846°
RAAN
68.8598°
Arg. of periapsis
137.8645°
True anomaly
23.87881°
Mean anomaly
23.8606°
Eccentric anomaly
23.8697°
Mean motion
0.25152 °/min
Orbital period
1,431.3 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
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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 29E is likely not visible in the next few days. |
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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
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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