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: 1 day ago
TLE from 1 day ago
0 INTELSAT 2-F4
1 02969U 67094A 25295.58995071 .00000146 00000-0 00000-0 0 9990
2 02969 3.4690 76.6352 0013771 140.4855 229.9787 1.00330150112938Epoch: 2025-10-22T14:09Z
TLE epoch observation values (Epoch: 2025-10-22T14:09:31.741Z)
Latitude
0.61287°
Longitude
-156.71717°
Altitude
35,807.211 km
Speed
3.073 km/s
True Right ascension
05h 47m 42s
True Declination
0° 36' 44"
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
10:29:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,829.35 km
Perigee altitude
35,713.262 km
Semi-major axis
42,149.443 km
Eccentricity
0.00138
Inclination
3.469°
RAAN
76.6352°
Arg. of periapsis
140.4855°
True anomaly
229.85799°
Mean anomaly
229.9787°
Eccentric anomaly
229.91833°
Mean motion
0.25082 °/min
Orbital period
1,435.31 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 | 2025-10-23 15:21:01.066Z | 244.249° WSW | 2025-10-23 19:40:01.066Z | 245.554° WSW | 21.454° | 2025-10-24 15:21:01.066Z | 244.127° WSW |
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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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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