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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2969 intel report (Beta)
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Identifier
Orbit
Country
US / ITSORelated business
Manufacturer
Hughes
Mission
Non-operational spacecraft
Bus & Motor
HS-303, SVM-1 S/N 3
Mass
163 kg wet, ~65 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 INTELSAT 2-F4
1 2969U 67094A 26306.81808779 -.00000268 00000-0 00000+0 0 9993
2 2969 4.4228 72.6389 0013223 152.0726 70.0401 1.00314019116703Epoch: 2026-11-02T19:38Z
TLE epoch observation values (Epoch: 2026-11-02T19:38:02.785Z)
Latitude
-2.96477°
Longitude
-41.81033°
Altitude
35,755.684 km
Speed
3.077 km/s
True Right ascension
19h 39m 09s
True Declination
-2° 57' 42"
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
10:25:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,831.561 km
Perigee altitude
35,720.081 km
Semi-major axis
42,153.958 km
Eccentricity
0.00132
Inclination
4.4228°
RAAN
72.6389°
Arg. of periapsis
152.0726°
True anomaly
70.1826°
Mean anomaly
70.0401°
Eccentric anomaly
70.11134°
Mean motion
0.25078 °/min
Orbital period
1,435.55 mins
BSTAR
0
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Other satellites on launch #94 in the year 1967 (1967-09-28 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 2-F4 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. |
|---|---|---|---|---|---|---|---|
| 247 mins | 2026-11-03 14:34:58.694Z | 105.888° ESE | 2026-11-03 14:34:58.694Z | 105.888° ESE | 13.21° | 2026-11-03 18:41:58.694Z | 109.41° ESE |
| 705 mins | 2026-11-04 02:49:58.694Z | 109.315° ESE | 2026-11-04 10:28:58.694Z | 104.334° ESE | 14.691° | 2026-11-04 14:34:58.694Z | 105.837° ESE |
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2969 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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