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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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Identifier
41308, 2016-004A
Orbit
GEO
Last TLE update
13 hours ago
Origin
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)
2016-01-27 (9 years ago)
Launch vehicle
ARIANE 5ECA
Launch site
French Guiana (FRGUI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 44 m
Radar Cross Section
59.953 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 13 hours ago
0 INTELSAT 29E
1 41308U 16004A   25182.62265287 -.00000257  00000-0  00000-0 0  9998
2 41308   5.6191  74.5793 0004579  39.3104 309.6930  1.00628831 34747
Epoch: 2025-07-01T14:56Z
TLE epoch observation values (Epoch: 2025-07-01T14:56:37.207Z)
Latitude
-1.06526°
Longitude
-80.46374°
Altitude
35,674.068 km
Speed
3.079 km/s
True Right ascension
04h 14m 25s
True Declination
-1° 03' 51"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-0.81748°
Longitude
118.69277°
Altitude
35,703.021 km
Speed
3.077 km/s
Apparent Right ascension
17h 43m 48s
Apparent Declination
-7° 03' 39"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
15:49:41
Azimuth
144.059° SSE
Elevation
36.148°
Doppler factor
1
Orbital elements
Apogee altitude
35,707.118 km
Perigee altitude
35,668.594 km
Semi-major axis
42,065.993 km
Eccentricity
0.00046
Inclination
5.6191°
RAAN
74.5793°
Arg. of periapsis
39.3104°
True anomaly
Unknown
Mean anomaly
309.693°
Eccentric anomaly
Unknown
Mean motion
0.25156 °/min
Orbital period
1,431.05 mins
BSTAR
0
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41308 neighbors
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Other satellites on launch #4 in the year 2016 (2016-01-27 UTC)

INTELSAT 29E 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 mins2025-07-02 04:08:20.183Z144.071° SSE2025-07-02 21:20:20.183Z138.42° SSE33.726°2025-07-03 04:08:20.183Z142.671° SSE
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