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INTELSAT 2-F4, 2969

Orbit data source: Space-Track

INTELSAT 2-F4, 2969 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Thu, 28 Sep 1967 UTC via a THOR DELTA E1 launch vehicle from the Air Force Eastern Test Range (AFETR). 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
2969, 1967-094A
Orbit
GEO
Country
Flag of UnknownUnknown / ITSO
Related business
Manufacturer
Hughes
Mission
Non-operational Civil Communications
Bus & Motor
HS-303, SVM-1 S/N 3
Mass
163 kg wet, ~65 kg dry
Launch date (UTC)
1967-09-28 (58 years ago)
Launch vehicle
THOR DELTA E1
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.7 m
Radar Cross Section
2.199 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 INTELSAT 2-F4
1 02969U 67094A   25256.19697068  .00000119  00000-0  00000-0 0  9999
2 02969   3.3668  77.0442 0013124 134.1314  48.5886  1.00312639112532
Epoch: 2025-09-13T04:43Z
TLE epoch observation values (Epoch: 2025-09-13T04:43:38.266Z)
Latitude
-0.14663°
Longitude
-163.48127°
Altitude
35,738.229 km
Speed
3.078 km/s
True Right ascension
17h 19m 26s
True Declination
0° 08' 47"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:33:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,831.535 km
Perigee altitude
35,720.888 km
Semi-major axis
42,154.348 km
Eccentricity
0.00131
Inclination
3.3668°
RAAN
77.0442°
Arg. of periapsis
134.1314°
True anomaly
48.70151°
Mean anomaly
48.5886°
Eccentric anomaly
48.64504°
Mean motion
0.25077 °/min
Orbital period
1,435.57 mins
BSTAR
0
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Other satellites on launch #94 in the year 1967 (1967-09-28 UTC)

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