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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 INTELSAT 2-F4
1 02969U 67094A 26037.31575546 .00000023 00000-0 00000-0 0 9991
2 02969 3.7433 75.5928 0011653 153.9000 255.3920 1.00372808114009Epoch: 2026-02-06T07:34Z
TLE epoch observation values (Epoch: 2026-02-06T07:34:41.271Z)
Latitude
2.83913°
Longitude
-125.40506°
Altitude
35,769.806 km
Speed
3.075 km/s
True Right ascension
08h 18m 53s
True Declination
2° 50' 11"
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
15:22:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,808.466 km
Perigee altitude
35,710.26 km
Semi-major axis
42,137.5 km
Eccentricity
0.00117
Inclination
3.7433°
RAAN
75.5928°
Arg. of periapsis
153.9°
True anomaly
255.26283°
Mean anomaly
255.392°
Eccentric anomaly
255.32741°
Mean motion
0.25092 °/min
Orbital period
1,434.7 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2026-02-06 13:16:24.548Z | 211.085° SW | 2026-02-07 10:25:24.548Z | 211.482° SW | 34.463° | 2026-02-07 13:16:24.548Z | 210.539° SW |
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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
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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